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PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
1Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
1C-130-2208
313N-() SIL 1-86
332D-11() SIL 1-84
332D-11A SB 23
477V-2 SB 3
477V-2 SB 3
51RV-4/4() SIL 1-90
51Y-7/7() SIL 1-84
614E-20R/20S/23R SIL 1-86
614E-20S SB 1
614E-20S SB 1
628T-2/2A SIL 1-84
977B-1-SB-10
AEM ATP 100377A
AEM ATP 100963
AEM ATP 101543
AEM ATP 102669
AEM ATP 102823
AEM ATP 21934
ARC-159/ARC-159(V)SIL1-85
ASB 118R
Nº PUB
USAF
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROCKWELL COLLINS, INC.!DBA
AEROEQUIP - MARKETING DEPT.
FABRICANTE
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
NAT.
0
000
0
0
2
000
0
000
000
0
1
000
0
0
0
0
0
0
0
1
000
ORDEM
GLA324A170000500
GLA323S870002000
GLA334A840007300
GLA334A840007500
GLA325I030053500
GLA325A850002800
GLA334A900006200
GLA334A840007400
GLA323S860003700
GLA334S890007100
GLA334S890007201
GLA323S860003800
GLA323I020007600
GLA300A040000300
GLA300A040000400
GLA300A040000500
GLA300A040000600
GLA300A040000700
GLA300A040000800
GLA323S860003901
GLA371S820003900
FADT
INSPECTION OF EXTERNAL POWERRECEPTACLE PIN
REDUCE GEAR BINDING
CLEANING AND LUBRIFICATION OF SLIP RINGS AND BRUSHES
INSTALLATION OF DUAL SLIP RINGS
ADD CAPABILITY TO TEST 51Y-7/7A AND 614L-11, 614L-12, OR 614L-13
ADD CAPABILITY TO TEST 51Y-7/7A AND 614L-11, 614L-12, OR 614L-13
GLIDESCOPE SELF-TEST INJECTION SIGNAL ADJUSTMENT
ADF-NDB SYSTEM INTEGRITY
SOLENOID SWITCH FAILURES
IMPROVE PUSHBUTTON OPERATION
IMPROVE PUSHBUTTON OPERATION
POWER SUPPLY AG EMI FILTER CAPACITOR REPLACEMENT AND TERMINAL SPACING
TEST PANEL
ADVANCE ENGINEERING MEMORANDUM
ADVANCE ENGINEERING MEMORANDUM
ADVANCE ENGINEERING MEMORANDUM
ADVANCE ENGINEERING MEMORANDUM
ADVANCE ENGINEERING MEMORANDUM
ADVANCE ENGINEERING MEMORANDUM
RADIO SET
AE272 FLEXWRAP SILICONE
TÍTULO
16/05/2016
27/06/1986
12/01/1984
14/03/1984
15/12/1969
15/12/1969
05/02/1990
18/01/1984
06/01/1985
25/03/1988
25/03/1988
14/02/1984
22/02/1997
10/06/1998
27/07/1998
23/10/1998
14/01/1999
28/01/1999
08/05/1998
01/02/1985
01/01/1982
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
I
R
R
R
R
I
R
O
O
R
O
I
I
I
I
I
I
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/06/1986
11/09/1978
15/12/1969
18/01/1984
06/01/1985
02/05/1988
09/03/1984
15/06/1985
01/01/1982
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
2Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
ASB 51RV-4/4-34-A22
ASB 54H60-61-A132
ASB 54H60-61-A134
ASB 54H60-61-A134
ASB 54H60-61-A135
ASB HSI-45-34-A4
BT GL 97 274 C-130 63
BT GL00 056 C-130 018
BT GL00 057 C-130E 019
BT GL00 060 C-130 020
BT GL01 070 C-130 24
BT GL01-072 C-130 25
BT GL01-072 C-130 25
BT GL02-311 C-130 69
BT GL02-312 C-130 70
Nº PUB
ROCKWELL COLLINS, INC.!DBA
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
ROCKWELL COLLINS, INC.!DBA
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
REV
REV
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
NAT.
0
5
1
2
1
000
0
0
0
0
0
0
1
0
0
ORDEM
GLA334S890006300
GLA361S020009600
GLTT61S990046600
GLA300S010000200
GLA300S010000300
GLA334S870001800
SPA322S060001400
GLA324A800012500
GLA329A800012600
GLA324A800012400
GLA300A810009900
GLA361S810008900
GLA360A000000100
GLA320A020007800
GLA320A020007900
FADT
FIRESLEEVE
RIPPLE ON DEVIATION LINES
PROPELLERS-INSPECTION AND REPAIR PROCEDURES FOR PROPELLER BLADE TAPER BORE
PROPELLERS-PROPELLER BLADE INSPECTION
PROPELLERS-PROPELLER BLADE INSPECTION
PROPELLERS-PROPELLER BLADE INSPECTION
POSSIBLE ERONEUS DISPLAY OF COURSE AND OR HEADING
ESTABELECER PROCEDIMENTOS DECOLETA DOS DADOS DE PERFORMANCE E REMESSA DOS DADOS, COLETADOS DOS MOTORESALLISON T56
MODIFICAR TBO DO PN 203430 TURBINE COOLING DE 600 HORASPARA 850
VISA ADOTAR INSTRUCOES DO PN604800 VALVULA HIDRAULICA DESANGRIA
MODIFICAR TBO
RECUPERACAO DO PN FDC 3835-2SUPPORT BRACKET MODIFICANDO-SE A SUA CATEGORIA PARA R
ESCLARECER O PROCESSO DO FENOMENO DE "DESFOLHAMENTO" DE BORDAS DE ATAQUE DE PAS DE HELICE
ESCLARECER O PROCESSO DO FENOMENO DE "DESFOLHAMENTO" DE BORDAS DE ATAQUE DE PAS DE HELICE
"MUDANÇA NA PINTURA DO COMPARTIMENTO DE CARGA DE (...) VERDE FOSCO (FED. STD.36583) PARA (...) VERDE BRILHANTE (FED. STD. 26583)"
MUDANÇA DE COR NA ÁREA DO TREM DE POUSO, DE (...)
TÍTULO
25/11/1986
24/06/1998
17/11/1997
17/11/1997
24/06/1998
28/10/1985
16/09/1997
28/04/1980
22/05/1980
13/06/1980
26/11/1981
10/11/1981
10/11/1981
02/05/2002
02/05/2002
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
R
M
M
M
M
M
I
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/11/2002
24/06/1998
20/03/2001
20/03/2001
28/10/1985
02/03/1999
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
3Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL02-318 C-130 76
BT GL03-322 C-130 78
BT GL03-324 C-130 80
BT GL03-326 C-130 81
BT GL04-330 C130 82
BT GL04-333 C-130 83
BT GL04-333 C-130 83
BT GL04-334 C-130 84
BT GL09-350 C-130-86
BT GL1 064 C-130 021
BT GL1 067 C-130 022
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
0
0
0
0
0
0
0
ORDEM
GLA323A030006900
GLA334A040003800
GLA341A030036800
GLA320S040006900
GLA357A090002800
GLA374A050002900
GLA374A050002900
GLA357A050000200
GLA300A090003300
GLA334S810009600
GLA328A810009700
FADT
ALUMÍNIO (FED. STD. 17178), PARA (...) BRANCO (FED. STD.17875).
"INSTALAR DOIS TRANSCEPTORESVHF 618M-5 (...); INSTALAÇÃODE CAIXAS DE CONTROLE G4422-25 (...)".
INSTALAÇÃO DO SISTEMA "COCKPIT VOICE RECORDER" (CVR), FABRICADO PELA EMPRESA 'L3 COMMUNICATIONS'.
"SUBSTITUIÇÃO DO GTC MODELO 85-71, TIPO AA32A3, PELO APUMODELO GTCP85-180LE, POR MODERNIZAÇÃO DAS ANV C-130".
" 'PALLET VIP' - MODIFICAÇÃODE PALLETS PN HCU-6/E (OU 7031843) E INSTRUÇÕES PARA MANUTENÇÃO PERIÓDICA".
REPARO DE BORON - PARÂMETROSDE INSPEÇÕES.
INCLUIR O P/N RT A1200, "EXTINGUISHER", E O P/N 120-61765-001, "SUPPORT ASSY", NO PROJETO A3, A SER UTILIZADO NAS ANV C-130 DA FAB
INCLUIR O P/N RT A1200, "EXTINGUISHER", E O P/N 120-61765-001, "SUPPORT ASSY", NO PROJETO A3, A SER UTILIZADO NAS ANV C-130 DA FAB
REPARO ASA CENTRAL AERONAVE FAB 2458
PROVIDENCIAR A INSTALAÇÃO DOPROPELLER BETA INDICATOR LIGHT (INDICADOR DE LUZ BETADAS HÉLICES) DAS AERONAVES C-130 MODERNIZADAS.
ESTABELECER TBO PARA O SEQUINTE EQUIPAMENTO 3322-200
INCLUIR DE INSPECAO ESPECIAL
TÍTULO
18/09/2002
28/10/2003
09/10/2003
03/12/2003
06/08/2004
22/11/2004
22/11/2004
29/12/2004
03/04/2009
23/03/1981
04/06/1981
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
R
O
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
4Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL1 068 C-130 023
BT GL12-356 C-130 87
BT GL6 001 C-130 01
BT GL6 002 C-130 02
BT GL6 003 C-130 03
BT GL6 009 C-130 04
BT GL6 017 C-130 006
BT GL7 023 C-130 08
BT GL7 029 C-130 12
BT GL7 031 C-130 11
BT GL78 040 C-130 013
BT GL78 040 C-130 013
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
NAT.
0
0
1
0
0
0
0
0
0
0
1
2
ORDEM
GLA351A810010000
GLA321A120001000
GLTT61S760000700
GLTT61A760001000
GLTT51A760000800
GLTT24S760000900
GLTT23A760001100
GLTT34S770006500
GLA336A780006100
GLTT72S770006800
GLA361S860011401
GLA361S890012902
FADT
PARA EXECUCAO DURANTE O CUMPRIMENTO DO HSC
INVERTER A POSICAO DO PARAFUSO INFERIOR PN MS20005-20
ESTABELER OS PROCEDIMENTOS PARA INSPEÇÃO DOS DUCTOS DE AR QUENTE DO SISTEMA PNEUMÁTICO DAS AERONQAVES C-130
DOTAR A MOUNTING BRACKET ANDCONNECTOR PN 568156 DE PINOSDE ANCORAGEM DO FRENO DOS PARAFUSOS FIXADORES DOS AFTERBODY
FRENAGEM DOS PARAFUSOS DE FIXACAO DOS AFTERBODY DAS AERONAVES C-130
DAR INSTRUCOES PARA TESTES EINSPECOES NA ESTACAO 737,0, MAIS ESPECIFIC NA AREA DO PN356182-1R FITTING BULK HEADDA ANV C-130
DEFINIR O TBO DAS UNIDADES 3S2060DC102D1 E 3S2060DR113A1
MUDANCA DE LOCAL DA ESTACAO AUXILIAR DE RADIO OPERADOR
MODIFICAR O EQUIPAMENTO DME,MOD 680E-2, MUDANDO O SEU PNDE 522-2702-014 PARA 522-2702-054
MODIFICACAO NO SISTEMA DE PARTIDA NOS AVIOES C-130E, NO QUAL O BOTAO DO STARTER SALTAVA COM 56CM A 62% RIM
ESTABELECER AS INSPECOES ANALITICAS DE REVISAO PARA AS TURBINAS DOS MOTORES T56-A-7B, FABRICADOS PARA ALLISON
ALTERAR TBO DOS SEQUINTES COMPONENTES 54H60-117, 582840, 572880
ALTERAR TBO DOS SEQUINTES
TÍTULO
22/07/1981
13/08/2012
20/04/1976
01/04/1976
28/04/1976
01/09/1976
29/11/1976
20/04/1977
10/03/1978
24/11/1977
23/09/1986
16/11/1989
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/10/1976
23/09/1986
16/11/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
5Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL8 040 C-130 013
BT GL8 042 C-130 015
BT GL8-041 C-130 014
BT GL82 075 C-130 27
BT GL82 084 C-130 29
BT GL82 089 C-130 33
BT GL82-085 C-130 30
BT GL82-087 C-130 31
BT GL82-088 C-130 32
BT GL83-098 C-130 35
BT GL83-101 C-130 36
BT GL83-102 C-130 37
BT GL84-116 C-130 39
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
NAT.
0
0
0
0
2
0
0
0
0
0
2
0
0
ORDEM
GLA361S780006200
GLA324A780006000
GLA327A780006300
GLA351A820010800
GLA305A970007002
GLA309A820010900
GLA351A820010000
GLTT00A860000100
GLA352A820009900
GLA305S830010800
GLA338A840019402
GLA324A830010900
GLA372S840019500
FADT
COMPONENTES 54H60-117, 582840, 572880
ALTERARA TBO DOS SEQUINTES COMPONENTES PNS 54H60-117, 582840, 582855
INSTALACAO DE 2 SPORT LIGHTSNOS AVIOES KC-130 2461 E 2462
ESTABELECER UMA INSPECAO URGENTE E INSPECOES ESPECIAIS P/OS PNS 339404, USADOS EM CONJUNTO COM OS ROD ASSY
ABRIR JANELA PARA ACESSO AO SWITCH PN 8911K525
INSTRUCOES P/INSPECOES,CONTROLE E TROCADE MANGUEIRAS USADAS NOS HIDRAULICOS...
ESTABELECIMENTO DE LIMITE PARA O PESO MAXIMO DAS ANVS C-130 A SER OBSERVADOS NAS OPERACOES DE TRATORAMENTO
MODIFICACAO DO P/N 397145-1 FITTING, PYLLON ATTACH, REARE DO P/N 382095-3 EYEBOLT, PYLON SUPPOR, OUTER WING, REAR BEAM
COLOCACAO DE DISPOSITIVO ANTI-CORROSIVO (CROMATO DE ESTRONCIO-CAPSULA), NAS ASASDOS AVIOES C-130.
COLOCACAO DE UM REFORCADOR EXTERNO SOBRE A PORTA DA TRIPULACAO NA WL 195
ESTABELECER OS ITENS CONTROLADOS, FIXAR SEUS RESPECTIVOS "TBOS"
REMOCAO DSO 2 MICTORIOS DA ESTACAO DA FUSELAGEM 245.0
INSTALACAO DE UM CRT BREAK NO PANEL BOX JUNCION, PASSAGEM...
COLOCACAO DE UMA JANELA DE INSPECAO NO LADO DIREITO DO
TÍTULO
03/09/1978
04/12/1978
05/10/1978
18/03/1982
30/06/1982
03/11/1982
24/06/1982
09/09/1982
09/08/1982
14/09/1983
01/09/1983
15/09/1983
17/05/1984
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/10/1997
04/06/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
6Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL84-125 C130 40
BT GL84-126 C-130 41
BT GL85-129 C-130 42
BT GL85-130 C-130 43
BT GL85-137 C-130 45
BT GL85-143 C-130 46
BT GL86-146 C-130 47
BT GL86-147 C-130 48
BT GL86-147 C-130 48
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
NAT.
0
0
0
0
0
1
0
0
1
ORDEM
GLA325A840020000
GLA325A840019900
GLA325A850009900
GLA332S850000400
GLA372A850010500
GLA325S860009501
GLA353A860010300
GLA379S860010400
GLTT70A860000200
FADT
REVEST. DOS QEC. DE TURBINASDOS C-130
ALTERAR A TBO (TIME BETWEEN OVERHAUL) DOS SEGUINTES COMPONENTES E SEUS RESPECTIVOS ALTERNADOS E CANCELAR O BT GL7 028 C130 010
MODIFICACAO DOS TRILHOS, FIXACAO DO SISTEMA PALETES DO PISO E POSICIONAMENTO DOSBANCOS DE PASSAGEIROS
COLOCACAO DE CAIXAS PARA CORRENTE NA ALTURA DA ESTACAO DA FUSELAGEM 245.0.
INFORMAR SOBRE O NOVO ESTADODE DESMONTAGEM NO QUAL OS TRENS-DE-POUSO DO NARIZ(NLG)DAS AERONAVES C-130 DEVERAO ESTAR QUANDO ...
INFORMAR O PROCEDIMENTO P/CUMPRIMENTO DO PROGRAMA DEANALISE ESPECTROMETRICA DE OLEOS (PAEO) NOS MOTORES T56E "GEAR BOXES"
IMPLANTACAO DE NOVO LUBRIFICANTE PASTOSO NOS CABOS E FERRAGENS COMANDO BOTES SALVA-VIDAS
MODIFICACAO ESTRUTURAL NO LOCAL ONDE EXISTIA UMA ANTENA "DOPPLER" NAS AERONAVES C-130
ESTENDER O TEMPO DE SUBSTITUICAO DE ALGUMAS MANGUEIRAS DE BORRACHA, USADAS NOS "POWER PACKAGES" DOS MOTORES T56A-78 E T56A-15 ...
ESTENDER O TEMPO DE SUBSTITUICAO DE ALGUMAS MANGUEIRAS DE BORRACHA, USADAS NOS "POWER PACKAGES" DOS MOTORES T56A-78 E T56A-15 ...
TÍTULO
17/10/1984
18/10/1984
15/03/1985
18/03/1985
06/08/1985
18/11/1985
10/03/1986
18/07/1986
18/07/1986
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
25/02/1986
30/07/1999
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
7Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL88-151 C-130 49
BT GL88-159 C-130 050
BT GL88-163 C-130 50
BT GL88-164 C-130 51
BT GL91-004 C-130 01
BT GL91-004 C-130 01
BT GL91-02 C-130 023
BT GL92-011 C-130 01
BT GL92-012 C-130 02
BT GL93-234 C-130 58
BT GL94-233 C-130 57
BT GL94-233 C-130 57
BT GL94-255 C-130 59
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
NAT.
0
0
0
0
0
0
0
0
0
0
1
1
0
ORDEM
GLA353A880011000
GLA324A880011200
GLA305S880011300
GLA353A880010900
GLA325A910013900
GLTT00A960025800
GLA327A910014000
GLTT05S920012400
GLTT53A920012300
GLA322A930003000
GLA300A940004900
GLA300A950007301
GLA332A940000101
FADT
INSTALACAO DO BERCO E SUPORTE DAS ROLDANAS DO ALVOA SER RECOLOCADOS PELAS AERONAVES C-130
ESTABELECER PROCED. PARA INSTALACAO DE 2 LAMPADAS BREAKWAY NOS "PODS"
FIXAR O TBO DO P/N 28B58-9B GENERATOR PARA 5000H INDEPENDENTE DE SUA LOCALIZACAO(MOTOR OU APU)...
INSTALACAO DE TRILHOS PARA FIXACAO DE CADEIRAS PARA OS OBSERVADORES NAS MISSOES DE BUSCA
APERFEICOAMENTO E REATIVACAODO SISTEMA DE ALIJAMENTO DE CARGA
APERFEICOAMENTO E REATIVACAODO SISTEMA DE ALIJAMENTO DE CARGA
COMPLEMENTAR AS INSTRUCOES DA FADT 140/88 REV.1 23/08/91 - SB 82-611
ESTABELECER O TBO (TIME BETWEEN OVERHAUL) DOS SEGUINTES COMPONENTES E SEUSRESPECTIVOS ALTERNADOS E CANCELAR O BT GL84-125 C130...
FECHAMENTO DA CARENAGEM P/N 388151-37 (DOOR ASSY), DE ACESSO AO COMPART...
TRANFERIR AS CARGAS DO FLIGHT DIRECTOR 1 E 2 E DOS VERT. GYRO 1 E 2 DA FASE A P/ A FASE B DO COPILOTS INSTR. POWER INVERTER(D20A)
NORMATIZAR O SISTEMA DE MANUTENCAO DAS AERONAVES C-130 E/H DE ACORDO COM ...
NORMATIZAR O SISTEMA DE MANUTENCAO DAS AERONAVES C-130 E/H DE ACORDO COM ...
ABERTURA DE DUAS JANELAS DE
TÍTULO
04/05/1988
19/05/1988
23/08/1988
14/09/1988
03/06/1991
03/06/1991
26/08/1991
02/04/1992
26/05/1992
10/12/1993
19/08/1994
19/08/1994
31/12/1984
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
07/03/1995
07/03/1995
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
8Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
BT GL94-257 C-130 60
BT GL94-260 C-130 61
BT GL98-300 C-130 65
BT GL99-302 C-130 67
BT SP13 543 C-130 002
BTGL00-304 C-130 68
CEB 72-1501
CEB 72-1502
CEB 72-1503
CEB 72-1506
CEB 72-1507
CEB 72-1508
CEB 72-1509
CEB 72-1511
CEB 72-1511
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMASP
PAMAGL
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
DETROIT-DIESEL/ALLISON DIV PLANT 2A
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
BSC
REV
REV
REV
BSC
BSC
REV
REV
REV
BSC
REV
RVC
RVC
REV
REV
NAT.
0
2
1
1
0
0
2
1
1
000
3
2
1
1
1
ORDEM
GLA351A960001601
GLA300A020000500
GLA328S020010200
GLA334A020010500
SPA341S130000500
GLA353A020008100
GLA372S910014802
GLA300S020070300
GLTT72S920001801
GLA383A800010601
GLA300S020073800
GLA300S030009100
GLA300S030004100
GLA372S820003601
GLA372S820003602
FADT
ACESSO NA CARENAGEM DO TREM DE POUSO PRINCIPAL DIREITO.
VERIFICAR A INTEGRIDADE ESTRUTURAL DOS REPAROS EXECUTADOS NOS "LONGERONS"...
NORMATIZAR PROCEDIMENTOS PARA PREVENCAO E CONTROLE DECORROSAO NAS AERONAVES C-130E/H
AUMENTAR A PROTECAO DA CABLAGEM UTILIZADA NA BOMBA DE COMBUSTIVEL PN 60-369A, NOM FUEL PUMP
INSTALAR O TRANSMISSOR LOCALIZADOR DE EMERGENCIA (TLE) DE PN 453-0405 FABRICADO PELA ARTEX, EM SUBSTITUICAO ...
ESTABELECER E PADRONIZAR OS PROCEDIMENTOS TÉCNICOS A SEREM EXECUTADOS NA OFICINA DE PNEUMATICA P/ DETERMINAR INSPEÇÕES PERÍODICAS.
PONTOS DE ATERRAMENTO NAS AERONAVES C-130
ENGINE - REDUTION GEAR TACHOMETER BEARING OIL TUBE
ENGINE - REDUCTION GEAR TACHOMETER DRIVE BEARING
ENGINE - TURBINE SECOND STAGE BLADES - REPLACE
ENGINE - COMBUSTION CHAMBER INNER CASING ASSEMBLY REWORK
ENGINE, TURBINE SECOND-STAGEBLADES - REPLACE.
ENGINE, TURBINE FIRST, SECOND, AND THIRD-STAGE BLADES - REPLACE
ENGINE - TURBINE FIRST - STAGE WHEEL ASSEMBLY - REPLACE
ENGINE - TURBINE SECOND STAGE VANES - REPLACE
ENGINE - TURBINE SECOND
TÍTULO
20/10/1994
18/11/1994
31/08/1998
09/08/1999
04/06/2013
30/06/2000
15/08/1974
16/09/1971
31/01/1978
20/12/1977
18/09/1974
30/06/1975
28/08/1972
31/01/1978
31/01/1978
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
I
M
R
M
M
R
R
R
R
R
M
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/02/2002
18/03/1999
30/10/2000
28/08/1975
26/04/1976
22/12/1978
20/12/1977
24/02/1977
07/02/1977
04/11/1976
15/09/1978
15/09/1978
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
9Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CEB 72-1512
CEB 72-1513
CEB 72-1516
CEB 72-1517
CEB 72-1518
CEB 72-1521
CEB 72-1522
CEB 72-1523
CEB 72-1524
CEB 72-1525
CEB 72-1526
CEB 72-1527
CEB 72-1529
CEB 72-1529
CEB 72-1530
CEB 72-1531
CEB 72-1533
CEB 72-1534
CEB 72-1536
CEB 72-1537
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
RVC
REV
REV
REV
REV
REV
REV
BSC
REV
REV
BSC
REV
REV
REV
REV
BSC
REV
BSC
BSC
BSC
NAT.
1
3
1
1
2
1
1
0
1
2
0
1
1
5
1
0
2
0
0
0
ORDEM
GLA322S030003300
GLA300S020075600
GLA300S020072000
GLA300S020072600
GLTT61A980064500
GLA372S850002101
GLA372S830003801
GLA300S020074500
GLA300S020074400
GLA383S910006302
GLA372S020074200
GLA300S030008300
GLA372S910003405
GLA300S020074100
GLA300S020074600
GLA372S840005701
GLA300S020076500
GLA372S820003700
GLA300S020074900
GLTT72S920002000
FADT
STAGE VANES - REPLACE
ENGINE - INNER REAR EXHAUST CONE SELF - LOCKING NUT- REPLACE
ENGINE - TURBINE VANE CASINGREPLACE
ENGINE - FIRST STAGE TURBINEVANES-REPLACE
ENGINE - REDUCTION GEAR BOX STARTER DRIVE SHAFT BEARING
ENGINE - GAS TURBINE OPERATIONS
ENGINE - REDUCTION GEAR PROPELLER SHAFT THURST NUT CUPLOCK-ADD
ENGINE - REDUCTION GEAR REARHOUSING OIL SEAL ADD
ENGINE - COMBUSTION LINER THERMOCOUPLE GROMMETS
ENGINE - REAR CARRIER...
ENGINE - ACCESSORY DRIVE HOUSING UNION - REPLACE
ENGINE- COMBUSTION LINER CROSSOVER TUBE CLAMPS-ADD
ENGINE - EXTERNAL SCAVENCE OIL FILTER SYSTEM, INSTALL...
ENGINE- REDUCTION GEAR MAIN DRIVE GEAR, MOLYBDENUM SPRAY
ENGINE- REDUCTION GEAR MAIN DRIVE GEAR, MOLYBDENUM SPRAY
ENGINE - COMPRESSOR DIFFUSERPUMP...
ENGINE - REDUCTION GEAR, LOCKED RACES FOR MAIN DRIVE,REAR CARRIER AND FRONT PINION BEARINGS - ADD
ENGINE - FIRST STAGE TURBINEBLADE - INCREASE
ENGINE - COMPRESSOR VANE ASSEMBLY AIR SEALS-REPLACE
REDUCTION GEAR BEARING BORE-ENBARGE
REDUCTION GEAR, REAR PINION
TÍTULO
08/11/1971
25/03/1978
31/01/1978
21/03/1978
30/01/1978
16/04/1982
15/07/1982
31/10/1979
20/02/1981
31/08/1980
01/10/1984
30/09/1980
01/05/1981
01/05/1981
22/04/1981
19/03/1984
20/02/1981
28/05/1982
02/08/1985
02/03/1984
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
R
R
R
R
M
R
M
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
21/01/1977
21/12/1979
19/09/1978
14/12/1979
10/08/1984
30/06/1982
20/05/1983
30/09/1981
02/01/1989
15/08/2001
31/07/1981
15/07/1992
15/05/1981
20/01/1982
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
10Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CEB 72-1538
CEB 72-1539
CEB 72-1544
CEB 72-1545
CEB 72-1547
CEB 72-1548
CEB 72-1549
CEB 72-1553
CEB 72-1554
CEB 72-1555
CEB 72-1556
CEB 72-1557
CEB 72-1560
CEB 72-1562
CEB 72-1566
CEB 72-1567
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
BSC
REV
BSC
RVC
BSC
BSC
BSC
REV
RVC
REV
BSC
REV
BSC
BSC
BSC
REV
NAT.
0
1
0
2
0
0
0
2
3
1
0
3
0
0
0
1
ORDEM
GLA371S840005200
GLTT72S920002201
GLA300S020074800
GLA300S030003400
GLA371A840018900
GLA300S020072300
GLA371A860008500
GLA300S020076400
GLA322S030003600
GLA372S910003601
GLTT72S920002300
GLA372S930001203
GLA300S020073100
GLA372S020073000
GLA300S020073400
GLA300S030002200
FADT
BEARING-REPLACE REAR HOUSING- REWORK TO PROVIDE INCREASED LUBRICATION
ENGINE - REDUCTION GEAR, PROP SHAFT THRUST BEARING-OUTER RACE LOCK-ADD
ENGINE REDUCTION GEARBOX-OILPUMP VALVE SHAFT REWORK AND REPLACE
ENGINE REDUCTION GEAR ASSY PLAQUET GEAR AND BEARING
ENGINE - TURBINE ASSEMBLY - REAR BEARING SUPPORT CONE ASSY-SERVICE REPAIR
ENGINE - POWER SECTION CONTROL ASSY-DIFFUSER BLEED PORT FLANGE
ENGINE - REDUCTION GEAR ASSY-PROP THRUST NUT LOCK CUP
ENGINE - SPLINE TURBINE, STARTER SHAFT 3/4 DRIVE
ENGINE - REDUCTION GEAR UNITSUN GEAR FLANGE HUB-REWORK
ENGINE - REDUCTIONS GEAR ASSY - TACHOMETER DRIVE IDLER GEAR -SHOT PEEN
ENGINE - TURBINE SECOND STAGE WHEEL, INSPECT
ENGINE - REDUCTION GEAR ASSEMBLY SAFETY COUPLING INTERMEDIATE INSPECT
ENGINE AIR INLET HOUSING,INSPECT REWORK
REDUCTION GEARBOX REAR CARRIER BEARING, SERVICE ABLILITY CRITERIA
3RD, 4TH, AND 5TH STAGE COMPRESSOR BLADE, INSPECTIONREQUIREMENTS
REAR CHARGER BEARING INSPECTION
APPROVED LIQUID GAS PATH CLEANERS
TÍTULO
19/03/1984
15/02/1985
09/05/1983
13/03/1985
16/03/1984
05/10/1984
20/03/1986
15/02/1985
22/12/1986
01/01/1989
15/09/1991
15/03/1992
21/12/1992
30/09/1993
26/01/1998
01/02/1998
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
R
R
R
O
R
R
M
R
R
R
M
R
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/08/1990
15/09/1998
20/08/1987
23/10/2000
30/03/1991
30/11/1996
23/09/2002
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
11Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CEB 72-1568
CEB 72-1569
CEB 72-1570
CEB 72-1573
CEB 72-1574
CEB 72-1575
CEB 72-1578
CEB 72-1580
CEB 72-346
CEB 72-4027
CEB 73-1501
CEB 73-1502
CEB 73-1505
CEB 73-1510
CEB 73-1511
CEB 73-1512
CEB 73-1512
CEB 73-1515
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
BSC
BSC
RVC
RVC
RVC
RVC
RVC
BSC
REV
BSC
BSC
BSC
REV
REV
REV
REV
REV
RVC
NAT.
0
0
1
1
1
2
2
0
001
000
0
0
1
1
1
1
1
2
ORDEM
GLA300S020073200
GLA322S020080800
GLA300S020076600
GLA322S020081000
GLA322S020080400
GLA300S020080600
GLA322S030003000
GLA322S030003500
GLTT72S770001401
GLTT72S920006800
GLA322S030008000
GLA372S800011100
GLA372S870001100
GLTT73S920004101
GLA373S870005401
GLA373S900006001
GLA373S900027301
GLA300S020080200
FADT
COMPRESSOR INLET BLOCKAGE
OIL FOAMING
T56/501-D SOLID STATE AMPLIFIER ADJUSTMENT
NEW REAR COMPRESSOR BEARING PN 23057662
NEW TORQUIMETER MID-BEARING PN 23064888
ENGINE, 14TH STAGE COMPRESSOR WHEEL, SILVER/INDIUM PLATING REMOVAL
REDUCTION GEAR SIDE SCREW BUSHING - REPLACE
RELEASE OF IMPROVED 1ST-STAGE TURBINE BLADE
REDUCTION GEAR-MAIN OIL PUMPAND FILTER ASSEMBLY-REWORK
ENGINE, AIR INLET HOUSING, INSPECT/REWORK
ENGINE FUEL & CONTROL - FUELCONTROL METERING VALVE SPRING NYLON SNUBBING BLOCK -- ADD
ENGINE FUEL AND CONTROL-FUELCONTROL THERMOSTAT
ENGINE FUEL AND CONTROL-SPEED SENSITIVE CONTROL DRIVE CONPLING-REPLACE
ENGINE FUEL CONTROL - ANTI-ICING AIR TUBE PROBE REPLACE
ENGINE FUEL AND CONTROL FUELNOZZLE INSPECTION
ENGINE FUEL AND CONTROL-SHROUDED ANT-ICE PROBE-REWORK
ENGINE FUEL AND CONTROL-SHROUDED ANT-ICE PROBE-REWORK
TURBINE ENGINE MAIN FUEL CONTROL NEW SERVICE LIMITS FOR GOVERNOR SHAFTS
TÍTULO
01/02/1998
01/02/1998
26/01/1998
14/05/1999
14/05/1999
10/08/1999
23/05/1983
18/03/2002
16/09/1971
15/03/1992
04/10/1976
13/11/1979
15/08/1973
05/03/1986
20/05/1986
01/07/1988
01/07/1988
01/09/1990
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
I
R
R
M
R
R
R
M
M
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/06/1998
05/05/2000
05/05/2000
20/07/2000
18/05/2001
25/03/1974
15/03/1992
15/07/1980
01/09/1990
10/07/1986
01/01/1990
01/01/1990
19/05/1998
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
12Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CEB 75-1501
CEB 75-1503
CEB 77-1501
CEB A-73-1507
CEB-72-1587
COIL-1027
COIL-1027
COIL-1503
COIL-1510
COIL-1510
COIL-1514
CSL 1533
CSL 1535
CSL 1554
CSL 1555
CSL 1556
CSL 1557
CSL 72-1566
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
DETROIT DIESEL
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE CORP
ALLISON ENGINE CO
ALLISON ENGINE CO
ALLISON ENGINE CO
ALLISON ENGINE CO
FABRICANTE
REV
BSC
REV
BSC
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
NAT.
1
0
1
0
0
0
1
001
0
000
000
0
0
0
0
0
2
0
ORDEM
GLA372S800010901
GLA300S020073500
GLA300S020075100
GLA300S020075400
SPA300S060001900
GLA372S870001200
GLA372S870001301
GLA372S820003800
SPA300S070003900
GLA372S800004500
GLA372S800004900
GLA372S020011500
GLA372S850002400
GLA322S030001200
GLA372S020011700
GLA377S020012000
GLA300S030000400
GLA322S030009000
FADT
AIR-COMPRESSOR AIR BLEED COLLECTOR ASSEMBLY REWORK
AIR-POWER SECTION ASSY ANTI-ICING AIR OUTLET FITTING-REPLACE
ENGINE INDICATING-THER MOCOUPLE INSPECTION
FUEL AND CONTROL BENDIX MODEL AP-B3 INSPECTION
NEW 5TH & 10TH STAGE BLEED GASKET PN 23079417 & 23079416
SERIES III TURBINE VANE INNER BAND SEAL TO SPACER KNIFE SEAL CLEARANCES.
SERIES III TURBINE VANE INNER BAND SEAL TO SPACER KNIFE SEAL CLEARANCES.
OVERHAUL OF FUEL NOZZLE SPRAY TIPES.
MATERIAL IDENTIFICATION OF COMMERCIAL TURBINE BLADES FOR ALPAK PURPOSES
MATERIAL IDENTIFICATION OF COMMERCIAL TURBINE BLADES FOR ALPAK PURPOSES
T56/501 SERIES II ENGINE-IMPROPER ASSEMBLY
ALLISON T56-LFE ENGINES-GENERAL INFORMATION
REDUCTION GEAR PROP SHAFT SEAL PN 6851491
T56-A-7A/B TO T56-A-15LFE CONVERSION KITS RELEASE
"INTRODUTION OF NEW COMPRESSOR 5TH- AND 10TH- STAGE BLEED GASKETS".
OPERATION AND MAINTENANCE OFTHE 501D/T56LFE THERMOCOUPLE".
"TURBINE MODULE INSTALLATIONKIT RELEASE".
"SCAVENGE OIL SYSTEM TEST KIT, 23008696".
TÍTULO
04/12/1974
01/10/1984
20/05/1986
22/03/1982
31/10/2005
30/04/1975
30/04/1975
13/08/1976
25/08/1978
25/08/1978
07/12/1979
15/07/1983
28/03/1985
28/06/1995
06/07/1995
06/07/1995
24/07/1995
09/10/1995
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
M
M
I
I
R
I
I
I
I
I
I
R
I
I
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/08/1980
10/07/1986
23/05/1975
22/04/1982
25/08/1978
07/12/1979
01/12/1997
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL ORGÂNICO/OPER
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
13Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CSL-1502
CSL-1502
CSL-1503
CSL-1506
CSL-1507
CSL-1508
CSL-1509
CSL-1510
CSL-1511
CSL-1512
CSL-1513
CSL-1515
CSL-1517
CSL-1519
CSL-1520
CSL-1520
CSL-1521
CSL-1522
CSL-1524
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
REV
REV
BSC
BSC
REV
BSC
BSC
BSC
BSC
CHG
BSC
BSC
REV
BSC
BSC
REV
BSC
BSC
REV
NAT.
6
8
0
0
21
0
0
0
0
3
0
0
4
0
000
001
0
0
2
ORDEM
GLA379S830003906
GLA379A140000200
GLA372S780002100
GLA370S800005400
GLA300S030002300
GLA300S020076700
GLA379S780002500
GLA379S980002000
GLA371S980001600
GLA379S790003803
GLA379S780002300
GLA371S980001800
GLA300S030002100
GLA371S780001800
GLA371S850002300
GLA371S850002501
GLA371A860008900
GLA372S800004400
GLA300S020078600
FADT
APPROVED LUBRICANTS - ENGINEOIL SYSTEM
APPROVED LUBRICANTS - ENGINEOIL SYSTEM
REDUCTION GEAR STARTER PAD DRAIN HOLE
501-D22A, -D22C AND T56-A-15LFE ENGINE TORCHING
AUTHORIZED ENGINE OVERHAUL AND REPAIR CENTERS
USE OF URIDE SHROND SECOND STAGE TURBINE BLADES
ENGINE OIL SYSTEM-CLEANING
ENGINE OIL LOSS
USE OF CUPWASHER BOCKING DEVICES ON REDUCTION GEAR ASSY ACCES-SORY DRIVES
501D- D13- D36 -D22 -D22A, -D22C AND T56-A-15LFE ENGINE OIL LEAKAGE
ENGINE - PROPELLER CONTROL LINKAGE INSPECTION
USE OF FRONT COMPRESSOR BEARING CONTAINING CORROSIONRESISTANT...
PROCUREMENT OF PUBLICATION
DELETION OF INTERNAL RELAINING RING PN 6842789
INSPECTION OF PROPELLER SHAFT THRUST NUT LOCK INSTALLATION ON POWER PLANT INSTALLATIONS WITH HAMILTON STANDARD PROPELLERS.
INSPECTION OF PROPELLER SHAFT THRUST NUT LOCK INSTALLATION ON POWER PLANT INSTALLATIONS WITH HAMILTON STANDARD PROPELLERS.
PERMANENT IDENTIFICATION OF SCARP PARTS
MAGNETIC PLUGS P/N 6792118, 6822092 AND 6822222
FIRE EXTINGUISHER MATERIAL
TÍTULO
16/02/1973
16/02/1973
15/02/1974
31/05/1974
31/07/1974
28/02/1975
04/09/1975
04/04/1975
23/01/1976
13/02/1976
05/03/1976
23/12/1977
22/10/1976
31/01/1978
21/07/1978
21/07/1978
10/10/1978
29/01/1979
30/08/1979
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
R
I
I
I
I
I
R
R
R
R
I
I
R
R
I
I
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
08/12/1997
19/05/2008
08/04/2002
02/02/1978
11/03/2002
21/07/1978
30/07/1981
27/02/1980
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
14Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CSL-1526
CSL-1527
CSL-1528
CSL-1528
CSL-1530
CSL-1531
CSL-1536
CSL-1537
CSL-1538
CSL-1539
CSL-1543
CSL-1543
CSL-1544
CSL-1546
CSL-1547
CSL-1551
CSL-1553
CSL-1554
CSL-1559
CSL-1561
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE
ROLLS ROYCE
ALLISON ENGINE CO
ALLISON ENGINE CO
FABRICANTE
BSC
BSC
BSC
REV
REV
BSC
RVC
BSC
BSC
BSC
BSC
REV
REV
BSC
BSC
REV
REV
CHG
RVC
REV
NAT.
0
0
000
1
3
0
4
0
0
0
0
1
1
0
0
1
2
2
1
2
ORDEM
GLA371A870005100
GLA361S800005300
GLA372S910004400
GLA372S910003701
GLTT72S920003203
GLTT72S840000100
GLA300S020077700
GLA300S020077300
GLA371A860009000
GLA300S020078000
GLA372S910004200
GLA372S910004301
GLTT00X980021900
GLA371A910004100
GLTT71S920003400
GLA300S030002400
GLA300S030002500
SPA322S060001800
GLA300S030001800
GLA300S030008700
FADT
(CLEANING)
ENGINE INSPECTION REQUIREMENTS WHIN EXPOSED TOVOLCANIC
UN EXPLAINED LOSS OF PROPELLER OIL
OIL LEAKAGE - ACCESSORY DRIVE HOUSING FITTING
OIL LEAKAGE - ACCESSORY DRIVE HOUSING FITTING
LFE PART NUMBER DIFFERENCES
TURBINE VANE TO SPACER RUBBING
PROPELLER RETAINING NUT TORQUE
IDENTIFICATION OF ALLISON POWER PARTS "APP"
REDUCTION GEAR PROPELLER SHAFT SEAL ASSEMBLY
RETURN OF PARTS FOR FIELD INVESTIGATION AT ALLISON...
OPERATION OF BENDIX FUEL CONTROLS EXPOSED TO FIRE OF SEVERE OVER TEMPERATURE.
OPERATION OF BENDIX FUEL CONTROLS EXPOSED TO FIRE OF SEVERE OVER TEMPERATURE.
IMPROVED ANTI-ICING AIR VALVE SEALS
REDUCTION GEAR ASSEMBLY SPLITLINE TORQUE PROCEDURE
EXCESSIVE OIL CONSUMPTION INFLIGHT AND/OR ON GROUND.
ENGINE GROUND STARTING PROCEDURES
"ROLLS-ROYCE PARTS ORDERING PROCESS".
T56-A-7A/7B TO T56-A-15LFE CONVERSION KITS RELEASE
"POWER SECTION AND REDUCTIONGEARBOX OIL PRESSURE LIMITS".
ENGINE PERFORMANCE GROUND
TÍTULO
02/06/1980
15/07/1980
12/02/1981
12/02/1981
15/10/1981
30/11/1982
15/06/1986
15/08/1985
26/02/1986
28/02/1986
01/12/1988
01/12/1988
01/08/1989
28/02/1991
28/02/1991
15/03/1993
28/06/1995
28/06/1995
31/07/1995
29/11/1996
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
M
I
I
I
M
I
I
I
I
I
M
I
I
R
I
O
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
12/02/1981
28/02/1991
15/12/1991
26/01/1998
01/04/1990
31/01/1994
01/09/1995
11/03/2002
15/06/2005
05/05/1999
22/03/2001
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
GERAL
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL BASE
NÍVEL BASE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
15Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CSL-1562
CSL-1563
CSL-1564
CSL-1565
CSL-1569
CSL-1571
CSL-1573
CSL-1574
CSL-1575
CSL-1576
CSL-1577
CSL-1578
CSL-1579
CSL-1580
CSL-1581
CSL-1582
CSL-1583
CSL-1584
CSL-1585
Nº PUB
ALLISON ENGINE CO
ROLLS ROYCE CORP
ROLLS ROYCE CORP
ROLLS ROYCE CORP
ALLISON TRANSMISSION, INC.
ROLLS ROYCE CORP
ROLLS ROYCE CORP
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE CORP
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE CORP
ROLLS ROYCE CORP
ROLLS ROYCE CORP
ALLISON TRANSMISSION, INC.
ROLLS ROYCE CORP
ROLLS ROYCE CORP
FABRICANTE
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
1
0
0
0
0
0
0
0
0
0
0
0
0
0
0
ORDEM
GLA322S020079200
GLA300S030000700
GLA322S030001700
GLA322S030001300
GLA322S020079900
GLA322S030000600
GLA322S030001000
GLA322S020079500
GLA322S020078900
GLA322S020078800
GLA322S030000800
GLA322S020079000
GLA300S020079400
GLA322S030000900
GLA300S030000100
GLA322S030000200
GLA300S030001600
GLA300S030000300
GLA300S030000500
FADT
CHECK PROCEDURE PERFORMANCE CALCULATIONS AND TRENDING SUPORT EQUIPMENT RELEASE
"FUEL NOZZLE BOLT LUBRICANT".
PROPELLER SHAFT CLEANING AT INSTALLATION
ENGINE FUEL NOZZLE CLEANING
ENGINE PARALLELING VALVE FAULT ISOLATION
IMPROVED STARTING FUEL SCHEDULE
COMPRESSOR INLET SENSING PROBE TORQUE
T56/501-D SERIES III 2ND-STAGE WHELL MEASUREMENT
T56/501-D SERIES II & III UNEXPLAINED OIL LOSS
OPERATION AND MAINTENANCE OFT56/501-D ENGINES IN EROSIVEAND CORROSIVE ENVIROMENTS
T56/501-D ENGINE OVERTOQUE ORHORSEPOWER LIMITATION EXCEEDENCE
ALLISON T56-LFE ENGINES
USE OF FLOW SPEED GROUND IDLE (LSGI)
T56/501-D PINION BEARING LIMITS
T56/501D ENGINE TORCHING AT HIGH POWER SETTINGS
TITANIUM NITRIDE (TIN) COATED COMPRESSOR BLADES
ROLLS-ROYCE ALLISON REPAIREDCOMBUSTION LINER EXCHANGE PROGRAM
"WATER QUALITY FOR ENGINE COMPRESSOR WASH/RINSE".
ALTERNATIVE SUBSTANCES FOR OZONE DEPLETING AND EPA-17 CHEMICALS
ALTERNATE FOR ACTI-THANE WC-100 PAINT
TÍTULO
25/09/1995
25/09/1995
25/09/1995
29/09/1995
01/12/1997
15/11/1997
15/12/1997
20/05/1988
23/02/1998
26/01/1998
15/12/1997
26/01/1998
12/01/1998
15/03/1998
09/03/1998
03/02/1999
28/01/1998
23/09/1999
05/04/2000
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
I
I
I
R
M
I
R
M
I
M
I
I
R
I
I
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
26/01/1998
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
16Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
CSL-1586
CSL-1589
CSL-1591
CSL-1592
CSL-1593
CSL-A1558
DT 72-323
G78-927
G80-1536
G80-787
G81-0823
G82-0276
G82-0755
G83-0950
G83-0997
GS-SL-45
GS-SL-48
GS-SL-56
HSI-45 SIL 1-85
IND-40() SB 5
Nº PUB
ROLLS ROYCE CORP
ROLLS ROYCE
ROLLS ROYCE
ROLLS ROYCE
ROLLS ROYCE
ALLISON ENGINE CO
SEM RAZAO SOCIAL
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
AIRCRAFT BRAKING SYSTEMS CORP.
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
TRL
TRL
TRL
BSC
BSC
BSC
REV
BSC
BSC
BSC
REV
NAT.
0
0
0
0
0
0
000
000
000
1
1
1
000
000
000
2
0
0
0
3
ORDEM
GLA322S030003100
GLA322S030002700
GLA300S030002800
GLA300S030002900
GLA322S030002000
GLA322S020079300
GLA372S800006400
GLA328A780004700
GLA327A980001500
GLA327S800003600
GLA327X810002100
GLA327X820002700
GLA327S820002900
GLA300A830005400
GLA327A830003400
GLA313S030018500
GLA332S020012300
GLA300A020000400
GLA334S880004500
GLA334A910005800
FADT
NEW SPRING FOR USE IN FUEL NOZZLE ASSEMBLIES
" WARRANTY POLICY GT-8545 (B) DATED 5/00 ".
"SHIPMENT OF FUEL SIYTEM COMPONENTS".
"VISUAL COLOR CHANGE OF 3RD-STAGE TURBINE BLADE, P/N 6875243".
'SPARE PART WARRANTY RETURN PROCESS".
"EXTREME OVERTEMPERATURE OPERATION".
MOTORES ALLISON 501-D13 - REDUTOR - APLICACAO DE BANHODE CROMO E ABERTURA DE UM FURO PARA...
CAPACITANCE TYPE FUEL QUANTITY TEST SET
CABLE MATERIAL CHANGE
HERCULES TRIM TAB POSITION TRANSMITTER PROBLEMS
MOLDED PHENOLIC CABLE - PULLEYS
C-130 AILERON BOOSTER ACTUATOR
CABLE MATERIAL CHANGE
HERCULES OPERATORS USAGE FORM
WING FLAP CARRIAGE ATTACH BOLTS
"REPLACEMENT OF NAS1601 AND NAS1602 PREFORMED PACKINGS".
EXTENSION OF SHELF OF BUNA-NBASED BEARING SEALS AND GREASE RETAINER BAFFLES
EFFECT OF CHEMICAL DISINFECTANTS ON WHEEL & BRAKE COMPONENTS
DME DISPLAY LAMP IMPROVEMENT
COMPATIBILITY WITH 860E-3
TÍTULO
17/05/2000
08/02/2001
25/11/2001
03/12/2001
01/02/2002
26/07/1995
18/12/1969
22/06/1978
25/11/1980
30/05/1980
03/06/1981
12/03/1982
27/05/1982
22/08/1983
25/08/1983
23/06/1997
15/06/1998
22/03/2001
08/11/1985
29/08/1989
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
I
R
I
I
I
R
R
R
I
I
I
I
R
I
I
I
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
18/12/1969
22/06/1978
25/11/1980
30/05/1980
03/06/1981
12/03/1982
27/05/1982
22/08/1983
25/08/1983
28/03/2003
20/08/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
17Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
IT GL00-149 C-130 55
IT GL00-149 C-130 55
IT GL09-199 C-130 61
IT GL09-200 C-130 62
IT GL09-202 C-130 63
IT GL82 C-130 01
IT GL83 C-130 002
IT GL84 C-130 02
IT GL85 C-130 05
IT GL85 C-130 06
IT GL85 C-130 06
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
NAT.
0
0
0
0
0
0
000
1
0
0
1
ORDEM
GLA300A010000000
GLA300A010000001
GLA334A090002200
GLA361A090002500
GLA376S090002700
GLA323S820010600
GLA372S830010700
GLA305A940005201
GLA300A850010100
GLTT00A860000300
GLA351A860009801
FADT
4/5 DME TRANSCEIVER
COLETA, ANÁLISE E PROCEDIMENTOS DE FILTRAGEM DE FLUÍDO HIDRÁULICO
COLETA, ANÁLISE E PROCEDIMENTOS DE FILTRAGEM DE FLUÍDO HIDRÁULICO
ESTABELECER PROCEDIMENTOS A SEREM ADOTADOS QUANTO A INSTALAÇÃO DAS CARENAGENS DEPROTEÇÃO NOS PLUGS INERCIAISDAS ANV C-130 K-130
PROCEDIMENTOS A SEREM ADOTADOS QUANTO A INSTALAÇÃODE CARENAGEM DE PROTEÇÃO DOSPLUGS DO HF AERONAVES C-130/KC-130
ESTABELECER OS PROCEDIMENTOSPARA O TESTE DE SENSIBILIDADE DOS SENSORES ÓTICOS PARA CONTRAMEDIDA (OSC) PN 3313-AS-700-1...
SUBSTITUICAO DE UM DOS SISTEMAS ADF DA AERONAVE C-130 POR UM SISTEMA DF-206
TBO DOS FUEL NOZZLES, DOS MOTORES T56A-7B
ESTABELECER PRAZOS PARA INSPECOES DE CORROSAO EM AREAS CRITICAS; ESPECIALMENTE NA AREA DO PISO, DAS AERONAVES DO PROJETO C-130.
UTILIZACAO DO PRODUTO "QUARTREX SLIP" NAS AERONAVES C-130
EMITIR PROCEDIMENTOS PARA INSPECAO NO MECANISMO DE ALIJAMENTO DOS BOTES. ESTA REVISAO CANCELA TOTALMENTE AIT BASICA DE 23 DEZ 85.
EMITIR PROCEDIMENTOS PARA INSPECAO NO MECANISMO DE ALIJAMENTO DOS BOTES. ESTA REVISAO CANCELA TOTALMENTE A
TÍTULO
20/07/2000
20/07/2000
17/03/2009
17/03/2009
03/07/2009
11/11/1982
08/06/1983
31/12/1984
14/08/1985
23/12/1985
23/12/1985
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
R
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
08/06/1983
22/11/1994
30/06/1986
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
18Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
IT GL85 C-130 06
IT GL86 C-130 07
IT GL86 C-130 08
IT GL86 C-130 10
IT GL86 C-130 11
IT GL87 C-130 12
IT GL87 C-130 13
IT GL87 C-130 14
IT GL88 C-130 17
IT GL88-003 C-130 19
IT GL88-005 C-130 01
IT GL88-006 C-130 02
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
REV
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
1
0
3
0
0
0
0
0
0
0
0
0
ORDEM
GLA357A860000103
GLA332A860010200
GLA300A100000500
GLA332A860009900
GLA336S860010000
GLA372S870004600
GLA334S870004300
GLA328A870004200
GLA361S880009500
GLA361S880011100
GLTT25A880000500
GLA329S880000201
FADT
IT BASICA DE 23 DEZ 85.
EMITIR PROCEDIMENTOS PARA INSPECAO NO MECANISMO DE ALIJAMENTO DOS BOTES. ESTA REVISAO CANCELA TOTALMENTE AIT BASICA DE 23 DEZ 85.
PROCEDIMENTO PARA CONTROLE DOS CONJUNTOS DE FREIO PN 9560685 E PN 9550071 APL NASANVS C-130E E H
ESTABELECER PROCEDIMENTOS DELAVAGEM DE COMPRESSORES APLICADOS NOS MOTORES T56-A-7B, T56-A-15 E T56-A-15LFE DA FAB.
ORIENTACAO P/USO DE DISPOSITIVO PARA BLOQUEIO DOS DISCOS PN 9531109 EM RELACAO AO "PLATE" ..
MODIFICACAO NA PECA PN DL1326M11 (ACTUATOR GTC DOOR)
OTIMIZAR O APOIO AOS OPERADORES DE ANV C-130 QUANTO AO FORNECIMENTO DE MOTORES T56A-7B E 15
AVALIACAO EXPERIMENTAL DO MOD.INTRODUZIDA NO SISTEMA OMEGA
ESTABELECER PROCEDIMENTO DE INSP.E MAINT.MANGUEIRAS REVO. KC-130
APLICACAO DOS CONJUNTOS DE LUVAS ESTACIONARIA E ROTATIVA...
ESTABELECER PROCEDIMENTO COMO CIRCUITO DO SYNCROPHASER DAS AERONAVES C-130 EM MANUTENCAO, CARREGAMENTO E/OU ABASTECIMENTO
CORRECAO NO POSICIONAMENTO DOS BANCOS E CINTOS DE SEGURANCA NO LADO DIREITO DOCOMPARTIMENTO DE CARGA.
ESTABELECER PRAZOS PARA O
TÍTULO
23/12/1985
07/07/1986
05/12/1986
11/09/1986
26/11/1986
15/05/1987
01/07/1987
16/12/1987
18/07/1988
23/08/1988
30/08/1988
31/08/1988
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
R
M
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/06/1986
12/03/2010
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
19Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
IT GL88-006 C-130 02
IT GL88-006 C-130 02
IT GL88-009 C-130 03
IT GL88-010 C-130 04
IT GL88-011 C-130 05
IT GL89-006 C-130 01
IT GL89-006 C-130 01
IT GL89-011 C-130 02
IT GL90-004 C-130 01
IT GL91-001 C-130 01
IT GL91-012 C-130 03
IT GL91-019 C-130 04
IT GL93 006 C-130 03
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
0
8
9
0
0
0
0
0
0
ORDEM
GLA332S880008400
GLA332S880009300
GLA300A880009600
GLA372S880008300
GLA311A880009700
GLA300A950007401
GLA300S980003301
GLA332A890011300
GLA300S900030902
GLA331A910000101
GLA361A910014100
GLA372A910014200
GLA372S930004300
FADT
CUMPRIMENTO DO CARTAO 1-095,DATADO DE 01 JUN 85.
ESTABELECER PRAZOS PARA O CUMPRIMENTO DO CARTAO 1-095,DATADO DE 01 JUN 85.
ESTABELECER PRAZOS PARA O CUMPRIMENTO DO CARTAO 1-095,DATADO DE 01 JUN 85.
ORIENTAR AS UNIDADES AEREAS E AS LINHAS DE REVISOES DO PAMAGL QUANTO A SELECAO DE MATERIAL...
MODIFICAR OS PROCEDIMENTOS PARA AS INSPECOES ESTRUTURAIS DO POWER PACKAGE(Q.E.C.)...
INSTALACAO DE ADESIVOS COM PROCEDIMENTOS PARA SITUACOESDE EMERGENCIA
ITENS CONTROLADOS
ITENS CONTROLADOS
ESTABELECER PROCEDIMENTOS PARA VERIFICAR A FIXACAO DOSPINOS TRAVAS E BUCHAS DOS TRENS DE POUSO PRINCIPAIS.
ESTABELECER PROCEDIMENTOS A SEREM ADOTADOS QUANDO DA MOVIMENTACAO DE ITENS CONTROLADOS.
INSTALAR O ALTITUDE DIGITIZER PN D120-P2-T NAS AERONABES DE MATRICULA, 2466E 2467 E PADRONIZAR COM O RESTO DA FROTA.
ESTABELECER PROCEDIMENTO COMOS QUEBRA CIRCUITOS DO "SYNCROPHASER"...
ESTABELECER PROCEDIMENTOS COM O QUEBRA CIRCUITO DOS "OIL COOLER FLAPS IND"...
ESCLARECER DUVIDAS QUANTO AOEMPREGO DAS REGUAS PN 6795880 E PN6899932 NO
TÍTULO
31/08/1988
31/08/1988
02/09/1988
25/10/1988
16/11/1988
27/07/1989
27/07/1989
31/10/1989
12/09/1990
08/01/1991
08/10/1991
31/10/1991
31/12/1993
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/02/1995
30/06/1998
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
20Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
IT GL93-002 C-130 02
IT GL93-003 C-130 01
IT GL93-007 C-130 04
IT GL93-108 C-130 36
IT GL94-109 C-130 37
IT GL94-110 C-130 38
IT GL94-111 C-130 39
IT GL94-112 C-130 40
IT GL95-121 C-130 44
IT GL95-122 C-130 045
IT GL95-123 C-130 46
IT GL95-124 C-130 47
IT GL95-126 C-130 48
Nº PUB
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
PAMAGL
FABRICANTE
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
1
0
0
0
0
0
000
0
0
ORDEM
GLA361S930003900
GLA300S930003700
GLA372X930004000
GLA338A930004200
GLA361S940005301
GLA329A940005500
GLA324S940005600
GLA300A940005400
GLA329A950007500
GLA383S950007695
GLA332A950007700
GLA327A950000202
GLA328A950000900
FADT
CALCULO DA PERFORMANCE DOS MOTORES ALLISON T56-A-7B
CORRIGIR EVENTUAIS ANORMALIDADES NO CIRCUITO DO"SWITCH" DE 86 DO "VALVE HOUSING".
ORIENTAR UNIDADES AEREAS QUANTO AO ENVIO DE REL. DE MATERIAL...
EVITAR QUE MOTORES ALLISON MODELOS T56-A-7B E T56-A-15...
INSTALAR O MICTORIO PN DGL3-0083 NA ESTACAO FS245.
REALIZAR INSPECAO INTERMEDIARIA NAS HELICES, NAS PUMP HOUSING,...
INSPECIONAR POR RAIOS-X O PN354648-1 ALAVANCA DO LEME DO...
PADRONIZAR AS ROSCAS NA CARCACA DO GERADOR PN 31220-004 COM A...
ESTABELECER OS PROCEDIMENTOSA SEREM ADOTADOS QUANDO DA ESTOCAGEM DAS AERONAVES.
ESTABELECER OS PROCEDIMENTOSDE ABASTECIMENTO DE OLEO HIDRAULICO NOS SISTEMAS...
ESTABELECER PROCEDIMENTOS DEREMESSA DE DADOS DE PERFORMANCE DOS MOTORES ALLISON.
DETERMINAR INSPECAO HOLOGRAFICA PARA OS PNEUS QUE TENHAM SOFRIDO UMA DECOLAGEM...
DETERMINAR A SUBSTITUICAO DOS PARAFUSOS PN:NAS517-4-5,UTILIZADOS NO TUBO DE TORQUEDOS PROFUNDORES DAS ANV C-130.
LIMITAR O NUMERO DE REVISOESSOFRIDAS PELOS PROBES DO SISTEMA DE INDICACAO DE
TÍTULO
06/04/1993
31/03/1993
08/07/1993
06/12/1993
31/01/1994
25/02/1994
08/04/1994
28/09/1994
16/01/1995
09/03/1995
28/03/1995
03/04/1995
30/06/1995
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
O
M
M
M
M
M
M
M
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
28/11/1994
28/03/1995
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
21Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
IT GL95-127 C-130 49
MMSRBB 051278
MSG 2685
MSG R221743Z
PMT C-130H-91
PS210/2009
PTD C-130H-12
PTD C-130H-18
PTD C-130H-8
R011300Z
R031415Z
R040158Z
R060522Z
R060830Z
R061600Z
R111355Z
Nº PUB
PAMAGL
USAF
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
USAF
AGUSTA S.P.A
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
AGUSTA S.P.A
AGUSTA S.P.A
AGUSTA S.P.A
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
ALT
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
000
0
0
000
C1
1
1
000
0
000
000
000
0
000
ORDEM
GLA361S950000600
GLA332A790008600
GLA371S820004000
GLA300S040003600
GLA300A020017000
GLA373S800006600
GLA334A020016700
GLA334A020017300
GLA300A020017100
GLA326A890001000
GLA361S970001200
GLA305A970005900
GLA354A940000900
GLA332A970005700
GLA332A970005800
GLA328A900001100
FADT
COMBUSTIVEL DA AERONAVE C-130.
ESTABELECER PROCEDIMENTOS EMCASO DE PERDA DE OLEO OU GRAXA PELO "ARM BORES"...
PROPOSED C-130 CLASS IVA MODIFICATION OF OXYGEN REGULATOR SUPPORT
ALL OPERATORS OF HERCULES AIRPLANES
T56 SIII AND IV INTERNATIONAL COMPONENT IMPROVEMENT PROGRAM
SOSTITUZIONE VHF COMM AN/ARC-134 CON VHF COMM ART-151
ENGINE COORDINATOR THROTTLE GIMBAL YOKE, CLAMP BOLT
"SOSTITUZIONE IMPIANTO I.F.F. TRA-62A CON N 2 SISTEMI SIT-421T"
SOSTITUZIONE IMPIANTO MB-51Z4; G/S 51V-4 VOR 101 CON 2 IMPIANTI RADIONAVEGAZIONE ANV141
SOSTITUZIONE IMPIANTO ADF AD-370B CON ADF ARG 80A
MAINTENANCE ADVISORY, C-130 AIRCRAFT
C-130 INTERMEDIATE PROP CONTROL LINKAGE
C130 AIRCRAFT PREFLIGHT VALIDITY PERIOD
TRUSS MOUNT UNINSPECTABILITYAND NDI ANOMALLY PROCEDURES , REF WR-ALC/LBL 201600Z
C-130 MAIN LANDING GEAR (MLG) STRUT SERVICING
MAINTENANCE ADVISORY FOR C130 NOSE LANDING GEAR ACTUATOR ROD END INSPECTION CRITERIA
RETRANSMITAL OF DEVIATIONS FOR INSTALLATION OF OUTER FUEL TANK VENT VALVES C-130
TÍTULO
11/10/1995
12/04/1979
06/01/1982
01/09/2003
27/03/1990
12/03/1980
29/05/1996
12/06/1996
18/01/1996
01/12/1988
01/06/1996
01/02/1997
01/06/1994
01/03/1997
01/08/1996
01/12/1989
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
I
I
I
M
I
M
M
M
R
R
R
R
R
R
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
06/01/1982
12/03/1980
10/05/1999
22/06/1996
18/10/1996
01/12/1988
01/02/1997
01/06/1994
01/03/1997
01/12/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
22Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
R140633Z
R160109Z
R171550Z
R191800Z
R231130Z
R240328Z
R241230Z
R270917Z
SB 012-0255-105
SB 104
SB 106
SB 107
SB 108
SB 108
SB 113
SB 2723
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
HONEYWELL INTERNATIONAL INC
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
BOEING
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
REV
BSC
BSC
BSC
NAT.
000
000
0
0
000
000
000
000
1
000
000
B
A
000
000
000
ORDEM
GLA370S970003200
GLA370S970003600
GLA352A970004200
GLA326A940001000
GLA324A900001500
GLA307A970005600
GLA372S890005300
GLA324S800001500
GLA334S030009200
GLA380S970002800
GLA380S970003400
GLA380S970003300
GLA380S970002600
GLA380S970003500
GLA380S970003100
GLA373S900005500
FADT
T56-15 ENGINE PERFORMANCE
MAINTENANCE ADVISORY ON C-130 ENGINE OPERATION
C-130 AIRCRAFT MAINTENANCE ADVISORY
C-130 MAINTENANCE ADVISORY -INSPECTION OF R/H FIRE EXTINGUISHER TUBE FOR CHAFING.
C-130 TCG PROJECT NUMBER TCG-90-002;LOCKHEED SERVICE BULLETIN NO. L89H2800, ALL MODELS, C-130 AIRCRAFT, TIMECOMPLIANCE TECHNICAL
C130 AIRCRAFT MAINTENANCE ADVISORY
C-130 INSPECTION OF ENGINE TRUSS MOUNTS
C-130 ENGINE OIL COOLER DOORACTUATOR, NSN 1680-01-329-7411, P/N 880T100-3
NAVIGATION-AIR DATA COMPUTER-INSTALL OPTIONAL DIFFERENTIAL PRESSURE TRANSDUCER
STAKING PROCEDURE FOR PLANETARY GEAR STUD THREAD
REPLACEMENT OF OIL SEAL ASSEMBLY
ELECTRIC E FLUID POWER DIVISION, THE BENDIX CORPORATION
REPLACEMENT OF OIL SEAL ASSEMBLY,PN,WITH,OIL SEAL PN.
REPLACEMENT OF OIL SEAL ASSEMBLY,PN,WITH,OIL SEAL PN.
DRY SUMP TEST STAND INSTALLATION FOR LYCOMING OPPOSED SERIES ENGINES.
ELECTRO-PNEUMATIC CABIN PRESSURE CONTROL SYSTEM MODIFICATION
TÍTULO
01/04/1997
01/12/1996
01/06/1997
01/09/1994
23/01/1990
01/01/1997
24/08/1989
01/01/1997
09/08/2002
01/01/1973
01/01/1992
01/01/1992
11/10/1974
11/10/1974
02/02/1976
24/05/1968
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
M
M
R
I
R
M
R
R
R
M
M
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/04/1997
01/12/1996
23/01/1990
01/01/1997
24/08/1989
01/01/1997
01/11/2002
01/01/1973
01/01/1992
01/01/1992
07/04/1975
11/10/1974
02/02/1976
24/05/1968
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
23Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 2723
SB 2846
SB 2CM353-24-01
SB 32-4
SB 3213722-21-1270
SB 34-617 (08)
SB 34-72R-94
SB 382-081
SB 38E73-80-124A
SB 51RV-4/()-34-A25
SB 51RV-4/()-34-A25
SB 51RV-4/4()-34-21
SB 51RV-4/4()-34-21
SB 51RV-4/4B/4D-34-27
SB 51RV-4/4B/4D-34-29
SB 51RV-4/4B/4D-34-32
SB 51Y-7/7A/7C/7D-34-19
Nº PUB
BOEING
BOEING
GE AIRCRAFT ENGINES
CONSULTAR CODEMP 001KK
HONEYWELL INTERNATIONAL INC
GE AVIATION BISHOPS CLEEVE CHELTENHAM
LITTON SYSTEMS INC.
LOCKHEED GEORGIA COMPANY
PARKER-HANNIFIN CORP
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
FABRICANTE
REV
BSC
REV
BSC
BSC
BSC
REV
BSC
REV
BSC
REV
REV
REV
BSC
REV
BSC
BSC
NAT.
001
000
1
000
000
0
2
0
3
0
1
2
3
0
1
0
0
ORDEM
GLA373S900005601
GLA377A960001400
GLA324S800009301
GLA332S880002300
GLA336A830005500
GLA334S800003400
GLA334X890002402
GLA381A060000100
GLA321S020011200
GLTT34A920006600
GLTT34A920006701
GLA334A900005902
GLA334A890005000
GLA334A950003500
GLA334A950003401
GLA334A950003300
GLA334A890004800
FADT
ELECTRO-PNEUMATIC CABIN PRESSURE CONTROL SYSTEM MODIFICATION
ENGINE OIL PRESSURE INDICATOR REPLACEMENT
MODIFICATION TO PRODUCT-IMPROVED CONFIGURATION 2CM353C1K AND 2CM353CIL
PISTON INSULATOR REPLACEMENTFOR BRAKE ASSEMBLY
AIR CONDITIONING - THREE-INCH DIAMETER FLUID PRESSUREREGULATING VALVE - REWORK VALVE
NAVIGATION - COUNTER POINTERALTIMETERS INTRODUCTION OF ANEW BAROCALE COUNTER
LTN-72/LTN-72R/RL NAV. SYS.MODIFY CIRCUIT CARDS BY HUM SEAL COATING.
STARTING-REVISION OF ENGINE STARTING SYSTEM
AIR TURBINE CONTROL VALVE - PRESSURE RISE RATE ADJUSTMENT
REDUCE BEARING DRIFT
REDUCE BEARING DRIFT
NAVIGATION - IMPROVED HUMIDITY PERFORMANCE
NAVIGATION - IMPROVED HUMIDITY PERFORMANCE
NAVIGATION - REPLACEMENT OF OBSOLETE PART FOR U431 ON CARD A4
NAVIGATION - REPLACEMENT OBSOLETE PART FOR U515 ON CARD A5
NAVIGATION - REPLACEMENT OF OBSOLETE PART FOR U808 ON CARD A8
NAVIGATION - REPLACEMENT FOROBSOLETE A4CR1
TÍTULO
24/05/1968
17/06/1969
01/05/1979
15/09/1987
16/10/1981
01/10/1978
26/04/1986
30/04/1970
20/03/1989
21/12/1991
21/12/1991
10/08/1983
10/08/1983
29/08/1994
29/08/1994
29/08/1994
15/04/1988
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
O
R
M
R
R
R
M
M
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
23/03/1973
17/06/1969
15/05/1979
15/09/1987
16/10/1981
28/01/1987
24/04/1995
06/01/1992
30/07/1985
27/03/1989
26/09/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
24Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 51Y-7/7A/7C/7D-34-20
SB 51Y-7/7A/7C/7D-34-22
SB 54H60-61-127
SB 54H60-61-140
SB 54H60-61-143
SB 54H60-61-146
SB 54H60-61-147
SB 54H60-61-149
SB 54H60-61-150
SB 54H60-61-153
SB 54H60-61-88
SB 54H60-61-88
SB 562C-5()-22-45
SB 61-100
SB 61-101
SB 61-102
Nº PUB
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATIONDBAAUXILARY POWER
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
UNITED TECHNOLGIES CORP HAMILTON STD DIV
UNITED TECHNOLGIES CORP HAMILTON STD DIV
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
ROCKWELL COLLINS, INC.!DBA
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
FABRICANTE
BSC
BSC
BSC
REV
REV
BSC
REV
BSC
REV
BSC
REV
REV
BSC
BSC
REV
BSC
NAT.
0
0
0
1
1
0
2
0
1
0
4
5
000
000
001
0
ORDEM
GLA334A900005800
GLA334A910005500
GLA361S020011600
GLA361A020005800
GLA361S020070400
GLA361S020004900
GLA361S020070500
GLA361S040018700
GLA361S020010900
GLA361S070003100
GLA361S020070700
GLA361S040010400
GLA322S940002900
GLA361S040007100
GLA361S820002501
GLA361S820002300
FADT
NAVIGATION - REPLACEMENT OF OBSOLETE PART FOR A4U1, A4U2, A4U4 AND A7U3
NAVIGATION - REPLACEMENT OF OBSOLETE PART FOR A4U1, A4U2, A4U4 AND A7U3
PROPELEERS - PITCHLOCK REGULATOR NEW 4 HOLE CONFIGURATION ORIFICE CUP
PROPELLERS - REPAIR OF BARREL SUPPORT RING - PN 514767 AND PN 557058
PROPELLERS - BLADE SEGMENT GEAR TO VENT GEAR TOOTH FRACTURE
PROPELLERS - BARKEL ASSEMBLY- CHANGE PROPELLER SERIAL NUMBER MARKED OU BARREL ASSEMBLY HALVES
PROPELLERS-BLADE SEGMENT GEAR INSPECTION OF BLADE SEGMENT GEAR TOOTH FRACTURE
PROPELLERS-BLADES INCORPORATION OF NEW WATER BASED POLYURETHANE TIP PAINT
PROPELLERS-BARREL ASSEMBLY-NEW SPLIT LINE SEAL
PROPELLERS - BARRIEL ASSEMBLY - CORRECT BLADE SEAL ORIENTATION MARKING
PROPELLERS - BARREL - INSPECTION AND REPAIR OF REAR BARREL BOLTS LUGS
PROPELLERS - BARREL - INSPECTION AND REPAIR OF REAR BARREL BOLTS LUGS
REDUCE INTERMITTENT AUTOPILOT DISENGAGEMENT
PROPELLER LOW PITCH STOP ASSEMBLY - INTRODUCTION OF PISTON STOP LEVER SET.
PROPELLER CONTROL REWORK OF OIL LEVEL INDICATOR.
PROPELLERS - BLADES REPLACEMENT OF BLADE
TÍTULO
06/09/1989
15/01/1991
15/01/1999
10/11/1998
07/05/1999
16/11/1999
15/09/2000
25/05/2001
07/08/2001
12/03/2007
14/10/1977
14/10/1977
21/10/1993
04/05/1981
26/08/1981
30/07/1981
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
O
R
M
R
M
I
M
M
M
M
O
I
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/05/1999
21/02/2002
05/03/2002
26/09/2001
28/02/2002
13/10/2003
21/10/1993
04/05/1981
15/10/1981
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
25Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 61-102
SB 61-113
SB 61-114
SB 61-117
SB 61-118
SB 61-118
SB 61-126
SB 61-128
SB 61-52
SB 61-52
SB 61-52
SB 61-52
Nº PUB
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
BSC
NAT.
0
000
000
000
0
0
000
0
1
2
000
000
ORDEM
GLA361S820002400
GLA361S840003500
GLA361S840003900
GLA361S870000900
GLTT00X980020500
GLTT00X980020501
GLTT61S090000100
GLA361S910002400
GLA361S030052300
GLA361S030052400
GLA361S840003800
GLA361S030024000
FADT
ALIGNMENT GAGE LOCATING PLATES
PROPELLERS - BLADES REPLACEMENT OF BLADE ALIGNMENT GAGE LOCATING PLATES
PROPELLERS - DOME ASSY - REMOVAL OF ANODIZED SURFACE FROM DOME SHELL
PROPELLERS CONTROL - INSPECTION AND REPAIR OF FRONT COVER
PROPELLERS - AFTER BODY INSTALLATION OF BUSHING IN AFTERBODY MOUTING BRACKET
PROPELLERS - PROPELLERS BLADES - INSPECTION FOR ELETRICAL BURNS.
PROPELLERS - PROPELLERS BLADES - INSPECTION FOR ELETRICAL BURNS.
PROPELLER CONTROL - VALVE HOUSING ASSEMBLY - INCORP. OF NEW SPRING FOR FEATHERINGSOLENOIDE VALVE.
PROPELLER CONTROL - PUMP HOUSING ASSEMBLY - INSPECTION OF CONTROL LUG TORQUE RETAINER.
PROPELLER FRONT SPINNER - INSTALLATION OF FRICTION REDUCTION STRIP ON FRONT BULK HEAD.
PROPELLER FRONT SPINNER - INSTALLATION OF FRICTION REDUCTION STRIP ON FRONT BULK HEAD.
PROPELLER FRONT SPINNER - INSTALLATION OF FRICTION REDUCTION STRIP ON FRONT BULK HEAD.
PROPELLER FRONT SPINNER - INSTALLATION OF FRICTION REDUCTION STRIP ON FRONT BULK HEAD.
TÍTULO
30/07/1981
05/01/1984
18/01/1984
30/08/1986
15/01/1986
15/01/1986
15/11/1990
15/02/1991
14/09/1984
14/09/1984
01/07/1971
14/09/1984
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
M
M
M
M
M
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
05/01/1984
18/01/1984
30/08/1986
15/11/1990
04/02/1985
15/12/1985
01/07/1971
14/09/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
26Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 61-54
SB 61-56
SB 61-58
SB 61-64
SB 61-65
SB 61-66
SB 61-70
SB 61-73
SB 61-73
SB 61-75
SB 61-84
SB 61-85
SB 61-86
Nº PUB
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
LITTON SYSTEMS INC.
LITTON SYSTEMS INC.
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
FABRICANTE
REV
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
BSC
BSC
NAT.
1
000
000
000
000
000
000
1
000
000
1
000
000
ORDEM
GLA361S830003301
GLA361S810002000
GLA361S780001300
GLA361S780001200
GLA361S810002700
GLA361S840004000
GLA361S810002600
GLA361X790003301
GLA361S810003700
GLA361S810002500
GLA361S840004101
GLA361S810002400
GLA361S810002200
FADT
PROPELLERS - BLADE ASSEMBLIES - INCORPORATION OF BLADE PLUG WITH PREFORMEDPACKING.
INCORPORATION OF MATCHED SETS OF FLUID TRANSFER SLEEVES IN PROPELLER CONTROLS.
INCORPORATION OF RULON BEARING STRIP IN SLEEVE AND IDLER GEAR ASSEMBLY OF PROPELLER CONTROL.
SPINNER INTERFERENCE - INSPECTION FOR AND REMOVAL OF
PROPELLER BARREL STUB ARM SHOTPEEN REMOVAL.
PROPELLERS - BETA AND SPEED SETTING LEVER SUPORT-PIN STAKING.
PROPELLER IMPROVED BONDING OF RUBBER SEALS.
PROPELLERS - PITCHLOCK REGULATOR ASSEMBLY - INSPECTION OF PITCHLOCK HOUSING AND FLUID TRANSFER HOUSING EXTENSION SLEEVE
PROPELLERS - PITCHLOCK REGULATOR ASSEMBLY - INSPECTION OF PITCHLOCK HOUSING AND FLUID TRANSFER HOUSING EXTENSION SLEEVE
PROPELLERS - BARREL, REPAIR OF PITCHLOCK REGULATOR RETAINING THREADS.
PROPELLERS - BLADE AND SPINNER - IMPROVED BONDING OF RUBBER PARTS.
AIRCRAFT PROPELLER CONTROL -REVERSE ANGLE ADJUSTMENT PROCEDURE AND STOP LEVER MODIFICATION.
PROPELLER - LOW PITCH STOP ASSEMBLY PREFORMED PACKING WEAR.
TÍTULO
17/11/1971
22/11/1971
02/03/1972
25/05/1973
10/12/1973
10/12/1974
18/06/1975
01/04/1981
01/04/1981
23/04/1976
07/12/1977
23/03/1977
15/07/1977
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
I
R
R
R
M
R
R
I
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/12/1982
22/11/1971
02/03/1972
25/05/1973
10/12/1973
10/12/1974
18/06/1975
01/04/1981
01/04/1981
23/04/1976
26/06/1979
23/03/1977
15/07/1977
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
27Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 61-89
SB 61-93
SB 61-94
SB 61-95
SB 61-99
SB 61-A103
SB 61-A124
SB 61-A49
SB 61-A71
SB 61-A71
SB 61-A73
SB 61-A73
SB 618M-3/3A-23-29
SB 618M-3/3A-23-32
SB 618T-2-23-23
Nº PUB
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
ROCKWELL COLLINS, INC.!DBA
ROCKWELL INT. CORP COLLINS GENERALAVIATION COSTA
ROCKWELL COLLINS, INC.!DBA
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
REV
REV
BSC
BSC
BSC
REV
NAT.
000
000
000
0
000
000
001
1
0
1
1
000
0
0
4
ORDEM
GLA361S800003700
GLA361S840004200
GLA361S840004300
GLA361S820003000
GLA361S810002900
GLA361S810002800
GLA361S880002401
GLA361S040007200
GLA361S850001700
GLA361S850001601
GLA361S040007400
GLA361S040007300
GLA323S870002100
GLA323A940002800
GLA323S780003504
FADT
PROPELLER - SYNCROPHASER CONTROL.
PROPELLERS - BLADE INSPECTION AFTER FAIRING INSTALLATION.
PROPELLERS - LOW PITCH STOP ASSEMBLY - INCORPORATION OF SEAL RING.
PROPELLERS - CONTROL REPLACEMENT OF OIL LEVEL INDICATOR ASSEMBLY ON PUMP HOUSING ASSEMBLY ON PUMP HOUSING ASEMBLY.
PROPELLER - SPINNER AND ANTI-ICING ASSEMBLY - IMPROVED AFTERBODY RETENTION.
PROPELLER - BLADE - INSPECTION OF LEADING EDGE FOR EROSION AND CORROSION
PROPELLER CONTROL - INSPECTION REPLACEMENT OF BRANCH ELECTRICAL CABLE ASSEMBLY SPIRAL WRAPPER.
PROPELLER - CONTROL - QUILL,BALLSCREW INSPECTION EMB 120.
PROPELLER CONTROLS CHECK FORFREDOM OF THE BETA FEEDBACK.
PROPELLER CONTROLS CHECK FORFREDOM OF THE BETA FEEDBACK.
PROPELLERS - PITCHLOCK REGULATOR ASSEMBLY INSPECTION OF FLUIDE HOUSINGEXTENSION SLEEVE.
PROPELLERS - PITCHLOCK REGULATOR ASSEMBLY INSPECTION OF FLUIDE HOUSINGEXTENSION SLEEVE.
INCREASED MODULATION ADJUST RANGE
IMPROVED REABILITY OF MODULATOR
REDUCTION OF INTERNAL SIGNALS
TÍTULO
15/01/1979
27/05/1980
15/06/1980
15/10/1980
01/04/1981
29/07/1981
18/05/1988
07/05/1991
28/07/1975
28/07/1975
19/12/1975
19/12/1975
07/02/1987
17/06/1993
15/09/1970
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
O
R
R
O
R
R
M
R
I
I
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/01/1979
27/05/1980
15/06/1980
01/04/1981
29/07/1981
01/06/1988
20/05/1991
08/08/1975
02/01/1976
19/12/1975
17/08/1977
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
28Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 618T-2/3-23-35
SB 618T-2/3-23-35
SB 628T-2-23-01
SB 628T-2-23-03
SB 628T-2-23-08
SB 628T-2-23-09
SB 628T-2-23-09
SB 628T-2-23-11
SB 628T-2-23-13
SB 66039/-01/29-192
SB 82-121
SB 82-134
SB 82-178
SB 82-178
SB 82-200A
SB 82-200A
SB 82-204
SB 82-216A
SB 82-230
Nº PUB
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ABEX CORP AEROSPACE DIV
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA
FABRICANTE
REV
BSC
BSC
REV
REV
REV
BSC
BSC
REV
BSC
BSC
REV
BSC
REV
BSC
REV
BSC
REV
BSC
NAT.
1
0
000
1
1
1
000
000
1
000
0
A
000
001
0
A
000
A
0
ORDEM
GLA323S780003701
GLA323S780003600
GLA323S890007000
GLA323S910007101
GLA323S910006901
GLA323S890006901
GLA323S890007300
GLA323S910007000
GLTT23S920008101
GLA329A910008300
GLA327A840001000
GLA327A840001100
GLA327A840001200
GLA327A030024400
GLA328A840010500
GLA328A840010601
GLTT49A920007300
GLA372S840008301
GLA357A910001100
FADT
ELIMINATE SPIKE WHEN POWER IS TURNED ON
ELIMINATE SPIKE WHEN POWER IS TURNED ON
HF RECEIVER - TRANSMITTER
IMPROVE 5V POWER SUPPLY FREQUENCY CONTROL
IMPROVE COAX CONTACT AND REDUCE POSSIBLE COIL SHORTS
RECEIVER PROTECTION FROM HIGH LEVEL RF ENERGY
RECEIVER PROTECTION FROM HIGH LEVEL RF ENERGY
REPLACEMENT OF OBSOLETE MECHANICAL FILTER
IMPROVE REABILITY OF LOWER AUDIO OUTPUT IMPEDANCE CIRCUIT
HYDRAULIC POWER-ENGINE DRIVEPUMP-REPLACE THERMAL ACTUATOR
FLIGHT CONTROLS-REVERSAL OF BOLTS IN THE ELEVATOR AND RUDDER CONTOL SYSTEM.
CONTROLS - REPLACEMENT OF ELEVATOR TRIM TAB RELAY
CONTROLS - INSPECTION AND REWORK OF ELEVATOR TRIM TAB ACTUATOR ROD-END BEARINGS
CONTROLS - INSPECTION AND REWORK OF ELEVATOR TRIM TAB ACTUATOR ROD-END BEARINGS
FUEL - MODIFICATION OF FUEL QUANTITY INDICATING SYSTEM
FUEL - MODIFICATION OF FUEL QUANTITY INDICATING SYSTEM
AIRBORNE AUXILIARY POWER-INSPECTION OF OVERSPEED TRIPASSEMBLY MONTING SCREWS
ELECTRICAL POWER - INSTALLATION OF ENGINE GROUND START INTERLOCK
ELECTRICAL POWER -
TÍTULO
02/01/1975
02/01/1975
09/10/1984
25/10/1985
12/10/1988
23/03/1989
23/03/1989
19/12/1990
01/03/1991
05/01/1990
26/01/1966
15/06/1966
16/08/1967
16/08/1967
02/04/1968
02/04/1968
29/03/1968
30/09/1969
16/10/1968
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
R
R
R
M
R
R
R
R
R
R
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
06/06/1977
09/10/1984
12/07/1989
11/07/1989
13/07/1989
23/03/1989
19/12/1990
28/03/1991
05/01/1990
08/08/1967
16/08/1967
22/12/1967
01/06/1970
29/03/1968
26/02/1970
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
29Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-230
SB 82-231
SB 82-242
SB 82-246A
SB 82-249
SB 82-255
SB 82-262
SB 82-263
SB 82-263
SB 82-263
SB 82-268
SB 82-268
SB 82-268
SB 82-269
Nº PUB
LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
BSC
BSC
REV
BSC
BSC
REV
REV
REV
BSC
REV
SPL
BSC
BSC
NAT.
A
000
000
001
000
000
A
A
B
000
A
A
000
000
ORDEM
GLA357A040007500
GLTT32S920000900
GLA332S840003300
GLTT57A920006401
GLA324A800001300
GLA332S830002900
GLA329A840002100
GLA332S030025600
GLA332X980000500
GLA332S030025500
GLA330A840021101
GLA330A840021202
GLA330A840002500
GLA323A840000400
FADT
INSPECTION AND RELOCATION OFWIRE HARNESS CLAMPS ON WING FRONT BEAM AT CWS 135
ELECTRICAL POWER - INSPECTION AND RELOCATION OFWIRE HARNESS CLAMPS ON WING FRONT BEAM AT CWS 135
LANDING GEAR - REWORK OF NLGDRAG STRUT ACTUATOR LOCKING KEY
LANDING GEAR - IMPROVEMENT IN NOSE GEAR FREE FALL CAPABILITY
WING - UPPER SURFACE CENTER WING-CENTER LINE ACCESS OPENING REPAIR
ELECTRICAL - ENGINE DRIVEN GENERATOR - INSTALLATION OF SANDWICH TYPE DISCONNECT
LANDING GEAR - REPLACEMENT OF NOSE LADING GEAR FIXED KEY WITH AN ADJUSTABLE KEY
HYDRAULIC POWER - MODIFICATION OF HYDRAULIC SUCTION BOOS PUMP CIRCUIT
LANDING GEAR-IMPROVMENT OF MLG PISTON NUT RESTRAINT
LANDING GEAR-IMPROVMENT OF MLG PISTON NUT RESTRAINT
LANDING GEAR-IMPROVMENT OF MLG PISTON NUT RESTRAINT
ICE AND RAIN PROTECTION - REPLACEMENT OF BLEED AIR DUCT COUPLING, NOSE WHEEL WELL
ICE AND RAIN PROTECTION - REPLACEMENT OF BLEED AIR DUCT COUPLING, NOSE WHEEL WELL
ICE AND RAIN PROTECTION - REPLACEMENT OF BLEED AIR DUCT COUPLING, NOSE WHEEL WELL
COMUNICATIONS - REPLACEMENT OF STATIC DISCHARGERS
TÍTULO
16/10/1968
05/11/1968
10/04/1969
06/05/1969
06/09/1970
30/01/1970
01/10/1970
08/06/1970
08/06/1970
08/06/1970
09/12/1970
09/12/1970
09/12/1970
31/12/1970
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
O
R
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/08/1969
05/11/1968
10/04/1969
29/06/1970
06/09/1970
30/01/1970
25/05/1972
16/09/1970
13/03/1972
08/06/1970
27/03/1974
27/03/1974
09/12/1970
31/12/1970
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
30Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-271
SB 82-274
SB 82-274
SB 82-282
SB 82-288
SB 82-297
SB 82-298
SB 82-302
SB 82-304
SB 82-306
SB 82-307
SB 82-308
SB 82-315
SB 82-316
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA
FABRICANTE
BSC
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
NAT.
000
000
001
000
000
000
000
000
000
0
000
000
000
002
ORDEM
GLA327A810000800
GLA372S030025800
GLA372S820004100
GLA357A800006100
GLA332S800002800
GLA332S800003200
GLTT57A770002800
GLA327A790000800
GLA327A800001600
GLA352A800007000
GLA353A780003100
GLA328A800002300
GLA327A790000900
GLA327A800007702
FADT
FLIGHT CONTROLS - RUDDER ANDAILERON SYSTEMS - REMOVAL OFREDUNDANT RELIEF
POWER PLANT - MODIFICATION OF BREATHER VENT PLUMBING TOFACILITATE REMOVAL OF QEC COOLER DUCT
POWER PLANT - MODIFICATION OF BREATHER VENT PLUMBING TOFACILITATE REMOVAL OF QEC COOLER DUCT
FLIGHT CONTROLS - INSTALLATION OF EXTENDED LIFE WING FLAP JACKISCREW
INSPECTION AND REWORK OF NOSE LANDING GEAR STRUT TO REMOVE CORROSION.
LANDING GEAR - INSTALLATION OF MAIN LANDING GEAR SOFT STRUT
WING - FLAPPER VALVE INSTALLATION OUTR WING DRY BAY REAR BEAM
FLIGHT CONTROL - INSPECTION OF RUDDER ATTACH POINT BEARINGS P/N MS20200KP10
FLIGHT CONTROLS - INSTALLATION OF RUDDER HINGESUPPORT ASSEMBLY BEARING RETAINER
DOORS - INSTALLATION OF IMPROVED RAMP LATCH ACTUATORFITTING
STRUCTURES - INSPECTION OF MLG BEAMS TO WING DRAG ANGLEFOR LOOSE, SHEARED OR MISSING FASTENERS
FUEL - GROUNDING OF FUEL QUANTITY INDICATOR COAXIAL SHIELD
FLIGHT CONTROL - INSPECTION AND REPLACEMENT OF FASTENERSIN THE ELEVATOR TORQUE COLLAR ASSEMBLY
FLIGHT CONTROLS -
TÍTULO
31/12/1970
29/01/1971
29/01/1971
18/01/1971
28/07/1971
22/09/1972
19/04/1974
29/11/1971
15/08/1972
08/05/1972
31/07/1972
26/06/1972
16/10/1972
15/09/1972
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
O
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/12/1970
29/01/1971
29/06/1981
18/01/1971
28/07/1971
22/09/1972
19/04/1974
29/11/1971
15/08/1972
31/07/1972
26/06/1972
16/10/1972
02/02/1976
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
31Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-317
SB 82-318
SB 82-320
SB 82-320
SB 82-320
SB 82-320
SB 82-323
SB 82-324
SB 82-331
SB 82-333
SB 82-333
SB 82-334
SB 82-336
SB 82-336
Nº PUB
LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
REV
REV
REV
REV
BSC
BSC
BSC
REV
BSC
RVC
BSC
BSC
NAT.
000
000
1
2
3
4
0
0
000
1
000
2
000
000
ORDEM
GLA324A780000600
GLTT55A770001300
GLA320A970007188
GLA357A030013100
GLA357A030013200
GLA357A910005904
GLA327A020033100
GLTT32S920001100
GLA361S780001401
GLA332S800003301
GLA332A030025900
GLA329A090001100
GLA380S970001500
GLA380S970002700
FADT
REPLACEMENT OF FASTENERS, WING FLAP DRIVE INSTALLATION
ELECTRICAL POWER - RETERMINATION OF POWER RELAYGROUND WIRE TO PREVENT AC INSTRUMENT AND ENGINE FUEL CONTROL BUS TRANSFER DELAY
STABILIZER - INSTALLATION OFCLIP BRACKETS ON HORIZONTAL STABILIZER LEADING EDGE FORMER
WING - OUTER WING LOWER SURFACE FATIGUE PREVENT/REPAIR KIT
WING - OUTER WING LOWER SURFACE FATIGUE PREVENT/REPAIR KIT
WING - OUTER WING LOWER SURFACE FATIGUE PREVENT/REPAIR KIT
WING - OUTER WING LOWER SURFACE FATIGUE PREVENT/REPAIR KIT
FLIGHT CONTROSL - INSPECTIONOF AILERON HING BRACKET BOLTHOLES
LANDING GEAR-INSTALLATION OFMLG TRACK SHOES WITH SLIPON FACES.
PROPELLERS - INSPECTION FOR,AND REMOVAL OF SPINNER INTERFERENCE
LADING GEAR - REPLACEMENT OFMLG BUNGEE CORDS WITH CHAINS
LADING GEAR - REPLACEMENT OFMLG BUNGEE CORDS WITH CHAINS
HYDRAULIC POWER - INSTALLATION OF MPEV3-032-2 AUXILIARY HYDRAULIC PUMP
STARTING - STAKING OF PLANETARY GEAR STUD FOR BENDIX STARTERS
STARTING - STAKING OF PLANETARY GEAR STUD FOR BENDIX STARTERS
TÍTULO
12/10/1972
22/01/1973
27/06/1974
27/06/1974
27/06/1974
27/06/1974
28/02/1973
10/08/1973
25/05/1973
31/01/1974
31/01/1974
23/04/1976
14/12/1973
14/12/1973
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
O
R
M
M
M
M
M
R
R
R
R
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
12/10/1972
22/01/1973
01/08/1974
04/11/1974
16/01/1987
25/04/1988
25/05/1973
07/02/1975
31/01/1974
29/01/2009
14/12/1973
14/12/1973
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
32Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-344
SB 82-344
SB 82-349
SB 82-361
SB 82-361
SB 82-367
SB 82-368
SB 82-370
SB 82-370
SB 82-370
SB 82-370
SB 82-373
SB 82-376
SB 82-379
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
BSC
BSC
REV
BSC
BSC
BSC
REV
REV
BSC
ERT
BSC
BSC
BSC
NAT.
3
000
0
1
000
000
0
2
3
000
N
000
000
000
ORDEM
GLA353A790004203
GLA353A030026000
GLA355A800004200
GLA328A800008001
GLA328A800002200
GLTT53A770003300
GLA324A020029400
GLA376A790000202
GLA376A820000603
GLTT76A760000200
GLA376A830000800
GLTT36A770003200
GLA324A780000700
GLTT25A770000300
FADT
FUSELAGE - INSPECTION OF FS 597 PORK CHOP FITTING
FUSELAGE - INSPECTION OF FS 597 PORK CHOP FITTING
STABILIZER - INSPECTION OF REAR FUSELAGE/HORIZONTAL STABILIZER JOINT AND REPLACEMENT OF HARDWARE
FUEL - OUTBOARD FUEL TANK VENT VALVE INSTALLATION IMPROVEMENT
FUEL - OUTBOARD FUEL TANK VENT VALVE INSTALLATION IMPROVEMENT
FUSELAGE - MODIFICATION OF LONGERON, LOWER LEFT-HAND FUSELAGE, F.S. 165 TO 245
ELECTRICAL POWER - INSPECTION AND ADJUSTMENT OFPN B-123J HARTMAN CONTACTOR
ENGINE CONTROLS - INSTALLATION OF LARGER DIAMETER THROTTLE CABLE PULLEYS
ENGINE CONTROLS - INSTALLATION OF LARGER DIAMETER THROTTLE CABLE PULLEYS
ENGINE CONTROLS - INSTALLATION OF LARGER DIAMETER THROTTLE CABLE PULLEYS
ENGINE CONTROLS - INSTALLATION OF LARGER DIAMETER THROTTLE CABLE PULLEYS
AIR CONDITIONING - REMOVAL OF REFRIGERATION UNITS SPEEDLIMIT CONTROL ORIFICES
ELECTRICAL - ENGINE DRIVEN GENERATOR - INSTALLATION OF SANDWICH TYPE DISCONNECT (BRAZIL)
STRUCTURE - MODIFICATION OF PARATROOP STATIC LINE ANCHOR
TÍTULO
11/10/1974
11/10/1974
18/06/1975
18/04/1975
18/04/1975
06/02/1976
30/04/1975
04/11/1977
14/11/1977
14/11/1977
14/11/1977
29/04/1977
21/12/1976
25/05/1976
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
M
R
R
R
R
R
O
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/02/1979
11/10/1974
12/06/1975
18/04/1975
06/02/1976
11/04/1979
25/11/1981
14/11/1977
18/04/1983
29/04/1977
21/12/1976
25/05/1976
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
33Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-380
SB 82-381
SB 82-381
SB 82-381
SB 82-382
SB 82-388
SB 82-389
SB 82-390
SB 82-394
SB 82-410
SB 82-411
SB 82-412
SB 82-416
SB 82-420
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
000
000
002
003
000
000
000
000
0
000
000
0
000
000
ORDEM
GLA332S790002200
GLA357A030026100
GLA357A030026200
GLA357A800006503
GLA328A810006900
GLTT57A920006900
GLTT32A760000300
GLA352A780002900
GLA332A840012700
GLA354A860001900
GLA332S840002900
GLTT27A770003600
GLTT00X980020800
GLA336A780000200
FADT
CABLE SUPPORT
LADING GEAR - WIRING CIRCUITRY REVISION
WING - FATIGUE PREVENT INSTALLATION AT OWS35, KINGPIN STIFFENER AREA
WING - FATIGUE PREVENT INSTALLATION AT OWS35, KINGPIN STIFFENER AREA
WING - FATIGUE PREVENT INSTALLATION AT OWS35, KINGPIN STIFFENER AREA
FUEL-INSPECTION FOR MISSING CLAMPS IN NO. 4 DRAY BAY OWS162.78
WING - INSPECTION/REPLACEMENT OF COUNTERSUNK SCREWS IN OUTER WING LOWER SURFACE
LANDING GEAR - INSPECTION OFHORIZONTAL AND VERTICAL MLG TORQUE SHAFTS
FUSELAGE - SEALING OF AFT ENTRY DOOR LOWER SILL
LANDING GEAR - INSTALLATION OF HYTROL MARK II ANTI-SKID SYSTEM AND MULTI-DISC BREAKES
POWER PLANT - REINFORCEMENT OF ENGINE MOUNT AFT TRUSS DIAGONAL BRACE LUGS
LANDING GEAR - INSTALLATION OF IMPROVED NOSE GEAR STRUT AND COMPONENTS
FLIGHT CONTROLS - INSPECTIONOF ELEVATOR TRIM TAB CONTROLSWITCHES
PROPELLER - INSPECTION OF LOW PITCH STOP QUAD RING PREFORMED PACKING AND PISTONSLEEVE
AIR CONDITIONING - MODIFCATION OF BLEED AIR PRESSURE REGULATOR CIRCUIT
TÍTULO
23/04/1976
30/01/1976
30/01/1976
30/01/1976
26/03/1976
05/06/1976
09/04/1976
12/05/1978
07/03/1977
03/03/1978
17/03/1978
15/07/1977
05/07/1977
12/05/1978
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
R
R
R
R
R
R
R
R
M
R
M
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
23/04/1976
30/01/1976
31/08/1976
21/05/1980
26/03/1976
05/06/1976
09/04/1976
12/05/1978
03/03/1978
17/03/1978
05/07/1977
12/05/1978
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
34Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-421
SB 82-428
SB 82-439
SB 82-446
SB 82-448
SB 82-450
SB 82-451
SB 82-451
SB 82-452
SB 82-455
SB 82-458
SB 82-461
SB 82-462
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
REV
BSC
BSC
REV
BSC
REV
BSC
BSC
BSC
REV
BSC
BSC
NAT.
000
001
0
000
1
0
1
000
0
000
1
000
000
ORDEM
GLTT32S770000600
GLA327A020010300
GLA376A790003400
GLA332X830002801
GLTT32A960014300
GLA329A800002500
GLA357A810004101
GLA357A030026500
GLA329A800002600
GLA371S800003900
GLA354A810003001
GLA355A800004300
GLA395A800000200
FADT
LANDING GEAR - INSPECTION AND MODIFICATION OF MAIN LANDING GEAR EXTENSION/RETRACTION MECHANISM HORIZONTAL TORQUE SHAFTS
MAINTENANCE CHECKS - INSPECTION FOR CORROSION IN AIRCRAFT CABLES
ENGINE CONTROLS - INSPECTIONOF THROTTLE CABLE FOR INTERFERENCE BETWEEN CABLE AND ADJACENT BOLT HEAD
LANDING GEAR - REPLACEMENT OR MODIFICATION OF MLG SWIVEL BRACKETS
LANDING GEAR - INSPECTION AND REWORK OF NLG STRUT TO REMOVE CORROSION
HYDRAULIC POWER - INSPECTIONFOR INTERFERENCE BETWEEN AUXILIARY HYDRAULIC LINES AND 10,00 POUND TIEDOWN FITTINGS
WING - INSPECTION OF CENTER-TO-OUTER WING ATTACHMENT BOLTS FOR CRACKS
WING - INSPECTION OF CENTER-TO-OUTER WING ATTACHMENT BOLTS FOR CRACKS
HYDRAULIC POWER-INSPECTION FOR AND REPLACEMENT OF CERTAIN RESTRICTORS IN THE AIRCRAFT HYDRAULIC SYSTEM
POWER PLANT - MODIFICATION OF ENGINE RELAY BOX MOUNTING ATTACHMENTS
NACELLES/PYLONS - INSPECTIONOF ENGINE MOUNT BOLTS FOR CRACKS
STABILIZERS - INSPECTION OF VERTICAL STABILIZER FORWARD ATTACH BLOCK
EQUIPMENT/FURNISHINGS - MODIFICATION OF EMERGENCY
TÍTULO
06/10/1977
09/05/1978
11/04/1979
19/12/1980
05/09/1979
12/10/1979
21/08/1979
21/08/1979
28/11/1979
10/05/1980
09/04/1980
23/04/1980
24/03/1980
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
R
R
M
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
06/10/1977
10/01/1979
19/12/1980
03/11/1989
08/06/1981
21/08/1979
10/05/1980
30/04/1981
23/04/1980
24/03/1980
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
35Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-465
SB 82-466
SB 82-466
SB 82-467
SB 82-468
SB 82-470
SB 82-471
SB 82-476
SB 82-484
SB 82-485
SB 82-487
SB 82-493
SB 82-493
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
NAT.
000
1
000
000
000
0
0
0
0
000
000
1
000
ORDEM
GLA332X800002700
GLA353A840010001
GLA353A810004600
GLA332S800003000
GLA361S800000300
GLA332A800003100
GLA329A820001400
GLA353A810004500
GLA332S810002300
GLA335A820005100
GLA332S820001900
GLA330A820001701
GLA330A820001500
FADT
ESCAPE ROPE
LANDING GEAR - INSTALLATION OF IMPROVED MLG DOWN POSITION VISUAL INDICATOR
FUSELAGE-REINFORCEMENT MIDIFICATION OF FAIRING ATTACHMENT FLANGESAT FS477 AND FS617
FUSELAGE-REINFORCEMENT MIDIFICATION OF FAIRING ATTACHMENT FLANGESAT FS477 AND FS617
LANDING GEAR - REPLACEMENT OF KEYS ON MLG BALL SCREW
ICE AND RAIN PROTECTION - INSPECTION OF PROPELLER SPINNER ANTI-ICING SYSTEM WIRE BUNDLES
LANDING GEAR - INSTALLATION OF MLG SPLASH GUARD
HYDRAULIC POWER - INSTALLATION OF SNUBBERS TO PROTECT HYDRAULIC SYSTEM PRESSURE SWITCHES AND GAGES
FUSELAGE - REPLACEMENT OF MLG TRACK FASTENERS
LANDING GEAR - INSPECTIUON AND MODIFICATION OF MAIN LANDING GEAR EXTENSION/RETRACTION MECHANISM VERTICAL TORQUE SHAFTS
OXYGEN - INSTALLATION OF IMPROVED OXYGEN SUPPLY LINE EMERGENCY SHUTOFF VALVE
LANDING GEAR - REPLACEMENT OF PINS IN CALCO BALLSCREWS
ICE AND RAIN PROTECTION - REVISION OF PROPELLER ANTI-ICING/DE-ICING AMMETER INSTRUMENT RANGE MARKINGS
ICE AND RAIN PROTECTION - REVISION OF PROPELLER ANTI-ICING/DE-ICING AMMETER INSTRUMENT RANGE MARKINGS
TÍTULO
24/06/1980
13/01/1981
13/01/1981
02/10/1980
15/08/1980
26/08/1980
30/10/1981
23/01/1981
03/04/1981
10/07/1981
01/07/1981
11/09/1981
11/09/1981
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
O
O
R
M
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
24/06/1980
07/12/1983
13/01/1981
02/10/1980
15/08/1980
10/07/1981
01/07/1981
12/05/1982
11/09/1981
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
36Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-495
SB 82-497
SB 82-499
SB 82-501
SB 82-501
SB 82-504
SB 82-505
SB 82-505
SB 82-506
SB 82-506
SB 82-509
SB 82-510
SB 82-510
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
BSC
BSC
SPL
BSC
BSC
ERT
BSC
ERT
BSC
BSC
ERT
NAT.
000
000
000
0
NOT
000
0
001
0
0
000
0
0
ORDEM
GLA324A840000500
GLA327A820001300
GLA324A820005800
GLA357A030013300
GLA357A830004001
GLA327A830001700
GLA324A830001200
GLA324A030013500
GLA327A830001800
GLA327A830005700
GLA327A830001900
GLTT27A830000300
GLA327A030013600
FADT
ELECTRICAL - POWER -INSTALLATION OF IMPROVED AC BUS OFF WARNING RELAY
FLIGHT CONTROLS - INSPECTIONAND RETORQUE OF ELEVATOR TRIM TAB JACKSCREW ATTACHINGBOLT AND NUT
ELECTRICAL POWER - MODIFICATION OF RUDDER, AILERON, AND ELEVATOR BOOST AND UTILITY COTOFF VALVE CONNECTOR WIRING
WING - INSPECTION AND REPLACEMENT OF OUTER WING RIB DIAGONAL BRACES
WING - INSPECTION AND REPLACEMENT OF OUTER WING RIB DIAGONAL BRACES
FLIGHT CONTROLS - REPLACEMENTE AND SERVICING OF RUDDER THRUST BEARING
ELECTRICAL POWER - REPLACEMENTE OF 35 AMP CIRCUIT BREAKRS WITH IMPROVED CIRCUIT BREAKERS
ELECTRICAL POWER - REPLACEMENTE OF 35 AMP CIRCUIT BREAKRS WITH IMPROVED CIRCUIT BREAKERS
FLIGHT CONTROLS - INSPECTIONOF RUDDER PEDAL ADJUSTER RETAINING NUTS
FLIGHT CONTROLS - INSPECTIONOF RUDDER PEDAL ADJUSTER RETAINING NUTS
FLIGHT CONTROLS - INSPECTIONAND TEST OF ELEVATOR CONTROLTENSION REGULATOR FOR BINDING
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
TÍTULO
03/02/1982
01/02/1982
13/11/1981
02/03/1982
02/03/1982
03/11/1982
17/11/1982
17/11/1982
16/08/1982
16/08/1982
26/10/1982
27/04/1983
27/04/1983
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
R
R
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
03/02/1982
01/02/1982
13/11/1981
15/03/1982
03/11/1982
17/11/1982
08/10/1982
26/10/1982
17/04/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
37Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-510
SB 82-510
SB 82-510
SB 82-510
SB 82-512
SB 82-515
SB 82-520
SB 82-520
SB 82-522
SB 82-523
SB 82-524
SB 82-524
SB 82-529
SB 82-531
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA
FABRICANTE
REV
REV
REV
REV
BSC
BSC
REV
REV
BSC
BSC
REV
BSC
BSC
BSC
NAT.
1
2
3
4
0
000
2
3
000
000
1
000
0
000
ORDEM
GLA327A030013700
GLA327A030013800
GLA327A030013900
GLA327A900008204
GLA328A830002300
GLA327A830002000
GLTT00X980021100
GLA354A850001803
GLA353A830000200
GLA328A830002400
GLA329A030014000
GLA329A840002200
GLA325A830001600
GLA335A830000300
FADT
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
FLIGHT CONTROLS. RETROFIT INSTALLATION OF SELF RETAINING FASTENERS
FUEL - MODIFICATION OF PYLONTANK SURGE BOX TO PREVENT FUEL PROBE INTERFERENCE
FLIGHT CONTROLS - INSPECTIONOF AILERON BOOSTER ACTUATOR ASSEMBLY
WING - INSPECTION OF EXTERNAL FUEL TANK PYLON STRUCTURE ASSEMBLY MOUNTING BOLT HOLES
WING - INSPECTION OF EXTERNAL FUEL TANK PYLON STRUCTURE ASSEMBLY MOUNTING BOLT HOLES
FUSELAGE - INSPECTION OF FS 737.00 RING SEGMENTS
FUEL - INSTALLATION OF IMPROVED FUEL SYSTEM PREFERRED SPARE DUMP MAST
HYDRAULIC POWER - REPLACEMENT OF RUDDER UTILITY PRESSURE TUBE ASSEMBLY WITH FLEXIBLE HOSE
HYDRAULIC POWER - REPLACEMENT OF RUDDER UTILITY PRESSURE TUBE ASSEMBLY WITH FLEXIBLE HOSE
EQUIPMENT/FURNISHINGS - INSPECTION FOR ENGINE AIR INTAKE SHIELD P/N 3402250 AND REMOVAL OF STOWAGE RETAINING FASTENERS
OXYGEN - INSPECTION AND
TÍTULO
27/04/1983
27/04/1983
27/04/1983
27/04/1983
28/02/1983
22/12/1982
30/09/1982
30/09/1982
12/04/1983
13/05/1983
06/05/1983
06/05/1983
06/06/1983
04/04/1983
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
M
R
R
M
M
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/03/1985
21/05/1987
14/12/1987
24/07/1989
22/12/1982
25/05/1983
25/10/1985
12/04/1983
13/05/1983
15/03/1984
06/05/1983
04/04/1983
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
38Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-532
SB 82-533
SB 82-535
SB 82-535
SB 82-538
SB 82-539
SB 82-540
SB 82-540
SB 82-540
SB 82-549
SB 82-553
SB 82-553
Nº PUB
LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
BSC
ERT
BSC
BSC
REV
REV
BSC
BSC
BSC
ERT
NAT.
0
000
000
S/N
0
0
1
2
000
0
000
000
ORDEM
GLA329A830002500
GLA324A830001300
GLA326A840001400
GLA326A030051500
GLA352A840009400
GLA329A840002300
GLA329A030049800
GLA329A030049900
GLA329A840000201
GLA324A840000800
GLA332S850001001
GLA332A030054200
FADT
REPLACEMENT OF LIQUID OXYGENSYSTEM SUPPLY LINE EMERGENCYSHUTOFF VALVE
HYDRAULIC POWER - REMOVAL OFAFT CARGO DOOR HYDRAULIC ACTUATOR BLEED VALVE
ELECTRICAL POWER - MODIFICATION OF MAIN AC BUS OFF INDICATOR RELAY WIRING
FIRE PROTECTION - INSPECTIONAND TEST OF FIRE EXTINGUISHER SYSTEM
FIRE PROTECTION - INSPECTIONAND TEST OF FIRE EXTINGUISHER SYSTEM
DOORS - INSTALATION OF IMPROVED OVERHEAD EMERGENCY EXIT DOOR RELEASE MECHANISM
HYDRAULIC POWER - INSPECTIONOF HYDRAULIC LINES IN WHELL POD AREA FOR POSSIBLE CHAFING.
HYDRAULIC POWER - INSTALLATION OF CHECK VALVESIN AILERON HYDRAULIC SYSTEM RETURN LINES
HYDRAULIC POWER - INSTALLATION OF CHECK VALVESIN AILERON HYDRAULIC SYSTEM RETURN LINES
HYDRAULIC POWER - INSTALLATION OF CHECK VALVESIN AILERON HYDRAULIC SYSTEM RETURN LINES
EQUIPMENT/FURNISHINGS - INSPECTION OF CARGO COMPARTMENT INSULATION BLANKETS FOR SECURITY AND CLEARANCE
LANDING GEAR - INSPECTION OFNLG DRAG STRUT ACTUATING CYLINDER ASSEMBLY
LANDING GEAR - INSPECTION OFNLG DRAG STRUT ACTUATING CYLINDER ASSEMBLY
TÍTULO
09/09/1983
20/09/1983
24/06/1983
24/06/1983
10/02/1984
10/02/1984
27/03/1984
27/03/1984
27/03/1984
02/10/1984
24/08/1984
24/08/1984
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
M
R
R
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
20/09/1983
24/06/1983
09/09/1983
01/10/1984
09/10/1990
27/03/1984
24/08/1984
20/12/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
39Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-560
SB 82-564
SB 82-566
SB 82-568
SB 82-568
SB 82-573
SB 82-573
SB 82-574
SB 82-574
SB 82-575
SB 82-577
SB 82-582
SB 82-583
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
BSC
REV
BSC
REV
BSC
REV
REV
BSC
BSC
BSC
REV
NAT.
000
000
000
1
000
1
000
4
4
000
000
000
001
ORDEM
GLA327A850000600
GLA376S850002700
GLA332S850001100
GLA328A030054300
GLA328A850000900
GLA353A970006401
GLA353A860000600
GLA332A030010700
GLA332A030010700
GLA327A860000700
GLA361S860001800
GLA311A860000300
GLA332A880002101
FADT
FLIGHT CONTROLS - INSPECTIONOF AILERON BOOSTER ACTUATINGLEVER
ENGINE CONTROLS - INSPECTIONOF ENGINE CONTROL ARM ASSEMBLY FOR CORROSION
LANDING GEAR - INSPECTION OFMLG BRAKE HOSE RESTRAINT CHAIN END CLAMPS
FUEL - INSPECTION OF OUTBOARD FUEL TANK VENT PLUMBING FOR CLAMPS WITH TEFLON INSERTS
FUEL - INSPECTION OF OUTBOARD FUEL TANK VENT PLUMBING FOR CLAMPS WITH TEFLON INSERTS
FUSELAGE - INSPECTION FOR INTERFERENCE AND REWORK TO PROVIDE CLEARANCE BETWEEN MLG BEAM AND WING BLEED AIR DUCT ISOLATION VALVE
FUSELAGE - INSPECTION FOR INTERFERENCE AND REWORK TO PROVIDE CLEARANCE BETWEEN MLG BEAM AND WING BLEED AIR DUCT ISOLATION VALVE
LANDING GEAR-INSPECTION OF NLG DRAG STRUT ACTUATOR ROD END.
LANDING GEAR-INSPECTION OF NLG DRAG STRUT ACTUATOR ROD END.
FLIGHT CONTROLS - INSPECTIONOF ELEVATOR CONTROL CABLES FOR CHAFING.
PROPELLER - INSPECTION OF PROPELLER FEATHERING SOLENOID CIRCUITRY GROUNDINGPOINTS
PLACARDS AND MARKINGS - RELOCATION OF EMERGENCY CUTOUT MARKINGS
FUSELAGE - INSPECTION AND REPLACEMENT OF FASTENERS IN
TÍTULO
01/04/1985
08/08/1985
15/02/1985
07/08/1985
07/08/1985
27/01/1986
27/01/1986
12/11/1985
12/11/1985
13/12/1985
06/05/1986
07/02/1986
05/08/1986
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
R
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/04/1985
08/08/1985
15/02/1985
28/02/1986
07/08/1985
29/07/1996
27/01/1986
07/07/2003
07/07/2003
13/12/1985
06/05/1986
07/02/1986
12/10/1987
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
40Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-586
SB 82-587
SB 82-591
SB 82-593
SB 82-597
SB 82-601
SB 82-602
SB 82-605
SB 82-610
SB 82-611
SB 82-615
SB 82-615
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
REV
ERT
REV
NAT.
000
000
000
000
000
000
000
1
000
1
1
001
ORDEM
GLA352A860002700
GLA353A860002900
GLA355A870001000
GLA376A870001500
GLA353A880004400
GLA328A880001300
GLA372S880001400
GLTT27A990049100
GLA376A880001600
GLA327A960001300
GLTT00X960002200
GLA332S970006300
FADT
MLG WHEEL WELL, WL 200 BEAM WEB TO LATERAL STIFFENER
FUSELAGE - INSPECTION AND INSTALLATION OF FASTENERS INAFT CARGO DOOR DOWNLOCK CABLE PULLEY BRACKET SUPPORTCHANNEL
FUSELAGE - INSPECTION OF THEFUSELAGE PRESSURE SKIN FASTENERS AT 245, FS 305E, AND FS 345E
STABILIZERS - INSPECTION OF HORIZONTAL STABILIZER UPPER SURFACE STUMP TYPE LOCKBOLTS
ENGINE CONTROLS - INSPECTIONOF ENGINE THROTTLE CONTROL CABLES AT CERTAIN PULLEY LOCATIONS.
FUSELAGE - ADDITION OF DORSAL FIN DRAINAGE PROVISIONS
AIR - REFUELING - INSPECTIONOF AIR REFUELING SYSTEM HOSEREEL ASSEMBLIES.
POWER PLANT - INSPECTION OF POWER PLANT FRONT MOUNTS FORLOOSENESS AND BOLT TORQUE
FLIGHT CONTROLS-INCORPORATION OF REVISED LOCKING METHOD FOR THE RUDDER BALANCE
MAINTENANCE CHECKS - INSPECTION OF CONTROL PEDESTAL WIRE HARNESSES FOR CHAFING
FLIGHT CONTROLS - REPLACEMENTE OF AILERON CONTROL LINK AND CONTROL RODASSEMBLIES
INSTALLATION OF MLG BALLSCREW TRUNNION LUBRICATION FITTINGS
INSTALLATION OF MLG BALLSCREW TRUNNION LUBRICATION FITTINGS
TÍTULO
31/07/1986
11/07/1986
16/10/1986
17/10/1986
03/06/1987
10/07/1987
21/10/1987
10/11/1987
25/11/1987
03/06/1988
16/05/1988
16/05/1989
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
R
M
M
I
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/07/1986
11/07/1986
16/10/1986
17/10/1986
03/06/1987
10/07/1987
21/10/1987
09/02/1998
25/11/1987
18/07/1990
23/08/1989
14/08/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
41Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-616
SB 82-618
SB 82-627
SB 82-628
SB 82-628
SB 82-630
SB 82-633
SB 82-642
SB 82-652
SB 82-652
SB 82-652
SB 82-654
SB 82-659
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA
FABRICANTE
BSC
BSC
BSC
BSC
ERT
REV
BSC
BSC
REV
REV
REV
BSC
BSC
NAT.
000
0
000
000
000
001
0
000
001
002
003
0
000
ORDEM
GLA376A880003200
GLA326A880001100
GLA353A890000300
GLA311A890000900
GLA311A040007800
GLA353A890005801
GLA371S890000400
GLA324A890000500
GLA349A930001500
GLA349A030053700
GLA349A030053800
GLTT32A920001200
GLA353A910000300
FADT
MAINTENANCE CHECKS - INSPECTION FOR WIRE BUNDLE CHAFING AND INSTALLATION OF CLAMPS IN FLIGHT STATION CONTROL PEDESTAL
FIRE PROTECTION - INSPECTIONOF FIRE EXTINGUISHER TUBE ASSEMBLY P/N 363800-72,FOR CORRECT INSTALLATION
FUSELAGE - INSPECTION OF MLGWHEEL WELL WL 200 LATERAL STIFFENER CHENNEL TO LONGERON FASTENERS
PLACARDS AND MARKINGS - INSTALLATION OF NEW SEATING ARRANGEMENT PLACARDS
PLACARDS AND MARKINGS - INSTALLATION OF NEW SEATING ARRANGEMENT PLACARDS
FUSELAGE - MIL WHEEL WELL SIDE PANEL FASTENERS INSPECTION, BL 61.23, FS 517TO FS 597
POWER PLANT - INSPECTION FORAND REPLACEMENTE OF HYDRAULIC PRESSURE HOSES IN QEC
ELECTRICAL POWER - INSPECTION OF AC-DC PANEL WIRE HARNESS FOR CHAFING ANDMODIFICATION OF CLAMP INSTALLATION
AIRBORNE AUXILIARY POWER - INSTALLATION OF IMPROVED APUFORWARD EXHAUST DUCT BRACKET
AIRBORNE AUXILIARY POWER - INSTALLATION OF IMPROVED APUFORWARD EXHAUST DUCT BRACKET
AIRBORNE AUXILIARY POWER - INSTALLATION OF IMPROVED APUFORWARD EXHAUST DUCT BRACKET
LANDING GEAR - REPLACEMENTE OF MLG BALLSCREW INTERNAL BALL RETURN INSERTS
FUSELAGE CORROSION
TÍTULO
21/12/1987
24/06/1988
13/02/1989
13/01/1989
13/01/1989
19/06/1989
15/06/1989
20/11/1989
11/07/1990
11/07/1990
11/07/1990
18/06/1990
04/10/1990
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
R
M
I
R
R
R
R
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
21/12/1987
13/02/1989
13/01/1989
22/05/1989
10/09/1992
20/11/1989
01/04/1992
17/05/1993
29/06/1993
04/10/1990
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
42Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-662
SB 82-663
SB 82-666
SB 82-667
SB 82-683
SB 82-686
SB 82-689
SB 82-691
SB 82-693
SB 82-693
SB 82-696
SB 82-696
Nº PUB
LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
REV
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
REV
REV
NAT.
000
001
000
000
0
0
0
0
2
3
1
2
ORDEM
GLA324A900000700
GLTT32A920000601
GLA375S910000600
GLA324A910001000
GLA327A930000300
GLA327A950001200
GLA357A950003701
GLA300A970002500
GLA353A020009300
GLA353A020009900
GLA300A970002000
GLA300A970002100
FADT
INSPECTION AND REPAIR,BL 20 LONGERON, FS 245 TO FS 477 AND FS 617 TO FS 737 UPPER
ELECTRICAL POWER - INSPECTION OF EXTERMINAL POWER - INSPECTION OF EXTERNAL POWER RECEPTACLE TERMINAL LUGS.
LANDING GEAR - REPLACEMENT OF MLG EMERGENCY SYSTEMS DECALS
POWER PLANT - INSPECTION ANDREPLACEMENT OF BLEED AIAR SYSTEM AEROQUIP COUPLINGS.
ELECTRICAL POWER - INSPECTION OF LH EXTERNAL FUEL TANK BOOST PUMP HEAD TERMINATIONS.
FLIGHT CONTROLS - INSPECTIONOF AILERON ELEVATOR, AND LIFE RAFT CABLE FAIRLEAD,F.S. 457
FLIGHT CONTROLS REPLACEMENT OF VALVE AND DAMPER SUPPORT BRAKET ON AILERON BOOSTER
POWER PLANT - NONDESTRUCTIVEINSPECTION OF OUTBOARD ENGINE TRUSS MOUNT TANGS
MLG-INSPECTION OF BRAKE CONTROL SYSTEM
FUSELAGE-INSPECTION OF F5737,777E OR 817E FLOOR TO RING BILKHEAD FITTING FOR CRACKS
FUSELAGE-INSPECTION OF F5737,777E OR 817E FLOOR TO RING BILKHEAD FITTING FOR CRACKS
FLIGHT CONTROLS-AILERON AND ELEVATOR BOOSTER ASSEMBLY,BY-PASS MANIFOLD MODIFICATION OF
FLIGHT CONTROLS-AILERON AND ELEVATOR BOOSTER ASSEMBLY,BY-PASS MANIFOLD
TÍTULO
17/10/1990
07/01/1991
10/05/1991
06/08/1991
06/04/1993
18/04/1994
18/03/1994
23/10/1995
15/08/1997
15/08/1997
01/01/1997
23/05/1996
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
R
R
M
M
R
M
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
17/10/1990
25/11/1991
10/05/1991
06/08/1991
28/05/1998
08/09/1999
07/02/1997
09/05/1997
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL GERAL
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
43Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-696
SB 82-696
SB 82-703
SB 82-716
SB 82-716
SB 82-719
SB 82-721
SB 82-723
SB 82-725
SB 82-729
SB 82-730
SB 82-730
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORP!LOCKHEED MARTINAERONAUTICAL S
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
REV
BSC
REV
REV
REV
REV
BSC
REV
BSC
REV
REV
NAT.
000
3
000
3
4
1
1
0
1
0
1
2
ORDEM
GLTT00S970013700
GLTT27A990049700
GLA332A960002097
GLA357A030005300
GLA357A040017901
GLTT76A990045800
GLA353A020010700
GLA321A040017300
GLA300S020003900
GLA352A020003700
GLA300A020003300
GLA353A020003600
FADT
MODIFICATION OF
FLIGHT CONTROLS-AILERON AND ELEVATOR BOOSTER ASSEMBLY,BY-PASS MANIFOLD MODIFICATION OF
FLIGHT CONTROLS-AILERON AND ELEVATOR BOOSTER ASSEMBLY,BY-PASS MANIFOLD MODIFICATION OF
MLG - INSPECTION OF MLG EMERGENCY EXTENSION WRENCH
WINGS-INSPECTION OF RIB FORMER AT OWS 293 LOWER WINGSURFACE FOR CRACKS
WINGS-INSPECTION OF RIB FORMER AT OWS 293 LOWER WINGSURFACE FOR CRACKS
ENGINE CONTROLS-INSPECTION OF ENGINE CONDITION TRANSFERASSEMBLY CLEVIS BOLT
FUSELAGE - INSPECTION FOR SUFFICIENT CLEARANCE BETWEENRAMP ACTUATOR PISTON ROD ANDFASTENER USED
ICE AND RAIN PROTECTION-DE ACTIVATION/REMOVAL OF NOSE RADOME ANTI-ICING SYSTEM, C-130 AIRCRAFT
AIR CONDITIONING - INSPECTION OF C-130 AIRCRAFTFLIGHT DECK AND CARGO COMPARTMENT AUXILIARY VENT VALVES PN 398650-1-1
DOORS-INSPECTION OF UPPER TORQUE TUBE ASSEMBLY OF CREWDOOR
FUSELAGE - INSPECTION OF FS 6970 RING SEGMENT AND ATTACHFITTING FOR MINIMUM EDGE DISTANCE ON LOWER TWO FASTENERS
FUSELAGE - INSPECTION OF FS 6970 RING SEGMENT AND ATTACHFITTING FOR MINIMUM EDGE DISTANCE ON LOWER TWO
TÍTULO
23/05/1996
23/05/1996
11/10/1996
05/09/1997
05/09/1997
09/01/1998
17/01/1999
14/11/1997
18/05/1998
03/06/1999
15/01/1999
15/01/1999
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
I
M
M
M
I
R
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
23/05/1996
16/11/1998
11/10/1996
01/11/2002
24/05/2004
20/10/1998
24/10/2000
01/11/1999
24/08/1999
20/02/2002
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
44Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-733
SB 82-739
SB 82-746
SB 82-749
SB 82-751
SB 82-752
SB 82-752
SB 82-752
SB 82-753
SB 82-755
SB 82-755
SB 82-756
SB 82-759
SB 82-760
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORP!LOCKHEED MARTINAERONAUTICAL S
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
USAF
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
BSC
REV
BSC
BSC
BSC
NAT.
0
0
0
0
0
0
1
4
0
0
1
0
0
0
ORDEM
GLA300A020003000
GLA376A020004300
GLA353A020003501
GLA332A040015700
GLA300A020004400
GLA300A020002600
GLA300A020002700
GLA353A070003201
GLA300A020002900
GLA352A020003400
GLA352A060000200
GLA328S020001100
GLA352A020012400
GLA351A020030500
FADT
FASTENERS
FLIGHT CONTROLS - INSPECTIONOF 359900-3 FLEXIBLE TUBE INCONTROL COLUMN FOR DAMAGE
ENGINE CONTROLS - INSPECTIONOF ENGINE CONDITION LEVER HARDWARE FOR PROPER TORQUE
FUSELAGE - INSPECTION 7 REPAIR OF 362010-6 SKIN LOCATED UNDER AIR CONDITIONING INLET SCOOP FORCORROSION
LANDING GEAR - BRAKE CABLE RIGGING INSPECTION
"EQUIPMENTS/FURNISHINGS - CARGO HANDLING SYSTEM SIDE RAIL BOLT APPLICATION TORQUECERTIFICATION STRIPE".
FUSELAGE - INSPECTION OF WING TO FUSELAGE ATTACH
FUSELAGE - INSPECTION OF WING TO FUSELAGE ATTACH
FUSELAGE - INSPECTION OF WING TO FUSELAGE ATTACH
FLIGHT CONTROLS - INSPECTIONOF AILERON CONTROL CABLE PULLEY
"DOORS - INSPECTION OF C-130CARGO RAMPS FOR IDENTIFICATION AND PROPER INSTALLATION".
"DOORS - INSPECTION OF C-130CARGO RAMPS FOR IDENTIFICATION AND PROPER INSTALLATION".
"SERVICING - PROHIBITION OF USE OF AMS 1428, TYPE II DE-ICING FLUID".
DOORS - REPLACEMENT OF BOLTSIN FITTING OF AFT NOSE GEAR DOOR
"STRUCTURES - INSPECTION ANDREPLACEMENT OF AFT FUSELAGE STRUCTURE FASTENERS AT FS 858, BL 61.6".
TÍTULO
26/04/1999
07/01/2000
15/06/2000
17/08/2000
01/05/2001
17/09/2000
17/09/2000
17/09/2000
17/09/2001
02/02/2002
02/02/2002
14/01/2002
11/04/2002
29/04/2002
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
I
I
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
17/01/2002
01/05/2007
13/02/2006
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
45Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-766
SB 82-766
SB 82-768
SB 82-769
SB 82-769
SB 82-770
SB 82-771
SB 82-773
SB 82-773
SB 82-775
SB 82-778
SB 82-779
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
ERT
BSC
ERT
REV
REV
REV
REV
REV
BSC
BSC
REV
NAT.
0
0
0
1
1
4
3
1
2
0
0
2
ORDEM
GLA357A030029900
GLA357A040014700
GLA357A040000200
GLA327A040014600
GLA327A040006800
GLA328A090000300
GLA357A090001000
GLA346A040012800
GLA328A070000400
GLA324A040015800
GLA371A090001400
GLA332A090000200
FADT
WING - INSPECTION OF CENTER WING LOWER FORWARD CORNER FITTINGS
WING - INSPECTION OF CENTER WING LOWER FORWARD CORNER FITTINGS
WINGS-INSPECTION OF FOR CENTER WING CAPS AND STRINGERS FOR HEAT TREATMENTAND CORROSION
FLIGHT CONTROLS-INSPECTION OF RUDDER AND ELEVATOR COUNTERBALANCE
FLIGHT CONTROLS-INSPECTION OF RUDDER AND ELEVATOR COUNTERBALANCE
FUEL - SFAR 88 DRY ZONAL INSPECTION AND INSPECTION/REPAIR OF STATIC GROUND TERMINALS OF FUEL SYSATEM PLUMBING
WINGS - INSPECTION OF CENTERWING UPPER AND LOWER RAINBOWFITTING FOR CRACKS
FUEL - SFAR 88 - LIGHTNING BONDING JUMPER INSTALLATION
FUEL - SFAR 88 - LIGHTNING BONDING JUMPER INSTALLATION
INSPECTION FOR CHAFFING OF THE ESSENTIAL DC BUS WIRING ( ... ) LOCATED BEHIND THE COPILOT'S SIDE CIRCUIT BREAKER PANEL.
TEFLON HOSES AS AN ALTERNATEFOR ELASTOMERIC (REBBER) HOSES OM POWER PLANT, NACELLE, AND QEC
"LANDING GEAR - ONE-TIME INSPECTION AND REWORK OF THEMAIN LANDING GEAR VERTICAL TORQUE SHAFT QUICK DISCONNECT JOINT SAFETY WIRE".
TÍTULO
02/09/2003
02/09/2003
15/10/2003
15/10/2003
15/10/2003
17/10/2003
07/12/2004
28/01/2004
28/01/2004
22/04/2004
23/01/2005
02/08/2004
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
I
M
I
M
M
M
M
M
M
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
03/05/2004
03/05/2004
17/02/2004
18/09/2008
25/04/2008
28/01/2004
20/11/2006
15/01/2008
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
46Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-781
SB 82-781
SB 82-784
SB 82-786
SB 82-792
SB 82-795
SB 82-795
SB 82-796
SB 82-798
SB 82-800
SB 82-804
SB 82-807
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN AERONAUTICAL
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
ERT
REV
BSC
BSC
ERT
REV
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
1
0
0
0
1
0
0
0
0
0
ORDEM
GLA334A050001600
GLA334A050001700
GLA371A070003300
GLA353A050001000
GLA328A060001600
GLA300A110000200
GLA328A090003601
GLA351A070000500
GLA327A060002200
GLA357A060001700
GLA357A080000700
GLA332S090003200
FADT
INSPECTION AND REWORK OF THEDF301 DIRECTION FINDER ANTENNA.
INSPECTION AND REWORK OF THEDF301 DIRECTION FINDER ANTENNA.
INSPECTION OF ENGINE TRUSS MOUNT FOR CRACKING OF THE DIAGONAL BRACE LUGS WITH PRESS FIT STEEL BUSHING INSTALLED
INSPECTION OF UPPER AFT SECTION OF LEFT AND RIGHT LONGERON AT FS 737.
FUEL- INSPECTION OF INTEGRALFUEL TANKS
"FUEL - SFAR 88 - LIGHTNING PROTECTIONFOR TANKS WITH WALL THICKNESS LESS THAN 0.080 INCH".
"FUEL - SFAR 88 - LIGHTNING PROTECTIONFOR TANKS WITH WALL THICKNESS LESS THAN 0.080 INCH".
STRUCTURES-INSPECTION OF INCORRECT FASTENERS INSTALLED IN LEFT & RIGHT STRUT(PN 385073) ASSEMBLIES AT FS 737
"FLIGHT CONTROLS - ONE-TIME INSPECTION FOR PROPER TORQUEOF ELEVATOR TORQUE TUBE BOLTS".
"WING - MAIN FUEL TANK ACCESS PANELS BOLTS TORQUE LIMITS".
WING - INSPECTION OF WING JOINT BOLTS FOR PROPER PROTRUSION THROUGH THE BARREL NUTS
LANDING GEAR - INSPECTION AND REPLACEMENT OF P/N 3303583-SÉRIES ONE-PIECE NOSE LANDING GEAR ACTUATOR
TÍTULO
02/11/2004
02/11/2004
06/01/2005
21/03/2005
14/02/2006
18/01/2007
18/01/2007
31/10/2006
28/08/2006
17/05/2006
26/09/2007
23/06/2009
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
I
M
M
M
I
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
17/03/2005
28/08/2006
07/01/2008
05/11/2007
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
47Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB 82-807
SB 82-808
SB 82-819
SB 860E-4/5-34-21
SB 860E-4/5-34-23
SB 860E-5-34-25
SB 9000000-34-6024
SB A82-149
SB A82-157
SB A82-181
SB A82-239
SB A82-265
SB A82-295
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN AERONAUTICAL
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
L-3 COMMUNICATIONS AVIONICS SYSTEMS
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
REV
REV
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
1
3
1
000
000
1
1
000
000
000
000
000
000
ORDEM
GLA332S100000300
GLA353A120000300
GLA353A120000500
GLA334A900006102
GLA334A890004900
GLA334A910005601
GLA300A140000100
GLA328A840002000
GLA328A840001800
GLA327A800001800
GLA329A840012600
GLA361S840004600
GLA376A840007600
FADT
ATTACH COLLAR ASSEMBLY
LANDING GEAR - INSPECTION AND REPLACEMENT OF P/N 3303583-SÉRIES ONE-PIECE NOSE LANDING GEAR ACTUATOR ATTACH COLLAR ASSEMBLY
FUSELAGE - REPLACEMENT OF MS21250( ), NAS1104, AND NAS1105 TENSION BOLTS ATTACHING THE MAIN LANDING GEAR VERTICAL BEAM TO THE(...)
FUSELAGE - INSPECTION OF FUSELAGE STATION (FS) 968 BULKHEAD FOR CRACKS
NAVIGATION - TRANSMITTER SPURIOUS OUTPUT SUPPRESSION
NAVIGATION - IMPROVE MODULATOR RELIABILITY
NAVIGATION - REDUCE NUISANCEFUSE FAILURES
NAVIGATION TRAFFIC AND TERRAIN COLLISION AVOIDANCE SYSTEM - T2CAS COMPUTER UNIT...
FUEL SYSTEM - INSPCTION AND REPLACEMENT OF SCREENS IN THE EXTERIOR JETTSON AND VENT MASTS
ELECTRICAL SYSTEM - INSPECTION OF AMPHENOL CONNECTORS, FUEL QUANTITY INDICATING SYSTEM
FLIGHT CONTROLS - INSPECTIONFOR END PLY OF WING FLAP JACKSCREWS
HYDRAULIC POWER - INSPECTIONOF P/N EA-1045-037-1A/2 HYDRAULIC PUMP FOR CORRECT ELECTRICAL GROUND
PROPELLER - INSPECTION OF PROPELLER PISTON DOME ASSEMBLY
ENGINE CONTROL - INSPECTION OF ENGINE THROTTLE CONTROL
TÍTULO
23/06/2009
20/07/2009
27/10/2011
05/05/1987
04/03/1988
15/04/1991
15/11/2011
10/11/1984
03/01/1967
27/04/1967
31/10/1968
14/04/1970
09/09/1971
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
R
R
M
R
R
R
R
M
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
04/01/2010
28/06/2010
03/01/2012
05/05/1987
04/03/1988
19/08/1991
15/03/2013
10/11/1984
03/01/1967
27/04/1967
31/10/1968
14/04/1970
09/09/1971
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL ORGÂNICO/OPER
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
48Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB A82-314
SB A82-328
SB A82-332
SB A82-346
SB A82-374
SB A82-374
SB A82-393
SB A82-393
SB A82-399
SB A82-435
SB A82-441
SB A82-478
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA
FABRICANTE
BSC
BSC
BSC
REV
REV
REV
ERT
BSC
BSC
BSC
BSC
REV
NAT.
0
0
0
8
3
3
0
000
000
0
0
1
ORDEM
GLA361S790003000
GLA327A020032900
GLA334A840015700
GLA357A910000208
GLA353A800007203
GLA353A800007204
GLA327A030014300
GLA327A790001200
GLTT32S770000800
GLA335A790004000
GLA376A790003500
GLA353A810004401
FADT
CABLES
PROPELLERS - INSPECTION OF PROPELLER FLUID HOUSING EXTENSION SLEEVE THREADS
FLIGHT CONTROL - INSPECTION OF AILERON TRIM TAB ACTUATORCONNECTIONS FOR SECURITY
NAVIGATION - INSPECTION OF ADF SENSE ANTENNA PANEL IN CENTER FUSELAGE LOWER PANEL
WING - INSPECTION OF OUTER WING FRONT BEAM LOWER CAP,FRONT BEAM WEB,AND LOWERSURFACE FORWARD SKIN PANEL AT OWS 144 TO OWS 165...
INSPECTION OF MAIN FRAME AT FS517 LEFT AND RIGHT FOR CRACKS AND INSTALLATION OF PREVENT/REPAIR
INSPECTION OF MAIN FRAME AT FS517 LEFT AND RIGHT FOR CRACKS AND INSTALLATION OF PREVENT/REPAIR
FLIGHT CONTROLS-INSPECTION AND REWORK OF RUDDER, AILERON, AND ELEVATOR BOOSTER AND SERVO CONTROL VALVES
FLIGHT CONTROLS-INSPECTION AND REWORK OF RUDDER, AILERON, AND ELEVATOR BOOSTER AND SERVO CONTROL VALVES
LANDING GEAR INSPECTION OF MULTIPLE DISC BRAKES FOR IMPROPER SEALS
MODIFICATION OF OXYGEN REGULATOR SUPORT AND INSPECTION OF OXIGEN PUMBING, RH FWD CARGO COMPARTMENT
INSPECTION OF ENGINE THROTTLE CONTROL CABLES AT CERTAIN PULLEY LOCATIONS.
FUSELAGE - INSPECTION OF
TÍTULO
19/05/1972
23/05/1973
18/07/1973
01/01/1979
22/07/1975
22/07/1975
22/04/1976
22/04/1976
15/09/1976
09/11/1978
20/12/1978
18/02/1981
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
M
M
M
M
R
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
04/04/1988
31/01/1977
31/01/1977
07/05/1976
22/04/1976
15/09/1976
24/04/1981
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
49Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB A82-483
SB A82-483
SB A82-489
SB A82-508
SB A82-508
SB A82-516
SB A82-516
SB A82-519
SB A82-541
SB A82-558
SB A82-572
SB A82-572
SB A82-578
Nº PUB
LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
BSC
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
REV
BSC
REV
NAT.
1
000
000
000
001
2
000
000
000
000
1
000
1
ORDEM
GLA311A810004801
GLA311A810000400
GLA327A810000900
GLA371S820003501
GLA372S040005500
GLA311A860003202
GLA311A820000700
GLA324A820001100
GLA328A840001900
GLA326A840000900
GLA357A030054500
GLA357A850000300
GLA326A030054600
FADT
BL20 LONGERON SPLICE FOR MISLOCATED BOLT HOLES.
MARKINGS - INSPECTION FOR AND REMOVAL OF ABRASIVE STRIPS FROM PARATROOP DOOR OPENING
MARKINGS - INSPECTION FOR AND REMOVAL OF ABRASIVE STRIPS FROM PARATROOP DOOR OPENING
FLIGHT CONTROLS - INSPECTIONOF THE RUDDER BOOSTER ASSY FOR INTERFERENCE BETWEEN TABWASHER AND FEEL LEVER.
POWER PLANT - INSPECTION OF REAR ENGINE MOUNT FOR PROPERSECURITY
POWER PLANT - INSPECTION OF REAR ENGINE MOUNT FOR PROPERSECURITY
FUEL - INSTALLATION OF MAIN FUEL TANK VENTING WARNING DECAL ON SINGLE POINT REFUELING CONTROL PANEL
FUEL - INSTALLATION OF MAIN FUEL TANK VENTING WARNING DECAL ON SINGLE POINT REFUELING CONTROL PANEL
ELECTRICAL - INSPECTION OF OVERHEAD CONTROL PANEL FOR CHAFED WIRE HARNESS.
FUEL-TESTING OF WING TANK SYSTEM CHECK VALVE .
FIRE PROTECTION - INSPECTIONOF FIRE EXTINGUISHER SQUIB
WING - INSPECTION OF OUTER WING LOWER SUFARCE SKIN PANEL KING PIN RISERS FOR CRACKS, OWS 29 TO OWS 35
WING - INSPECTION OF OUTER WING LOWER SUFARCE SKIN PANEL KING PIN RISERS FOR CRACKS, OWS 29 TO OWS 35
FIRE PROTECTION - INSPECTIONOF TURBINE OVERHEAT WARNING
TÍTULO
31/03/1981
31/03/1981
24/04/1981
12/05/1982
12/05/1982
08/06/1982
08/06/1982
25/08/1982
21/02/1983
04/10/1984
27/11/1985
27/11/1985
29/10/1985
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
M
M
M
R
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/04/1981
31/03/1981
24/04/1981
12/05/1982
22/06/1982
20/08/1986
08/06/1982
25/08/1982
21/02/1983
04/10/1984
01/01/1992
27/11/1985
25/04/1986
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
50Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB A82-578
SB A82-581
SB A82-607
SB A82-607
SB A82-607
SB A82-607
SB A82-612
SB A82-612
SB A82-612
SB A82-613
SB A82-635
SB A82-635
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
BSC
ERT
REV
BSC
ERT
BSC
ERT
ERT
BSC
REV
REV
NAT.
000
000
1
1
000
000
0
0
1
000
1
2
ORDEM
GLA326A860000500
GLA353A860002800
GLA357A030054000
GLA357A890005601
GLA357A030053900
GLA357A030054100
GLTT57A870000100
GLTT57A870000200
GLA357A040004400
GLA357A880004000
GLA353A890006401
GLA300A020000600
FADT
SYSTEM WIRING
FIRE PROTECTION - INSPECTIONOF TURBINE OVERHEAT WARNING SYSTEM WIRING
FUSELAGE - INSPECTION AND INSTALLATION OF FASTENERS INFS 93 BULKHEAD AT WL 195,LBL6.75 TO RBL 6.75
WING - EXAMINATION FOR STATUS FOR OUTER WING LOWER SURFACE PANEL RISERS FOR REPAIRS, OWS 0 TOOWS 360.
WING - EXAMINATION FOR STATUS FOR OUTER WING LOWER SURFACE PANEL RISERS FOR REPAIRS, OWS 0 TOOWS 360.
WING - EXAMINATION FOR STATUS FOR OUTER WING LOWER SURFACE PANEL RISERS FOR REPAIRS, OWS 0 TOOWS 360.
WING - EXAMINATION FOR STATUS FOR OUTER WING LOWER SURFACE PANEL RISERS FOR REPAIRS, OWS 0 TOOWS 360.
WING - INSPECTION OF HEAT SHIELD NUTPLATE AND AFT NACELLE FAIRING HOLES, OWS 161 TO OWS 195
WING - INSPECTION OF HEAT SHIELD NUTPLATE AND AFT NACELLE FAIRING HOLES, OWS 161 TO OWS 195
WING - INSPECTION OF HEAT SHIELD NUTPLATE AND AFT NACELLE FAIRING HOLES, OWS 161 TO OWS 195
WING INSPECTION OF OUTER WING DRY BAY LOWER FORWARD BEAM CAP, OWS 144 TO OWS 214
FUSELAGE INSPECTION OF PRESSURIZED FAIRING SUPPORT STRUCTURE, FS 477 TO FS 517,BL 61L TO BL 61R
FUSELAGE INSPECTION OF PRESSURIZED FAIRING SUPPORT
TÍTULO
29/10/1985
18/11/1985
30/11/1987
30/11/1987
30/11/1987
30/11/1987
30/11/1987
30/11/1987
30/11/1987
30/11/1987
28/04/1989
28/04/1989
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
I
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
29/10/1985
18/11/1985
12/08/1988
14/11/1988
30/11/1987
02/05/1988
30/11/1987
25/04/1988
30/11/1987
19/05/1989
13/12/1991
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
51Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB A82-653
SB A82-653
SB A82-684
SB A82-684
SB A82-694
SB A82-694
SB A82-694
SB A82-695
SB A82-700
SB A82-700
SB A82-726
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
NAT.
000
1
1
000
000
000
000
000
0
0
1
ORDEM
GLA353A900000900
GLA353A910000500
GLA326A930000101
GLA326A930000500
GLA300A960000300
GLA332A950000700
GLA332A950000800
GLA300A970001400
GLA376A970004400
GLA376S960000600
GLA352A030012600
FADT
STRUCTURE, FS 477 TO FS 517,BL 61L TO BL 61R
FUSELAGE - INSPECTION OF FORWARD FUSELAGE CABIN UNDERFLOOR BULKHEAD STRUCTURE AT FS 180.5, WL 170,BETWEEN BL 18 TO BL 27,LEFT.....
FUSELAGE - INSPECTION OF FORWARD FUSELAGE CABIN UNDERFLOOR BULKHEAD STRUCTURE AT FS 180.5, WL 170,BETWEEN BL 18 TO BL 27,LEFT.....
FIRE PROTECTION - INSPECTIONOF FIRE EXTINGUISHER SYSTEM TUBE ASSEMBLY NUTS
FIRE PROTECTION - INSPECTIONOF FIRE EXTINGUISHER SYSTEM TUBE ASSEMBLY NUTS
INSPECTION OF NLG STEERING CYLINDER FOR MISSING SAFETY WIRE
INSPECTION OF NLG STEERING CYLINDER FOR MISSING SAFETY WIRE
INSPECTION OF NLG STEERING CYLINDER FOR MISSING SAFETY WIRE
EQUIPMENT FURNISHINGS-STATICLINE RETRIEVING WINCH SUPPORT-REPLACEMENT OF FASTENERS
ENGINE CONTROLS - INSPECTIONOF THROTTLE PULLEY GIMBAL YOKE FOR PROPER RETENTION ONENGINE COORDINATOR SHAFT.
ENGINE CONTROLS - INSPECTIONOF THROTTLE PULLEY GIMBAL YOKE FOR PROPER RETENTION ONENGINE COORDINATOR SHAFT.
DOORS-INSPECTION OF 382776-5PARATROOP DOOR OUTER WINDOW PANE AND REPLACEMENT OF 342398...
TÍTULO
01/03/1990
01/03/1990
05/05/1993
05/05/1993
22/08/1995
22/08/1995
22/08/1995
30/08/1995
20/03/1996
20/03/1996
02/03/1998
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
R
R
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/03/1990
06/11/1990
29/06/1993
05/05/1993
22/08/1995
22/08/1995
22/08/1995
30/08/1995
09/03/1998
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
52Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB A82-726
SB A82-742
SB A82-742
SB A82-742
SB A82-802
SB AV82-61-006
SB AV82-61-007
SB AV82-61-008
SB AV82-61-009
SB CMA-734-34-107
SB CMA-734-34-108
SB CMA-734-34-109
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
FABRICANTE
BSC
REV
SPL
SPL
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
NAT.
000
1
32
59
0
0
1
1
0
0
0
0
ORDEM
GLTT52A990048800
GLTT28A990050800
GLA328A030012400
GLA328A030012500
GLA327A060001500
GLA361S900006600
GLA361S020004801
GLTT61S990046200
GLTT61S990046400
GLA334S890002500
GLA334A890003300
GLA334S900004900
FADT
DOORS-INSPECTION OF 382776-5PARATROOP DOOR OUTER WINDOW PANE AND REPLACEMENT OF 342398...
FUEL-DEACTIVATION/INSPECTIONOF MAIN FUEL TANK DUMPS PUMPS AND DEACTIVATION OF EXTERNAL TANK BOOST PUMPS, C-130 AIRCRAFT
FUEL-DEACTIVATION/INSPECTIONOF MAIN FUEL TANK DUMPS PUMPS AND DEACTIVATION OF EXTERNAL TANK BOOST PUMPS, C-130 AIRCRAFT
FUEL-DEACTIVATION/INSPECTIONOF MAIN FUEL TANK DUMPS PUMPS AND DEACTIVATION OF EXTERNAL TANK BOOST PUMPS, C-130 AIRCRAFT
ONE-TIME INSPECTION OF AILERON BOOSTER INPUT QUADRANT CABLE RETENTION CLIP FASTENERS FOR TIGHTNEESAND REPLACEMENT OF NUTS.
PROPELLERS - PROPELLER BLADEINSPECTION, ALL HERCULES AIRCRAFT
PROPELLERS-PROPELLER BLADE INSPECTION-ALL 54H60 PROPELLER BLADES
PROPELLERS-PROPELLER BLADE INSPECTION ALL 54H60 PROPELLER BLADES EXHIBITING SERIAL NUMBER 840119 TO 866281
PROPELLERS - PROPELLER BLADEINSPECTION
NAVIGATION - ANTENNA CONPLERUNIT - CMA-734 O.N.S
OMEGA NAVIGATION SYSTEM CMA-734 - RPU MOD. OF BITE AND P/S ON PWB ASSEMBLY FOR IMPROVED SYSTEM IMMUNITY TO NOISE AND POWER ...
OMEGA NAVIGATION SYSTEM
TÍTULO
02/03/1998
03/07/1999
03/07/1999
03/07/1999
07/06/2006
25/05/1990
16/05/1997
30/07/1998
24/11/1998
05/02/1988
08/06/1988
04/07/1988
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
R
R
M
M
I
M
M
R
R
O
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
02/03/1998
27/07/1999
02/07/1999
02/07/1999
30/07/1998
13/01/1999
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
53Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB CMA-771-34-135
SB CMA-771-34-137
SB CMA-771-34-138
SB CMA-771-34-139
SB CMA-771-34-52
SB CMA-771-34-78
SB CMA-771-34-90
SB CMA-900-34-53
SB GS-70-1
SB GS-70-1
SB GS-87-1
SB GS-88-2
SB GS2001-3
SB GS89-2
SB GS90-1
SB GS90-2
Nº PUB
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CANADIAN MARCONI CO
CMC ELECTRONICS INC
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
AIRCRAFT BRAKING SYSTEMS CORP.
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
REV
BSC
REV
BSC
BSC
REV
REV
NAT.
0
0
0
0
0
0
0
0
3
4
000
3
0
000
1
1
ORDEM
GLA334A890004600
GLA334A900005700
GLA334A900005000
GLA334A900005100
GLA334A900007800
GLA334A890003700
GLA334A840006800
GLA334A110001400
GLA332S910009703
GLA332S030014800
GLA332S870003200
GLA332S020011900
GLA332A020008000
GLA332S910002700
GLA332S910002501
GLA332S910002601
FADT
IMPROVED KEYBOARD PUSH BUTTON RELIABILITY
ANTENNA COUPLER UNIT CMA-771ONS ACU - CASE MOD
MOD.OF BITE & P/S ON PWB ASSY FOR IMPROVED SYSTEM IMMUNITY TO NOISE AND POWER TRANSIENTS
MOD.1 ARINC-429 INTERFACE PWB ASSY. FOR IMPROVE RELIABILITY OF ARINC-561 OUTPUTS
IMPROVED KEYBOARD PUSHBUTTONRELIABILITY
RPU- REDUCTION OF CAPACTIVE LOADING ON "TAS VALID" INPUT
RPU - MEMORY TIMING LOGIC FUNCTION: NOISE IMMUNITY
MOD.OF RECEIVER PWB ASSEMBLYFOR ELIMINATION OF SELF-TESTSIGNAL LEAKAGE
NAVIGATION - CMA-900 FLIGHT MANAGEMENT SYSTEM INTRODUCTION OF 2010 MANGETIC VARIONTION MODEL
AIRCRAFT TAIRE, TUBE, AND WHEEL HANDLING PRECAUTIONS. (VER SB GS70-1)
AIRCRAFT TAIRE, TUBE, AND WHEEL HANDLING PRECAUTIONS. (VER SB GS70-1)
NITROGEN TIRE INFLATION
DRY STRIPPING OF PAINT
LANDING GEAR - BRAKE ASSEMBLY - BOLTS AND NUTS
MIL-T-83483 ANTIUSEIZES CUNPOUND.
HOLDERS OF GENERAL SERVICE BULLETIN GS-1 FOR PLUG WARNING USED ON ALL AIRCRAFTBRAKING SYSTEMS BRAKES
HOLDERS OF GENERAL SERVICE BULLETIN GS90-2 FOR PIN PLUG
TÍTULO
09/02/1988
27/05/1988
25/05/1988
30/06/1988
10/09/1981
24/08/1983
20/06/1984
01/06/2010
15/05/1970
15/05/1970
27/08/1987
01/09/1988
10/12/2001
02/11/1989
20/07/1990
20/07/1990
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
R
R
I
I
I
I
I
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
17/07/1989
18/05/1990
27/08/1987
16/11/1999
02/11/1989
02/10/1990
01/10/1990
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
REMOTO
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
54Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB GTCP85-49-5809
SB HSI-45-34-03
SB L382-32-4
SB M-1120
SB M-1137
SB M-1137
SB M-1142
SB M-1185
SB M-1196
SB M-1199
SB M-1199
SB M-1755
SB M-1896
SB M-1896
SB M-3001
Nº PUB
HONEYWELL INTERNATIONAL INC
ROCKWELL COLLINS, INC.!DBA
CONSULTAR CODEMP 001KK
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
FABRICANTE
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
REV
REV
BSC
BSC
REV
BSC
REV
NAT.
000
000
000
000
1
000
000
2
1
2
0
000
1
000
3
ORDEM
GLA349S890006700
GLA334S840010100
GLA332S040008000
GLTT34A770003000
GLA334A780002601
GLA334A780002700
GLA334A780002800
GLA334A820004802
GLA334A820005000
GLA334A800007502
GLA334A800007400
GLTT34A910000501
GLA334S860003001
GLA334S860003100
GLTT34A890000401
FADT
REPAIR USED ON ALL AIRCRAFT BRAKING SYSTEMS BRABES
AIRBONE AUXILIARY POWER - FUEL CONTROL UNIT - INCORPORATION OF NON
REPLACEMENT OF LAMP DRIVER DEVICER
ASTON INSULATOR REPLACEMENT FOR BRAKE ASSEMBLY
RADIO ALTIMETER - REPLACING COUNTER BOARD CAPACITORS WITH MATCHED CAPACITORS
CAPACITOR C26 ON FLAG ALARM BOARD AND C26 ON TRANSITTER ASSEMBLY
CAPACITOR C26 ON FLAG ALARM BOARD AND C26 ON TRANSITTER ASSEMBLY
RADIO ALTIMETER - RESISTOR ADDED TO 26 VAC OUTPUT
INTERNAL MOD1 TO STRIPLINE ASSEMBLY PN 2037046-0501 RECEIVER MIXER DIOG REPLACEMENT
UNIT MODERNIZATION WITH LATEST STATE OF ART TRANSMITTER
REPLACEMENT OF 2N536 TRANSISTORS WITH 2M1893 TRANSISTORS
REPLACEMENT OF 2N536 TRANSISTORS WITH 2M1893 TRANSISTORS
TO IMPROVE COMMUTATING CAPABILITY OF TRIAC Q5001
TO IMPROVE OPERATING OF D.H MONITOR WHEN D.H BUG IS BELOW 100 FT
TO IMPROVE OPERATING OF D.H MONITOR WHEN D.H BUG IS BELOW 100 FT
TO REAJUST THE BIAS ON TRANSISTOR Q501, DUE TO TRANSISTOR TYPE CHANGE WHEN MOD 6 WAS INCORPORATED
TÍTULO
28/10/1988
30/05/1984
15/09/1987
01/10/1976
01/12/1976
01/12/1976
01/01/1977
01/08/1977
01/02/1978
01/08/1979
01/08/1979
01/11/1990
01/08/1985
01/08/1985
01/04/1987
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
O
O
R
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
28/10/1988
30/05/1984
15/09/1987
01/10/1976
01/04/1977
01/12/1976
01/01/1977
01/03/1980
01/04/1980
01/12/1979
01/11/1990
01/05/1986
01/08/1985
01/03/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
55Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB M-3226
SB M-3342
SB M-3393
SB M-3393
SB M-3393
SB M-3393
SB M-3393
SB M-3430
SB M-3576
SB M-3726
SB M-3956
SB M-3956
SB M-962
SB MI 1C30-34-0001
SB ONS-TE-010
SB ONS-TE-011
SB SBL11115A
SB TPA-81A-34-120
Nº PUB
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
AVIONICS SERVICES
CANADIAN MARCONI CO
CANADIAN MARCONI CO
ASTRONAUTICS CORP OF AMERICA
HONEYWELL INTERNATIONAL, INC
FABRICANTE
REV
REV
REV
REV
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
BSC
BSC
REV
NAT.
002
1
1
2
000
3
4
000
000
000
000
000
1
0
0
0
0
2
ORDEM
GLA334A940002202
GLTT34A920003601
GLA334A030015500
GLA334A030015600
GLA334A900006300
GLA334A030015700
GLA334A940002604
GLA334A900006700
GLTT34A910000601
GLTT34A920003500
GLTT23A920004000
GLTT23S920002400
GLA334S890006001
GLA334A030001500
GLA334A890001800
GLA334A890001900
GLA377A130000600
GLA334S030006400
FADT
PPI-1TB WEATHER RADAR INDICATOR
TO PREVENT MOISTURE INTRUSION
TO IMPROVE TOLERANCE INTEGRITY
TO IMPROVE TOLERANCE INTEGRITY
TO IMPROVE TOLERANCE INTEGRITY
TO IMPROVE TOLERANCE INTEGRITY
TO IMPROVE TOLERANCE INTEGRITY
TO PREVENT RESISTOR FROM BURNINGY REGULATOR BOAR
TO ELIMINATE VIDEO WEDGES AT47 EACH SIDE OF DISPLAY
TO ENHANCE TUNING ADJUSTMENTOF AFC COILS
ALA-51A RADIO ALTIMETER TODISABLE AFC CIRCUIT
ALA-51A RADIO ALTIMETER TODISABLE AFC CIRCUIT
ANA-51()ALTIMETER ANTENNAS
NAVEGAÇÃO-INSTALAÇÃO DO SISTEMA TCAS E TRANSPONDER MODE S
PROCESSOR CONTROL PANEL 412-347 NEW VARIATION(003) WITH EXPANDED EPROM MEMORY
ADAPTER TEST JIG 477-878 IMPROVED SIMULATION OF AIRCRAFT WIRING IMPROVED TIMING IN DME SIMULATOR CIRCUITS REVISED PWB WIRING ...
ENGINE DATA CONCENTRATOR - RPM FLUTUATIONS - CONNECT CAPPED & STOWED WIRES TO AIRCRAFT GROUND
NAVIGATION - TPA-81A TCAS PROCESSOR UNIT MOD 28 FOR DATA LOADER AND NON-DATA
TÍTULO
01/02/1989
01/04/1989
01/02/1990
01/02/1990
01/02/1990
01/02/1990
01/02/1990
01/12/1989
01/07/1990
01/07/1991
01/05/1992
01/05/1992
01/05/1974
10/06/2002
25/03/1983
12/04/1983
29/01/2010
12/12/2000
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
O
R
R
R
R
R
R
R
O
O
O
R
M
O
M
M
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/08/1990
01/09/1991
01/11/1990
01/12/1990
01/02/1990
01/01/1993
01/05/1993
01/12/1989
01/07/1990
01/07/1991
01/05/1992
01/05/1992
01/04/1988
15/10/2002
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL PARQUE/BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
56Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB TPA-81A-34-126
SB TPA-81A-34-126
SB V82-21-001
SB V82-71-004
SB V82-71-008
SB V82-71-011
SB V82-71-013
SB V82-71-022
SB V82-71-025
SB V82-71-026
SB V82-71-027
SB V82-71-35
SB V82-80-001
SB V82-80-003
Nº PUB
HONEYWELL INTERNATIONAL, INC
HONEYWELL INTERNATIONAL, INC
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
REV
BSC
NAT.
2
3
000
0
0
0
0
000
0
0
0
0
1
000
ORDEM
GLA334S030006700
GLA334S030009400
GLA321S830001000
GLTT73S770006300
GLTT71S770001100
GLTT72S770006400
GLTT71S770006100
GLA371S780000400
GLA371S780001500
GLA371S780001600
GLA300S020076800
GLA375S840007200
GLA380A780003201
GLA380S810004200
FADT
LOADER UNITS TO INSTALL NEW SOFTWARE
MINOR SOFTWARE REVISION AND CONVERSION OF TPA-81A PART NUMBER FOR DATA LOADER UNITS
MINOR SOFTWARE REVISION AND CONVERSION OF TPA-81A PART NUMBER FOR DATA LOADER UNITS
AIR CONDITIONING - REWORK OFCABIN AIR PRESSURE OUTFLOW VALVE AIR JET PUMP ASSEMBLY
POWER PLANT - MODIFICATION OF SPRING MOUNTING BRACKET ON THE FUEL METERING VALVE
POWER PLANT - REPLACEMENT OFTURBINE, FIRST, SECOND, AND THIRD STAGE BLADES
POWER PLANT - REPLACEMENT OFTURBINE FIRST STAGE WHEEL ASSEMBLY
POWER PLANT - REPLACEMENT OFINNER REAR EXHAUST CONESELF-LOCKING NUT.
POWER PLANT - OUTER COMBUSTION CASE INSPECTION.
POWER PLANT - INSTALLATION OF ENGINE SPRAY SHIELD BRACKET.
POWER PLANT - MODIFICATON OFCOMBUSTION CHAMBER INNER CSSING ASSEMBLY.
POWER PLANT - USE OF FRONT COMPRESSOR BEARING CONTAINING CORROSION RESISTANT STEEL.
POWER PLANT- 1-2 STAGE TURBINE SPACER, INSPECTION FOR
STARTING-REVISED INSTALLATION, OPERATION, ANDMAINTENANCE INSTRUCTIONS FORBENDIX 36 E 84 SERIES STARTERS
STARTING - REPLACEMENT OF ENGINE DRIVE COUPLING AND
TÍTULO
10/12/2001
10/12/2001
27/10/1983
14/01/1977
24/02/1977
29/03/1977
19/05/1977
24/03/1978
24/04/1978
19/04/1978
14/04/1978
11/03/2002
18/10/1974
10/06/1980
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
M
M
R
R
R
R
R
R
M
I
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/10/2002
05/11/2002
27/10/1983
24/03/1978
07/07/1978
10/06/1980
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
57Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SB V82-80-004
SB V82-80-005
SB V82-80-006
SB V82-80-007
SIL 10-75
SIL 2-92
SIL 37
SIL APU-42
SIL GEN-17
SIL GP-11
SIL T56 94-13R
SIL T56/501D: 94-14
SIL T56/501D: 94-15
SIL T56: 94-01
SIL T56: 94-02
SIL T56: 94-10
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
ROCKWELL COLLINS, INC.!DBA
ROCKWELL COLLINS, INC.!DBA
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
HONEYWELL ENGINES & SYSTEMS
SMITHS
HONEYWELL INTERNATIONAL INC
ROLLS ROYCE
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
FABRICANTE
REV
BSC
BSC
BSC
REV
BSC
BSC
BSC
REV
BSC
BSC
REV
BSC
REV
REV
REV
NAT.
2
000
000
000
001
000
0
0
2
0
0
A
0
A
A
A
ORDEM
GLA380S910005702
GLA380S830000500
GLA380S860002600
GLA380S040006700
GLA324A040008500
GLTT23A940000700
GLA332S840003200
GLA349A900000300
GLA300A090001700
GLA349A890006600
SPA300S060002000
GLA372S950002201
GLA372S950002100
GLA372S950002701
GLA372S950002601
GLA372S950002501
FADT
YOW RETURN PLATE ASSEMBLY
STARTING - ADJUSTMENT OF STARTER CONTROL VALVE.
STARTING - INSPECTION OF COUPLING CLAMP P/N 2483677 AND INSTALATION OF MOUNTING HEAD P/N 2489140
STARTING - MODIFICATION OF 36 E 84 STARTERS TO THE - QFCONFIGURATION.
STARTING - INSPECTION FOR AND REPLACEMENT OF AIR TURBINE STARTER COUPLING CLAMP.
SYSTEM INSTALLATION IN THE C-130H/L382B, L382E, L382G AIRCRAFT
COAXIAL CABLE FOR NEW AISCRAFT INSTALLATIONS
MLG TRACK SHOE CLEARANCES
IMPROVER SERVICING PROCEDURES - UNAUTHORIZED USE OF SILICONE - BASED LUBRICANTS ON OIL-WETTED COMPONENTS WITHIN THE APU'S ...
SERVICE INFORMATION LETTER
APPROPRIATE INSTRUCTIONS FORREPAIR ORDERS ON ELETRONIC COMPONENTS RETURNED TO GARRET FACILITIES FOR MAINTENANCE
SERIES II TO SERIES III CONVERSION KITS RELEASE
T56/501D ENGINE MODELS AND APPLICATIONS
ALLISON DIRECT PARTS ORDERING PROCESS.
FUEL NOZZLE BOLT LUBRICANT
ENHANCED RELIABILITY GEARBOX-KIT RELEASE
T56 ENGINE PERFORMANCE
TÍTULO
10/06/1980
07/04/1983
31/01/1986
04/12/1989
01/12/1975
24/09/1992
01/06/1979
17/02/1989
01/01/2005
13/01/1989
21/05/2004
15/10/1994
15/09/1994
01/02/1994
15/02/1994
30/03/1994
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
M
I
R
I
I
I
I
O
I
I
I
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
07/01/1991
07/04/1983
31/01/1986
04/12/1989
31/05/1991
24/09/1992
01/01/2009
15/11/1994
01/09/1994
15/10/1994
30/06/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
58Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SIL T56: 94-11
SIL T56: 94-13
SIL T56: 94-16
SIL T56: 94-17
SIL T56:94-10R
SIL T56:94-13R
SIL-1000
SIL-1003
SIL-1004
SIR 005
SIR 54H60-104
SIR 54H60-112
SIR 54H60-116
SIR 54H60-117
SIR 54H60-117A
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ROLLS ROYCE
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED GEORGIA COMPANY
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION³DIV HAMILTON
HAMILTON SUNDSTRAND CORPORATION
UNITED TECHNOLGIES CORP HAMILTON STD DIV
UNITED TECHNOLGIES CORP HAMILTON STD DIV
FABRICANTE
BSC
BSC
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
000
000
000
C
1
0
0
0
0
0
0
0
0
0
ORDEM
GLA372S950002400
GLA372S950002300
GLA372S950002000
GLA372S950001900
GLA372S040008400
GLA372S040008300
GLA300A070000200
GLA370A080000100
GLA329A090000400
GLA361S020010600
GLA361S020008400
GLA361A020005000
GLA361S970003800
GLA361S020011000
GLA361S020073600
FADT
CALCULATION & TRENDING - SUPPORT EQUIPMENT RELEASE.
ENGINE PERFORMANCE - MAINTENANCE GROUND CHECIL PROCEDURE.
SERIES II TO SERIES III CONVERSION KIT RELEASE
NEW 5TH & 10TH STAGE BLEED GASKETS
TD AMPLIFIER P/N 23009257 RECALL
"T56/501D SERIES I/II/III ENGINE PERFORMANCE CALCULATION TRENDING SOFTWARE AND EQUIPMENT RELEASE".
"T56-A-7A/7B TO T56-A-15LFE CONVERSION KITS RELEASE".
INTRODUCING THE C130B-H SERVICE INFORMATION LETTER
NACELLES AND PYLONS - QEC TRUSS MOUNT ATTACHMENT BOLT DEFICIENCY.
HYDRAULIC POWER - 47560 MAINLANDING GEAR SELECTOR VALVE DEFECT.
PROPPELER TRAINING 2002 SCHEDULE
54H60 PROPELLER BLADE ALERT SERVICE BULLETINS
NEW SERIAL NUMBER CONFIGURATION FOR 54H60 PROPELLER BLADES
REPORTING OF 54H60 PROPELLERS BLADES REMOVED FROM FURTMER SERVICE USE
TIME DEALINE APPLICABLE TO INSPECTION OF THE RETENTION FILLET RADIUS OF 54H60 PROPELLER BLADES
TIME DEADLINE APPLICABLE TO INSPECTION OF THE RETENTION FILLET RADIUS OF 54H60 PROPELLER BLADES
TÍTULO
25/08/1994
15/08/1994
15/10/1994
15/12/1994
30/03/1994
15/08/1994
19/12/2006
21/01/2008
02/10/2008
26/10/2001
20/10/1998
21/02/2000
12/10/2000
01/08/2001
15/08/2002
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
I
I
I
I
I
M
M
I
I
I
M
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/08/1994
15/10/1994
15/12/1994
23/02/2001
12/12/2000
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
59Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SIR : NEWSLETTER 02
SIR : NEWSLETTER : 01
SIR: 54H60-110
SIR: 54H60-119
SL 1878
SL 1878
SL 1878
SL 1878
SL 1878
SL 1878
SL 1878
SL 1878
SL 1878
Nº PUB
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
HAMILTON SUNDSTRAND CORPORATION
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
BF GOODRICH
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
0
0
0
0
0
0
0
0
0
ORDEM
GLA361S020006200
GLA361S020005700
GLA361S020006300
GLA361S030007100
GLA300A010000400
GLA300A010000500
GLA300A010000600
GLA300A010000700
GLA300A010000800
GLA300A010000900
GLA300A010001000
GLA300A010001100
GLA300A010001200
FADT
LARGE COMMERCIAL AND MILITARY PROPELLER ACTIVITY UPDATE
LARGE COMMERCIAL AND MILITARY PROPELLER SYSTEMS
"DESIGN CRITICAL CHARACTERISTICS (DCC) PROGRAM".
INSPECTION OF RESIDUAL STRESS (COLD ROLLING) IN 54H60 PROPELLER BLADES
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OF
TÍTULO
30/08/1999
01/02/1999
31/12/1999
31/01/2003
27/03/2001
27/03/2001
27/03/2001
27/03/2001
27/03/2001
27/03/2001
27/03/2001
27/03/2001
27/03/2001
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
I
I
R
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
60Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SL 1878
SL 85-02
SL 85-02
SL 85-02
SL 86-03
SL 86-06
SL 88-30
SL 89-08
SL GS-SL-11
SL GS-SL-11
SL GS-SL-17
SL GS-SL-18
SL GS-SL-18
Nº PUB
BF GOODRICH
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
HONEYWELL INTERNATIONAL INC³DBA HONEYWELL
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
FABRICANTE
BSC
BSC
REV
REV
BSC
BSC
BSC
BSC
REV
REV
REV
REV
REV
NAT.
0
000
1
2
000
000
000
000
2
3
1
4
5
ORDEM
GLA300A010001300
GLA334A860002500
GLA334S040011500
GLA334A910006202
GLA334A880002900
GLA334A860002400
GLA334X900004400
GLA334A890005400
GLA332S860001202
GLA332S040008100
GLA332S860001101
GLA332A910001404
GLA332S020014500
FADT
DISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
"LANDING GEAR - WHEEL AND BRAKE ASSEMBLIES - EFFECT OFDISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES".
CHANGE IN PART NUMBER FOR RELAY K1501, ON FLAG ALARM BOARD
CHANGE IN PART NUMBER FOR RELAY K1501, ON FLAG ALARM BOARD
CHANGE IN PART NUMBER FOR RELAY K1501, ON FLAG ALARM BOARD
COMPONENT FAILURE OF BOURNS (V32997) MINIATURE VARIABLE RESISTORS
CLOKE BENDIX PN 2068179-0701, MFG. PN JB172C10, NSN 5950-00-175-9197
RADIO ALTIMETER INDICATOR BEARINGS
TO ELIMINATE THE REMOVAL OF THE TRANSMITTER FOR THE-13V ADJUCTMENT AND...
HOLDERS OF SERVICE LETTER GS-SL-11 EMPHASSIS ON PROCEDURES COMMONLY PERFORMED INADEQUATELY DURING ASSEMBLY OF AIRCRAFT WHEELS
HOLDERS OF SERVICE LETTER GS-SL-11 EMPHASSIS ON PROCEDURES COMMONLY PERFORMED INADEQUATELY DURING ASSEMBLY OF AIRCRAFT WHEELS
HOLDERS OF SERVICE LETTER GS-SL-17 FOR MAIN LANDING GEAR BRAKE FREEZE-UP
HOLDERS OF GEWNERAL SERVICE LETTER GS-SL-18 FOR STANDARDGY-GYR RIVETS
HOLDERS OF GEWNERAL SERVICE
TÍTULO
27/03/2001
01/02/1985
01/02/1985
01/02/1985
01/02/1986
01/03/1986
01/05/1989
01/06/1989
03/09/1981
03/09/1981
07/02/1985
13/09/1985
13/09/1985
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
M
R
R
R
I
I
I
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/02/1985
01/02/1987
01/03/1989
01/02/1986
01/03/1986
01/05/1989
01/06/1989
18/07/1989
28/11/1990
20/09/1985
13/09/1990
10/01/2000
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
61Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SL GS-SL-21
SL GS-SL-22
SL GS-SL-25
SL GS-SL-29
SL GS-SL-30
SL GS-SL-33
SL GS-SL-35
SL GS-SL-35
SL GS-SL-36
SL GS-SL-36
SL GS-SL-38
SL GS-SL-39
SL GS-SL-39
SL GS-SL-46
SL GS-SL-7
SL GS-SL-9
SL GS-SL-9
SL L-382-SL-1
SL L-382-SL-1
Nº PUB
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
CONSULTAR CODEMP 001KK
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
FABRICANTE
REV
BSC
BSC
BSC
REV
BSC
REV
REV
BSC
REV
BSC
BSC
REV
REV
REV
REV
REV
BSC
REV
NAT.
1
0
0
000
1
000
1
2
000
2
000
000
1
1
3
2
3
0
1
ORDEM
GLA332A910008401
GLA332A880001900
GLA332S910001600
GLA332S910008500
GLA332S910009601
GLA332S910001500
GLA332S020011100
GLA332A930002502
GLA332S930002600
GLA332S930002902
GLA332S940001400
GLA332S940003400
GLA332S030015900
GLA332S020012100
GLA332S910009503
GLA332A030016000
GLA332A910008803
GLA332A940001500
GLA332A940001601
FADT
LETTER GS-SL-18 FOR STANDARDGY-GYR RIVETS
ASBESTOS - FREE LININGS
IMPROVED CORROSION PREVENTIVE COMPOUND
AIRCRAFT WHEEL BEARINGS AND BEARING CUPS
PRESSURE RELEASE PLUG LEAK TEST
USE OF UNAUTHORIZED PARTS INAIRCRAFT BRAKING SYSTEM WHELL AND BRAKES ASSEMBLIES
DRAW FLATTENING PROCEDURE FOR STEEL BRAKE ASSEMBLIES
INTRODUCTION OF THE AUTHORIZED PARTS TAG.
INTRODUCTION OF THE AUTHORIZED PARTS TAG.
WHEEL INSPECTION AND OVERHAUL SCHEDULES
WHEEL INSPECTION AND OVERHAUL SCHEDULES
TIMKEN PERFORMANCE CODE 629 FOR BEARING CUPS AND BEARINGCONES
NON - DESTRUCTIVE TESTING OFWHEEL ASSEMBLIES AND BRAKE ASSEMBLIES
NON - DESTRUCTIVE TESTING OFWHEEL ASSEMBLIES AND BRAKE ASSEMBLIES
PAINT WHITCH COMPLIES WITH EPAEMISSION STANDARDS
CHECKING OF WHEEL FASTENERS,TIE BOLTS AND NUTS
AIRCRAFT WHEEL BEARING CLASSNUMBERS
AIRCRAFT WHEEL BEARING CLASSNUMBERS
LANDING GEAR-BRAKE ASSEMBLY
LANDING GEAR-BRAKE ASSEMBLY
TÍTULO
30/06/1986
28/11/1986
15/12/1988
18/04/1990
21/09/1990
26/02/1991
15/01/1993
15/01/1993
19/07/1993
19/07/1993
18/02/1994
01/04/1994
01/04/1994
10/10/1997
21/02/1980
09/02/1983
09/03/1983
15/03/1994
15/03/1994
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
M
R
I
I
R
I
I
I
I
I
I
I
I
I
I
I
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/08/1989
18/04/1990
24/02/1997
26/02/1991
30/07/1993
27/05/1994
19/07/1993
17/01/1994
18/02/1994
01/04/1994
07/12/1996
26/07/1999
17/07/1989
31/05/1989
04/02/1994
15/09/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
62Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
SL TCAS-TPA-81A-01
SL TCAS-TPA-81A-01
SL TCAS-TPA-81A-02
SL-10
SL-10
SL-10E
SL-113
SL-12
SL-12
SL-12
TCTO 13C2-1-506
TCTO 13C2-1-507
TCTO 16G3-2-81-502
TCTO 16L1-3-10-501
TCTO 1C-130-1000
TCTO 1C-130-1000
TCTO 1C-130-1000
TCTO 1C-130-1004
Nº PUB
HONEYWELL INTERNATIONAL INC
HONEYWELL INTERNATIONAL INC
HONEYWELL
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
L-3 COMMUNICATIONS AVIONICS SYSTEMS
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
REV
REV
REV
REV
BSC
REV
BSC
REV
REV
BSC
BSC
BSC
BSC
BSC
SPL
SPL
BSC
NAT.
0
1
1
C
D
0
A
000
A
B
000
000
0
0
000
C
D
0
ORDEM
GLA300S030009800
GLA334S020021200
GLA334S030006800
GLA300X980001100
GLA334A850001502
GLA300S040008200
GLA334X910002801
GLA334S840010301
GLA334A840010201
GLA334A030053100
GLA325A800000700
GLA325A830000700
GLA332S810001600
GLA332S860001500
GLA325A860000400
GLTT20A800000103
GLA325A870001902
GLA327A790001100
FADT
POSSIBLE REAR INTERCONNECT WITH FAULT CABLES W-1131 THROUGGH W-1138
POSSIBLE REAR INTERCONNECT WITH FAULT CABLES W-1131 THROUGGH W-1138
NOTIFICATION OF PART NUMBER CONVERSION FOR HONEYWELL (FORMELY ALLIED SIGNAL) CHANGE 7.0 TCAS PROCESSORS
GYRO HANDLING AND PACKAGING
GYRO HANDLING AND PACKAGING
GYRO HANDLING AND PACKAGING
SHELF LIFE
SELF- CONTAINED INDICATOR OPERATION
SELF- CONTAINED INDICATOR OPERATION
SELF- CONTAINED INDICATOR OPERATION
URGENT ACTION ONE TIME INSPECTION OF THE DOWN ADJUSTE TYPE CGU-AE, MFG PART NUMBER FDC-5730 ORDER
ONE TIME INSPECTION REMOVAL OF ALL TIE DOWN ADJUSTERS
IMPROVEMENT OF BALLSCREN RELIABILITY, CALCO P/N 8353 AND 8430.
INSPECTION OF GLINDER HEADS ON THE NOSE LANDING GEAR
IMPROVED STATIC LINE RETRIEVER CABLE CLIPS
IMPROVED STATIC LINE RETRIEVER CABLE CLIPS
IMPROVED STATIC LINE RETRIEVER CABLE CLIPS
INSPECTION AND REPAIR OF F.S.93 FLIGHT CONTROL PULLEYBRACKETS, PART NO.350283, 350285, AND 350096, C-130
TÍTULO
24/04/2001
24/04/2001
25/07/2001
01/01/1984
01/01/1984
22/02/1995
20/02/1991
19/07/1976
19/07/1976
19/07/1976
18/10/1979
15/01/1983
16/10/1981
15/01/1986
01/06/1986
01/06/1986
01/06/1986
20/06/1979
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
I
I
I
I
I
I
R
I
I
I
I
I
M
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/08/2001
28/09/2001
01/03/1984
22/10/1984
13/03/1991
19/07/1976
08/08/1980
07/10/1985
18/10/1979
15/01/1983
01/06/1986
24/07/1986
08/02/1987
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL REMOTO
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
63Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1004
TCTO 1C-130-1005
TCTO 1C-130-1005
TCTO 1C-130-1005
TCTO 1C-130-1005
TCTO 1C-130-1005
TCTO 1C-130-1005
TCTO 1C-130-1006
TCTO 1C-130-1006
TCTO 1C-130-1009
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
SPL
SPL
SPL
SPL
SPL
BSC
SPL
BSC
NAT.
C
0
C
D
E
G
H
0
C
0
ORDEM
GLA327A030037200
GLA325A810000600
GLA325A030037700
GLA325A030037600
GLA325A030037500
GLA325A030037300
GLA325A030037400
GLA354A800004000
GLA354A800004101
GLA332S790001700
FADT
AIRCRAFT
INSPECTION AND REPAIR OF F.S.93 FLIGHT CONTROL PULLEYBRACKETS, PART NO.350283, 350285, AND 350096, C-130 AIRCRAFT
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
REMOVAL OF BY-PASS COMPONENTS FROM LEFT LATCHESOF A/A32H-4A, CARGO HANDLINGSYSTEM, C-130A/B/D/E/H, EC/MC-130E AND RC-130A ...
INSPECTION OF TRUSS ASSEMBLY, ENGINE MOUNT, NO.2AND NO.3 ENGINES, C-130 AIRCRAFT
INSPECTION OF TRUSS ASSEMBLY, ENGINE MOUNT, NO.2AND NO.3 ENGINES, C-130 AIRCRAFT
INSPECTION OF ONE-WAY
TÍTULO
20/06/1979
23/11/1982
23/11/1981
23/11/1981
23/11/1982
23/11/1981
20/03/1987
28/09/1979
28/09/1979
25/06/1979
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
R
R
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
28/08/1979
15/01/1982
15/09/1982
21/12/1982
29/08/1984
07/08/1987
30/11/1979
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
64Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1011
TCTO 1C-130-1013
TCTO 1C-130-1013
TCTO 1C-130-1013
TCTO 1C-130-1015
TCTO 1C-130-1015
TCTO 1C-130-1017
TCTO 1C-130-1019
TCTO 1C-130-1021
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
SPL
SPL
BSC
SPL
BSC
BSC
SPL
NAT.
0
0
C
D
0
C
0
0
C
ORDEM
GLA361S820003300
GLA321A800000400
GLA321A800000501
GLA321A800000602
GLA327A800002000
GLA300A030037800
GLA332A800002900
GLA372S800005200
GLA361S810003201
FADT
RESTRICTOR VALVE, PART NO.1R3084-025, INSTALLED IN NORMAL HYDRAULIC BRAKE ACCUMULATOR SYSTEM AND ...
INSPECTION OF HAMILTON STANDARD PUMP HOUSING FILLERFLANGE, PART NO.513675, C-130 AIRCRAFT
REACTIVATION OF INTEGRAL LIGHTING CABIN AIR PRESSURE OUTFLOW VALVE, PART NO.102538 AND 102076, C-130 AIRCRAFT
REACTIVATION OF INTEGRAL LIGHTING CABIN AIR PRESSURE OUTFLOW VALVE, PART NO.102538 AND 102076, C-130 AIRCRAFT
REACTIVATION OF INTEGRAL LIGHTING CABIN AIR PRESSURE OUTFLOW VALVE, PART NO.102538 AND 102076, C-130 AIRCRAFT
INSPECTION FOR CUTLER-HAMMERRELAY, PART.NO.6041H230, IN THE ELEVATOR AND AILERON TRIM TAB CONTROL SYSTEM, C-130 SERIES AIRCRAFT
INSPECTION FOR CUTLER-HAMMERRELAY, PART.NO.6041H230, IN THE ELEVATOR AND AILERON TRIM TAB CONTROL SYSTEM, C-130 SERIES AIRCRAFT
INSPECTION FOR AND REMOVAL OF METAL OVERHAUL DATA PLATES FROM MAIN LANDING GEAR BALL SCREW ASSEMBLIES -C-130 AIRCRAFT
INSPECTION OF ENGINE MOUNT BOLTS FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF PROPELLER FEATHER OVERRIDE SWITCH JUMPER WIRE INSTALLATION, C-130 AIRCRAFT
TÍTULO
31/12/1979
01/02/1980
01/02/1980
01/02/1980
15/01/1980
15/01/1980
19/10/1979
02/01/1980
20/10/1980
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
24/03/1980
16/09/1980
28/02/1980
12/12/1980
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
65Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1021
TCTO 1C-130-1021
TCTO 1C-130-1021
TCTO 1C-130-1021
TCTO 1C-130-1024
TCTO 1C-130-1024
TCTO 1C-130-1024
TCTO 1C-130-1027
TCTO 1C-130-1027
TCTO 1C-130-1027
TCTO 1C-130-1029
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
SPL
SPL
BSC
SPL
SPL
BSC
SPL
SPL
BSC
NAT.
D
E
F
G
0
C
D
0
C
E
0
ORDEM
GLA361S810003302
GLA361S810003503
GLA361S810003404
GLA361S810003605
GLA376A800006000
GLA376A800006201
GLA376A800006302
GLA352A800006800
GLA352A800007101
GLA352A820005502
GLA323A800001100
FADT
INSPECTION OF PROPELLER FEATHER OVERRIDE SWITCH JUMPER WIRE INSTALLATION, C-130 AIRCRAFT
INSPECTION OF PROPELLER FEATHER OVERRIDE SWITCH JUMPER WIRE INSTALLATION, C-130 AIRCRAFT
INSPECTION OF PROPELLER FEATHER OVERRIDE SWITCH JUMPER WIRE INSTALLATION, C-130 AIRCRAFT
INSPECTION OF PROPELLER FEATHER OVERRIDE SWITCH JUMPER WIRE INSTALLATION, C-130 AIRCRAFT
INSPECTION OF FUEL COORDINATOR SHAFT, GIMBAL YOKE AND ALL ROD ENDS AND BOLTS, ENGINE CONTROL INSTALLATION, C-130 AIRCRAFT
INSPECTION OF FUEL COORDINATOR SHAFT, GIMBAL YOKE AND ALL ROD ENDS AND BOLTS, ENGINE CONTROL INSTALLATION, C-130 AIRCRAFT
INSPECTION OF FUEL COORDINATOR SHAFT, GIMBAL YOKE AND ALL ROD ENDS AND BOLTS, ENGINE CONTROL INSTALLATION, C-130 AIRCRAFT
AFT CARGO DOOR ACTUATING CYLINDER ROD END BEARING CHANGE, C-130B AND SUBSEQUENT AIRCRAFT
AFT CARGO DOOR ACTUATING CYLINDER ROD END BEARING CHANGE, C-130B AND SUBSEQUENT AIRCRAFT
AFT CARGO DOOR ACTUATING CYLINDER ROD END BEARING CHANGE, C-130B AND SUBSEQUENT AIRCRAFT
INSPECTION OF ADF ANTENNA COVERS AND DOPPLER RADOMES,
TÍTULO
20/10/1980
20/10/1980
20/08/1900
20/10/1980
15/02/1980
15/02/1980
15/02/1980
18/04/1980
18/04/1980
18/04/1980
18/04/1980
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
M
M
M
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
20/05/1981
14/09/1981
07/12/1981
13/09/1982
31/03/1980
09/05/1980
19/11/1980
18/08/1981
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
66Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1029
TCTO 1C-130-1030
TCTO 1C-130-1030
TCTO 1C-130-1036
TCTO 1C-130-1043
TCTO 1C-130-1043
TCTO 1C-130-1047
TCTO 1C-130-1047
TCTO 1C-130-1048
TCTO 1C-130-1052
TCTO 1C-130-1052
TCTO 1C-130-1052
TCTO 1C-130-1053
TCTO 1C-130-1053
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
SPL
BSC
BSC
SPL
BSC
SPL
BSC
BSC
SPL
SPL
BSC
SPL
NAT.
C
0
C
0
0
C
0
C
0
0
C
D
0
C
ORDEM
GLA323A810000100
GLA323A800001200
GLA323A030038100
GLA324A800001400
GLA322A810000300
GLA322A820000301
GLA321A810000200
GLA321A030039700
GLA373S810003800
GLA327A810001000
GLA324A030039800
GLA324A030039900
GLA329A810001300
GLA329A030040000
FADT
ALL C-130 AIRCRAFT
INSPECTION OF ADF ANTENNA COVERS AND DOPPLER RADOMES, ALL C-130 AIRCRAFT
INSPECTION OF WIRE BUNDLE FOR CHAFING AT F.S.457, C-130B/E/H, HC-130H/N/P, WC-130E/H, AND AC-130H AIRCRAFT
INSPECTION OF WIRE BUNDLE FOR CHAFING AT F.S.457, C-130B/E/H, HC-130H/N/P, WC-130E/H, AND AC-130H AIRCRAFT
INSPECTION OF WIRE BUNDLE INUPPER MAIN AC POWER PANEL, F.S.245, C-130 AIRCRAFT
INSTALLATION OF NUTPLATES ONK-6A GYRO MOUNTING PLATE, C-130 AIRCRAFT
INSTALLATION OF NUTPLATES ONK-6A GYRO MOUNTING PLATE, C-130 AIRCRAFT
INSPECTION FOR INSTALLATION OF HEAT DEFLECTOR TUBE SUPPORTS, C-130 AIRCRAFT
INSPECTION FOR INSTALLATION OF HEAT DEFLECTOR TUBE SUPPORTS, C-130 AIRCRAFT
ONE-TIME INSPECTION OF NACELLE FUEL SUPPLY HOSE ASSEMBLY, C-130B AIRCRAFT, SERIAL NO.57-525, THROUGH C-130H AIRCRAFT, SERIAL ...
INSPECTION OF FLAP POSITION TRANSMITTER, C-130 AIRCRAFT
INSPECTION OF FLAP POSITION TRANSMITTER, C-130 AIRCRAFT
INSPECTION OF FLAP POSITION TRANSMITTER, C-130 AIRCRAFT
CHANGE-OVER OF MIL-H-5606 HYDRAULIC FLUID TO MIL-H-83282 SYNTHETIC HYDRAULIC FLUID, C-130 AIRCRAFT
CHANGE-OVER OF MIL-H-5606 HYDRAULIC FLUID TO MIL-H-83282 SYNTHETIC HYDRAULIC
TÍTULO
18/04/1980
20/05/1980
20/05/1980
04/04/1980
20/12/1980
20/12/1980
20/02/1981
20/02/1981
17/11/1980
02/02/1981
02/02/1981
02/02/1981
03/02/1981
03/02/1981
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
M
R
R
M
M
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
11/02/1981
20/06/1980
28/08/1981
13/11/1981
26/08/1981
30/09/1981
13/04/1981
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
67Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1053
TCTO 1C-130-1060
TCTO 1C-130-1072
TCTO 1C-130-1072
TCTO 1C-130-1074
TCTO 1C-130-1074
TCTO 1C-130-1080
TCTO 1C-130-1082
TCTO 1C-130-1084
TCTO 1C-130-1084
TCTO 1C-130-1084
TCTO 1C-130-1084
TCTO 1C-130-1084
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
BSC
SPL
BSC
REV
BSC
BSC
SPL
BSC
SPL
SPL
SPL
NAT.
D
0
0
C
0
C
0
0
H
0
C
D
E
ORDEM
GLA329A030040100
GLA332S810001500
GLA327A810001200
GLA327A030040200
GLA332S820002000
GLA332S810001701
GLA335A820003100
GLA326A820001200
GLA395A850003405
GLA395A840008900
GLA395A840008401
GLA395A850002902
GLA395A850003103
FADT
FLUID, C-130 AIRCRAFT
CHANGE-OVER OF MIL-H-5606 HYDRAULIC FLUID TO MIL-H-83282 SYNTHETIC HYDRAULIC FLUID, C-130 AIRCRAFT
INSPECTION OF MAIN LANDING GEAR EMERGENCY EXTENSION MITER GEAR BOX, PART NO.355390-1, 355390-2 AND 355390-501, FOR INSTALLATION...
INSPECTION OF RUDDER, AILERON, AND ELEVATOR BOOST AND UTILITY CUT-OFF VALVE CONNECTORS, C-130 AIRCRAFT
INSPECTION OF RUDDER, AILERON, AND ELEVATOR BOOST AND UTILITY CUT-OFF VALVE CONNECTORS, C-130 AIRCRAFT
IMPROVEMENT OF BALL SCREW RELIABILITY, CALCO, PART NO.8353 AND 8430 - C-130 AIRCRAFT
IMPROVEMENT OF BALL SCREW RELIABILITY, CALCO, PART NO.8353 AND 8430 - C-130 AIRCRAFT
INSPECTION FOR INTERFERENCE BETWEEN PORTABLE OXYGEN BOTTLE FILLER HOSES AND SIDECIRCUIT BREAKER PANELS, C-130 AIRCRAFT
INSPECTION FOR AIRCRAFT FIREEXTINGUISHER TUBE BLOCKAGE, C-130 AIRCRAFT.
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
TÍTULO
03/02/1981
15/05/1981
11/09/1981
11/09/1981
09/10/1981
09/10/1981
08/01/1982
29/01/1982
28/10/1983
28/10/1983
28/10/1983
28/10/1983
28/10/1983
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
M
M
M
M
M
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
13/11/1981
03/11/1981
13/10/1991
04/04/1988
27/01/1984
12/04/1985
17/05/1985
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
68Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1084
TCTO 1C-130-1084
TCTO 1C-130-1091
TCTO 1C-130-1091
TCTO 1C-130-1091
TCTO 1C-130-1092
TCTO 1C-130-1092
TCTO 1C-130-1092
TCTO 1C-130-1096
TCTO 1C-130-1097
TCTO 1C-130-1100
TCTO 1C-130-1100
TCTO 1C-130-1100
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
BSC
SPL
SPL
BSC
SPL
SPL
BSC
BSC
BSC
SPL
SPL
NAT.
G
J
0
C
D
0
C
D
0
0
0
C
D
ORDEM
GLA395A880003904
GLA395A880004106
GLA327A830002100
GLA327A030040400
GLA327A030040500
GLA372S820004400
GLA372S820004201
GLA372S820004502
GLA357A820000500
GLA332A820001800
GLA357A030040600
GLA357A830005002
GLA357A830004103
FADT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REWORK OF LIFE RAFT COMPARTMENT C-130 AIRCRAFT
REPLACEMENT OF CONNECTORS ONBOOST AND UTILITY CUT-OFF VALVES, C-130 AIRCRAFT
REPLACEMENT OF CONNECTORS ONBOOST AND UTILITY CUT-OFF VALVES, C-130 AIRCRAFT
REPLACEMENT OF CONNECTORS ONBOOST AND UTILITY CUT-OFF VALVES, C-130 AIRCRAFT
INSPECTION OF REAR ENGINE MOUNTS, PART NO.LM200SA14 AND LM200SA15, AND SPARE T56ENGINE POWER PACKAGES, C-130AIRCRAFT
INSPECTION OF REAR ENGINE MOUNTS, PART NO.LM200SA14 AND LM200SA15, AND SPARE T56ENGINE POWER PACKAGES, C-130AIRCRAFT
INSPECTION OF REAR ENGINE MOUNTS, PART NO.LM200SA14 AND LM200SA15, AND SPARE T56ENGINE POWER PACKAGES, C-130AIRCRAFT
INSPECTION OF OUTER WING DRAIN HOLES, O.W.S.176 AND O.W.S.208, C-130 AIRCRAFT
INSPECTION OF 100 CUBIC INCHHYDRAULIC ACCUMULATORS, PARKER-HANNIFIN PART NO.1356-583317, INSTALLED INNOSE LANDING GEAR WHEEL ...
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
TÍTULO
28/10/1983
28/10/1983
01/06/1983
01/06/1983
01/06/1983
11/05/1982
11/05/1982
11/05/1982
21/05/1982
21/06/1982
20/12/1982
20/12/1982
20/12/1982
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
I
I
I
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/08/1987
31/08/1988
09/08/1983
11/05/1984
14/05/1982
12/08/1988
14/01/1983
26/01/1983
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
69Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1100
TCTO 1C-130-1100
TCTO 1C-130-1100
TCTO 1C-130-1100
TCTO 1C-130-1112
TCTO 1C-130-1112
TCTO 1C-130-1113
TCTO 1C-130-1113
TCTO 1C-130-1113
TCTO 1C-130-1113
TCTO 1C-130-1113
TCTO 1C-130-1113
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
SPL
SPL
BSC
SPL
BSC
SPL
SPL
SPL
SPL
SPL
NAT.
E
F
G
H
0
C
0
C
D
F
G
H
ORDEM
GLA357A030040700
GLA357A030040800
GLA357A840009503
GLA357A030040900
GLA324A830001400
GLA324A030041200
GLA357A830004200
GLA357A830004700
GLA357A030041300
GLA357A840009202
GLA357A860002303
GLA357A030041400
FADT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF WING ATTACH ANGLE AND VERTICAL BEAMS, C-130 AIRCRAFT
INSPECTION OF AC GENERATOR LEADS AND CIRCUIT BREAKERS, C-130 AIRCRAFT
INSPECTION OF AC GENERATOR LEADS AND CIRCUIT BREAKERS, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDEFUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDEFUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDEFUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDEFUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDEFUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF LOWER SURFACE BEAM CAPS AND PANELS, INSIDE
TÍTULO
20/12/1982
20/12/1982
20/12/1982
20/12/1982
15/12/1982
15/12/1982
01/11/1982
01/11/1982
01/11/1982
01/11/1982
01/11/1982
01/11/1982
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
07/06/1983
20/09/1983
20/01/1984
18/05/1984
18/01/1983
15/11/1982
31/01/1983
05/03/1984
24/06/1986
05/09/1986
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
70Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1116
TCTO 1C-130-1116
TCTO 1C-130-1123
TCTO 1C-130-1124
TCTO 1C-130-1126
TCTO 1C-130-1127
TCTO 1C-130-1127
TCTO 1C-130-1129
TCTO 1C-130-1129
TCTO 1C-130-1130
TCTO 1C-130-1130
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
BSC
BSC
BSC
BSC
SPL
BSC
SPL
BSC
SPL
NAT.
0
C
0
0
0
0
D
0
C
0
C
ORDEM
GLA371A830003500
GLA371A830003601
GLA330A830002700
GLA352A830004400
GLA327A830002200
GLA335A830004800
GLA335A840009302
GLA329A830002600
GLA329A030041700
GLA324A840000600
GLA324A030041800
FADT
FUEL TANKS, OWS 0 TO 144 ANDOWS 212 TO 360, C-130 AIRCRAFT
INSPECTION OF ATTACHING HARDWARE FOR ENGINE MOUNT TRUSS TO WING, C-130 AIRCRAFT
INSPECTION OF ATTACHING HARDWARE FOR ENGINE MOUNT TRUSS TO WING, C-130 AIRCRAFT
INSPECTION OF NESA WINDSHIELD POWER STUD INSTALLATION FOR MISSING PARTS AND INSTALLATION OF IMPROPER HARDWARE, C-130 AIRCRAFT
INSPECTION OF PARATROOP DOORLONGERON FITTINGS AND DOOR SILL DRAIN HOLES C-130 AIRCRAF
INSPECTION OF ELEVATOR TORQUE TUBE COLLAR ATTACHINGHARDWARE, C-130 AIRCRAFT
INSTALLATION OF PINS IN OXYGEN BOTTLE BRACKET STRAPS, C-130 AIRCRAFT
INSTALLATION OF PINS IN OXYGEN BOTTLE BRACKET STRAPS, C-130 AIRCRAFT
INSPECTION OF 25-AND 50-CUBIC INCH HYDRAULIC SYSTEM ACCUMULATORS, PART NO.1356-583314 AND 1356-583315, FOR CRACKED/CORRODED END...
INSPECTION OF 25-AND 50-CUBIC INCH HYDRAULIC SYSTEM ACCUMULATORS, PART NO.1356-583314 AND 1356-583315, FOR CRACKED/CORRODED END...
INSPECTION OF MAIN AC BUS OFF INDICATOR RELAY WIRING C-130 AIRCRAFT
INSPECTION OF MAIN AC BUS OFF INDICATOR RELAY WIRING
TÍTULO
22/12/1982
22/12/1982
16/03/1983
25/01/1988
21/04/1983
13/12/1985
26/08/1983
28/04/1983
28/04/1983
27/02/1984
27/02/1984
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
M
R
R
M
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
18/02/1983
30/11/1983
26/01/1984
15/11/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
71Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1133
TCTO 1C-130-1133
TCTO 1C-130-1133
TCTO 1C-130-1133
TCTO 1C-130-1134
TCTO 1C-130-1134
TCTO 1C-130-1134
TCTO 1C-130-1134
TCTO 1C-130-1146
TCTO 1C-130-1146
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
SPL
SPL
SPL
SPL
SPL
SPL
BSC
SPL
NAT.
0
C
D
E
E
F
G
H
0
C
ORDEM
GLA327A840001500
GLA327A030041900
GLA327A030042000
GLA327A030042100
GLA321A830005101
GLA321A830005202
GLA321A850003803
GLA321A830001106
GLA372S830000100
GLA372S840006501
FADT
C-130 AIRCRAFT
REPLACEMENT OF RUDDER PEDAL NEUTRAL POSITION ADJUSTER ASSEMBLY RETAINER NUTS C-130AIRCRAFT
REPLACEMENT OF RUDDER PEDAL NEUTRAL POSITION ADJUSTER ASSEMBLY RETAINER NUTS C-130AIRCRAFT
REPLACEMENT OF RUDDER PEDAL NEUTRAL POSITION ADJUSTER ASSEMBLY RETAINER NUTS C-130AIRCRAFT
REPLACEMENT OF RUDDER PEDAL NEUTRAL POSITION ADJUSTER ASSEMBLY RETAINER NUTS C-130AIRCRAFT
INSPECTION OF CARGO COMPARTMENT UNDER FLOOR HEATCONTROL VALVE FOR INTERFERENCE WITH HYDRAULIC LINES, C-130 AIRCRAFT
INSPECTION OF CARGO COMPARTMENT UNDER FLOOR HEATCONTROL VALVE FOR INTERFERENCE WITH HYDRAULIC LINES, C-130 AIRCRAFT
INSPECTION OF CARGO COMPARTMENT UNDER FLOOR HEATCONTROL VALVE FOR INTERFERENCE WITH HYDRAULIC LINES, C-130 AIRCRAFT
INSPECTION OF CARGO COMPARTMENT UNDER FLOOR HEATCONTROL VALVE FOR INTERFERENCE WITH HYDRAULIC LINES, C-130 AIRCRAFT
INSPECTION OF AFT ENGINE MOUNT BEAM P/N 363803-1, AFTENGINE MOUNT BEAM SUPPORT P/N 363801-1, AND UPPER LONGERONS P/N 362502 ...
INSPECTION OF AFT ENGINE MOUNT BEAM P/N 363803-1, AFTENGINE MOUNT BEAM SUPPORT
TÍTULO
30/10/1983
30/10/1983
30/10/1983
30/10/1983
06/04/1984
06/04/1984
06/04/1984
06/04/1984
31/10/1983
31/10/1983
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/12/1983
08/02/1984
20/04/1984
28/06/1984
19/07/1984
19/10/1984
06/09/1985
23/11/1983
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
72Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1146
TCTO 1C-130-1161
TCTO 1C-130-1161
TCTO 1C-130-1161
TCTO 1C-130-1162
TCTO 1C-130-1171
TCTO 1C-130-1171
TCTO 1C-130-1174
TCTO 1C-130-1174
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
SPL
SPL
BSC
BSC
SPL
BSC
SPL
NAT.
D
0
C
D
0
0
C
0
C
ORDEM
GLA372S840006702
GLA325A840001300
GLA325A030043700
GLA325A030043800
GLA376A840008100
GLA332S860001600
GLA332S860001401
GLA329A840002400
GLA329S030043900
FADT
P/N 363801-1, AND UPPER LONGERONS P/N 362502 ...
INSPECTION OF AFT ENGINE MOUNT BEAM P/N 363803-1, AFTENGINE MOUNT BEAM SUPPORT P/N 363801-1, AND UPPER LONGERONS P/N 362502 ...
INSPECTION OF STATIC LINA ATTACHING TURNBUCKLE BARREL,PART NO.MS21251B10L FOR CONDITION OF INTERNAL THREADS, C-130 AIRCRAFT
INSPECTION OF STATIC LINA ATTACHING TURNBUCKLE BARREL,PART NO.MS21251B10L FOR CONDITION OF INTERNAL THREADS, C-130 AIRCRAFT
INSPECTION OF STATIC LINA ATTACHING TURNBUCKLE BARREL,PART NO.MS21251B10L FOR CONDITION OF INTERNAL THREADS, C-130 AIRCRAFT
INSPECTION OF ENGINE CONTROLCABLE, PART NO.363905-8, FORLOOSE ENDS
INSPECTION OF CYLINDER HEADSON THE NOSE LANDING GEAR UPLOCK ASSEMBLIES, PART N.358800-1 AND -5,C-130 AIRCRAFT (ALL SERIES/MODELS)
INSPECTION OF CYLINDER HEADSON THE NOSE LANDING GEAR UPLOCK ASSEMBLIES, PART N.358800-1 AND -5,C-130 AIRCRAFT (ALL SERIES/MODELS)
INSPECTION OF YORK 100- AND 50-CUBIC INCH ACCUMULATORS INSTALLED IN NOSE LANDING GEAR WHEEL WELL, C-130 AIRCRAFT
INSPECTION OF YORK 100- AND 50-CUBIC INCH ACCUMULATORS INSTALLED IN NOSE LANDING GEAR WHEEL WELL, C-130 AIRCRAFT
TÍTULO
31/10/1983
13/02/1984
13/02/1984
13/02/1984
15/02/1984
15/01/1985
15/01/1985
10/07/1984
10/07/1984
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
20/12/1983
18/05/1984
10/05/1985
21/10/1985
07/08/1984
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
73Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1175
TCTO 1C-130-1177
TCTO 1C-130-1177
TCTO 1C-130-1177
TCTO 1C-130-1177
TCTO 1C-130-1177
TCTO 1C-130-1183
TCTO 1C-130-1183
TCTO 1C-130-1186
TCTO 1C-130-1193
TCTO 1C-130-1193
TCTO 1C-130-1193
TCTO 1C-130-1193
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
SPL
SPL
SPL
SPL
BSC
SPL
BSC
BSC
SPL
SPL
SPL
NAT.
0
0
C
D
E
F
0
C
0
0
C
D
E
ORDEM
GLA327A840001600
GLA325A890000600
GLA325A890000101
GLA325A880000104
GLA325S890000205
GLA325A900000205
GLA327A850000700
GLA327A030044000
GLA325A850000100
GLA324A880000900
GLA324A880004601
GLA324A880004702
GLA324A880004803
FADT
INSPECTION OF ELEVATOR UPPERAND LOWER SPAR CAPS AND HINGE PIN AREA, ELEVATOR STATION 296, FOR CRACKS, C-130 AIRCRAFT
INSTALLATION OF PARACHUTE STATIC LINE RETRIEVER WINCH LIMITER
INSTALLATION OF PARACHUTE STATIC LINE RETRIEVER WINCH LIMITER
INSTALLATION OF PARACHUTE STATIC LINE RETRIEVER WINCH LIMITER
INSTALLATION OF PARACHUTE STATIC LINE RETRIEVER WINCH LIMITER
INSTALLATION OF PARACHUTE STATIC LINE RETRIEVER WINCH LIMITER
INSPECTION OF AILERON BOOSTER ACTUATING LEVER, PART NO.343863
INSPECTION OF AILERON BOOSTER ACTUATING LEVER, PART NO.343863
INSPECTION OF LIFE RAFT RIGGING ON C-130
INSPECTION OF AUXILIARY TANKDUMP INTERLOCK RELAYS, PART NO.MS24149D1, MS24568D1, MS25024-2, AND AN3311-2, FORCORROSION, ...
INSPECTION OF AUXILIARY TANKDUMP INTERLOCK RELAYS, PART NO.MS24149D1, MS24568D1, MS25024-2, AND AN3311-2, FORCORROSION, ...
INSPECTION OF AUXILIARY TANKDUMP INTERLOCK RELAYS, PART NO.MS24149D1, MS24568D1, MS25024-2, AND AN3311-2, FORCORROSION, ...
INSPECTION OF AUXILIARY TANKDUMP INTERLOCK RELAYS, PART
TÍTULO
27/06/1984
31/08/1987
31/08/1987
31/08/1987
31/08/1987
31/08/1987
09/10/1984
09/10/1984
27/11/1984
30/10/1987
30/10/1987
30/10/1987
30/10/1987
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
26/01/1988
13/05/1988
01/06/1989
30/10/1989
31/10/1984
26/01/1988
23/03/1988
20/04/1988
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
74Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1214
TCTO 1C-130-1214
TCTO 1C-130-1214
TCTO 1C-130-1217
TCTO 1C-130-1217
TCTO 1C-130-1221
TCTO 1C-130-1221
TCTO 1C-130-1222
TCTO 1C-130-1222
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
SPL
BSC
REV
BSC
SPL
BSC
SPL
NAT.
0
C
D
0
C
0
C
0
E
ORDEM
GLA325A850000500
GLA325A860003301
GLA325A860003402
GLA328A870000500
GLA328A870000601
GLA327A860000900
GLA327A030016700
GLA327A850000800
GLA327A030016800
FADT
NO.MS24149D1, MS24568D1, MS25024-2, AND AN3311-2, FORCORROSION, ...
INSPECTION FOR AND REPLACEMENT OF BRASS STATIC LINE ATTACHING TURNBUCKLE BARRELS, PART NO.MS21251B10L, C-130 AIRCRAFT
INSPECTION FOR AND REPLACEMENT OF BRASS STATIC LINE ATTACHING TURNBUCKLE BARRELS, PART NO.MS21251B10L, C-130 AIRCRAFT
INSPECTION FOR AND REPLACEMENT OF BRASS STATIC LINE ATTACHING TURNBUCKLE BARRELS, PART NO.MS21251B10L, C-130 AIRCRAFT
INSPECTION OF SINGLE POINT REFUELING (SPR) ADAPTER, PART NO.MS24484-2, CONTRACT NUMBERS F09603-78-G-0292 ANDF00603-83-D-0661-001,
INSPECTION OF SINGLE POINT REFUELING (SPR) ADAPTER, PART NO.MS24484-2, CONTRACT NUMBERS F09603-78-G-0292 ANDF00603-83-D-0661-001,
INSPECTION OF ELEVATOR BOOSTER ASSEMBLIES FOR PISTON ROD END LOOSENESS, C-130 AIRCRAFT
INSPECTION OF ELEVATOR BOOSTER ASSEMBLIES FOR PISTON ROD END LOOSENESS, C-130 AIRCRAFT
INSPECTION OF AILERON AND RUDDER BOOSTER ASSEMBLIES FOR PINSTON ROD END LOOSENESS C-130 AIRCRAFT
INSPECTION OF AILERON AND RUDDER BOOSTER ASSEMBLIES
TÍTULO
18/07/1985
18/07/1985
18/07/1985
30/10/1986
30/10/1986
19/08/1985
19/08/1985
03/09/1985
30/09/1985
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
R
M
M
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
23/04/1986
24/06/1986
28/01/1987
26/09/1985
30/10/1985
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
75Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1229
TCTO 1C-130-1229
TCTO 1C-130-1229
TCTO 1C-130-1229
TCTO 1C-130-1229
TCTO 1C-130-1243
TCTO 1C-130-1244
TCTO 1C-130-1244
TCTO 1C-130-1246
TCTO 1C-130-1246
TCTO 1C-130-1246
TCTO 1C-130-1248
TCTO 1C-130-1248
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
SPL
SPL
SPL
BSC
BSC
SPL
BSC
SPL
SPL
BSC
SPL
NAT.
0
C
E
F
G
0
0
C
0
D
E
0
C
ORDEM
GLA328A880000800
GLA328A030044500
GLA328A890000800
GLA328A030044600
GLA328A030044400
GLA323A870000700
GLA326A870000800
GLA326A030044700
GLA356A860002000
GLA356A870001402
GLA356A030044800
GLA327A860001000
GLA327A030044900
FADT
FOR PINSTON ROD END LOOSENESS C-130 AIRCRAFT
INSTALLATION OF OUTER WING FUEL TANK AUXILIARY VENT VALVE, PART NO.12F135, C-130AIRCRAFT
INSTALLATION OF OUTER WING FUEL TANK AUXILIARY VENT VALVE, PART NO.12F135, C-130AIRCRAFT
INSTALLATION OF OUTER WING FUEL TANK AUXILIARY VENT VALVE, PART NO.12F135, C-130AIRCRAFT
INSTALLATION OF OUTER WING FUEL TANK AUXILIARY VENT VALVE, PART NO.12F135, C-130AIRCRAFT
INSTALLATION OF OUTER WING FUEL TANK AUXILIARY VENT VALVE, PART NO.12F135, C-130AIRCRAFT
INSPECTION OF INTERPHONE SYSTEM (AIC-10/-18A/-25) TO CORRECT MISSING OR OPEN GROUND WIRES, C-130 AIRCRAFT
INSPECTION OF TURBINE OVERHEAT WARNING SYSTEM WIRING C-130 AIRCRAFT
INSPECTION OF TURBINE OVERHEAT WARNING SYSTEM WIRING C-130 AIRCRAFT
INSPECTION FOR CORROSION IN NESA-EQUIPPED WINDSHIELDS AND WINDOWS, C-130 AIRCRAFT
INSPECTION FOR CORROSION IN NESA-EQUIPPED WINDSHIELDS AND WINDOWS, C-130 AIRCRAFT
INSPECTION FOR CORROSION IN NESA-EQUIPPED WINDSHIELDS AND WINDOWS, C-130 AIRCRAFT
INSPECTION OF AILERON TRIM TAB WIRE FOR CHAFING, C-130 AIRCRAFT
INSPECTION OF AILERON TRIM
TÍTULO
29/07/1988
29/07/1988
29/07/1988
29/07/1988
29/07/1988
24/12/1986
02/10/1986
02/10/1986
06/06/1986
06/06/1986
06/06/1986
09/07/1986
09/07/1986
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
R
R
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
18/04/1989
11/05/1989
09/04/1990
16/05/1991
08/12/1986
09/03/1987
31/07/1987
27/03/1987
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
76Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1248
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1256
TCTO 1C-130-1268
TCTO 1C-130-1268
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
SPL
SPL
SPL
SPL
REV
SPL
SPL
SPL
BSC
SPL
NAT.
D
0
C
D
E
F
G
H
J
L
0
E
ORDEM
GLA327A030045000
GLA357A960001801
GLA200X960000100
GLA300S020000900
GLA357A900006902
GLA357A030045400
GLA357A030045300
GLA357A030045500
GLA300S020000800
GLA300S020001000
GLA356A880002500
GLA356A030045700
FADT
TAB WIRE FOR CHAFING, C-130 AIRCRAFT
INSPECTION OF AILERON TRIM TAB WIRE FOR CHAFING, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
REMOVAL OF DOUBLERS FROM CENTER WING LOWER SURFACE CWS 62 TO CWS 68, C-130 AIRCRAFT
INSPECTION OF AIRCRAFT WINDSHIELDS FOR MISSING SPACERS, C-130 AIRCRAFT
INSPECTION OF AIRCRAFT
TÍTULO
09/07/1986
09/04/1987
09/04/1987
09/04/1987
09/04/1987
09/04/1987
09/04/1987
09/04/1987
09/04/1987
09/04/1987
29/09/1987
29/09/1987
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
R
I
I
I
R
I
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/09/1987
04/05/1987
22/08/1988
06/10/1989
30/01/1990
30/11/1990
27/03/1991
15/12/1992
20/01/1999
11/08/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
77Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1277
TCTO 1C-130-1281
TCTO 1C-130-1281
TCTO 1C-130-1281
TCTO 1C-130-1281
TCTO 1C-130-1281
TCTO 1C-130-1283
TCTO 1C-130-1285
TCTO 1C-130-1288
TCTO 1C-130-1288
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
SPL
SPL
SPL
SPL
BSC
BSC
BSC
SPL
NAT.
0
0
D
E
F
G
0
0
0
C
ORDEM
GLA355A880002700
GLA324A880001000
GLA324A030045800
GLA324A030045900
GLA324A030046000
GLA324A030046100
GLA327A950001300
GLA324A880000700
GLA327A900000400
GLA327A030046200
FADT
WINDSHIELDS FOR MISSING SPACERS, C-130 AIRCRAFT
INSPECTION OF HORIZONTAL STABILIZER FRONT BEAM UPPER AND LOWER CAP FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF AC GENERATING SYSTEM/FOUR ENGINE PARTIAL POWER ROLL BACK, C-130 AIRCRAFT
INSPECTION OF AC GENERATING SYSTEM/FOUR ENGINE PARTIAL POWER ROLL BACK, C-130 AIRCRAFT
INSPECTION OF AC GENERATING SYSTEM/FOUR ENGINE PARTIAL POWER ROLL BACK, C-130 AIRCRAFT
INSPECTION OF AC GENERATING SYSTEM/FOUR ENGINE PARTIAL POWER ROLL BACK, C-130 AIRCRAFT
INSPECTION OF AC GENERATING SYSTEM/FOUR ENGINE PARTIAL POWER ROLL BACK, C-130 AIRCRAFT
INSPECTION FOR EVIDENCE OF INTERFERENCE BETWEEN AILERONBOOSTER QUADRANT CABLE CLIP,PART NO.344997-3, AND AILERON BOOSTER ...
INSPECTION OF FLIGHT STATIONCIRCUIT BREAKERS FOR CHAFINGOF ELECTRICAL WIRING HARNESSAND CABLE CLAMPS, C-130 AIRCRAFT
INSPECTION OF CENTER AND OUTER WING FLAP CONNECTING LINK TUBE ASSEMBLIES, LEFT AND RIGHT, PART NO.340188-5 AND 340188-6, C-130 ...
INSPECTION OF CENTER AND OUTER WING FLAP CONNECTING LINK TUBE ASSEMBLIES, LEFT AND RIGHT, PART NO.340188-5
TÍTULO
15/11/1987
04/06/1987
04/06/1987
04/06/1987
04/06/1988
04/06/1987
01/07/1987
22/07/1987
06/03/1989
06/03/1989
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
02/07/1987
07/07/1987
10/08/1987
23/02/1988
23/08/1990
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
78Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1288
TCTO 1C-130-1288
TCTO 1C-130-1289
TCTO 1C-130-1289
TCTO 1C-130-1299
TCTO 1C-130-1299
TCTO 1C-130-1300
TCTO 1C-130-1300
TCTO 1C-130-1300
TCTO 1C-130-1315
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
BSC
SPL
BSC
SPL
BSC
SPL
SPL
BSC
NAT.
D
F
0
C
0
C
0
D
E
0
ORDEM
GLA327A900008502
GLA327A900008603
GLA372S880000400
GLA372S880000500
GLA327A880000600
GLA327A880004901
GLA353A880004200
GLA353A030046300
GLA353A030046400
GLA372S910004600
FADT
AND 340188-6, C-130 ...
INSPECTION OF CENTER AND OUTER WING FLAP CONNECTING LINK TUBE ASSEMBLIES, LEFT AND RIGHT, PART NO.340188-5 AND 340188-6, C-130 ...
INSPECTION OF CENTER AND OUTER WING FLAP CONNECTING LINK TUBE ASSEMBLIES, LEFT AND RIGHT, PART NO.340188-5 AND 340188-6, C-130 ...
INSPECTION OF FIRE EXTINGUISHER LINE, PART NO.363800-155, FOR CORRECT POSITION OF DISCHARGE HOLES,C-130 AIRCRAFT
INSPECTION OF FIRE EXTINGUISHER LINE, PART NO.363800-155, FOR CORRECT POSITION OF DISCHARGE HOLES,C-130 AIRCRAFT
INSPECTION FOR SAGGING AND IMPROPER CLAMPING OF WIRE BUNDLE (LOCATED APPROXIMATELY FS 1050) AT BOTTOM OF STRINGER DIRECTLY ...
INSPECTION FOR SAGGING AND IMPROPER CLAMPING OF WIRE BUNDLE (LOCATED APPROXIMATELY FS 1050) AT BOTTOM OF STRINGER DIRECTLY ...
INSPECTION OF LONGERON END FITTING F.S.737, BL 61.62 FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF LONGERON END FITTING F.S.737, BL 61.62 FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF LONGERON END FITTING F.S.737, BL 61.62 FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130
TÍTULO
06/03/1989
06/03/1989
15/12/1987
15/12/1987
03/11/1987
03/11/1987
05/02/1908
05/02/1988
05/02/1988
21/11/1990
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
26/03/1991
30/07/1992
15/03/1988
17/08/1988
16/12/1988
14/03/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
79Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1315
TCTO 1C-130-1316
TCTO 1C-130-1324
TCTO 1C-130-1328
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
SPL
SPL
SPL
SPL
SPL
SPL
BSC
BSC
BSC
NAT.
C
D
E
F
G
H
J
K
0
0
0
ORDEM
GLA372S030047100
GLA372S910004702
GLA372S910004803
GLA372S910004904
GLA372S910005005
GLA372S910005106
GLA372S910005207
GLA372S910005308
GLA326A880001200
GLA327A890001100
GLA357A910006400
FADT
AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF HEAT SENSING ELEMENTS FOR CHAFING AND INCORRECT ROUTING, ON C-130 AIRCRAFT
INSPECTION OF FIRE CONTROL "T" HANDLE SWITCH, P/N G56845-1, FOR LOOSE OR MISSING SCREWS, ALL C-130 AIRCRAFT
INSPECTION OF FLAP POSITION TRANSMITTER, PART NO.EA573A1, FOR SERIAL NUMBER 8398G THROUGH 8453G AND 8491G THROUGH 8584G, C-130 ...
INSPECTION OF CENTER WING
TÍTULO
21/11/1990
21/11/1990
21/11/1990
21/11/1990
21/11/1990
21/11/1990
21/11/1990
21/11/1990
14/09/1989
24/02/1989
03/08/1989
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/04/1991
09/04/1991
31/08/1991
20/04/1992
15/04/1993
31/08/1993
28/10/1994
28/10/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
80Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1328
TCTO 1C-130-1328
TCTO 1C-130-1328
TCTO 1C-130-1333
TCTO 1C-130-1333
TCTO 1C-130-1333
TCTO 1C-130-1333
TCTO 1C-130-1333H
TCTO 1C-130-1335
TCTO 1C-130-1335
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
SPL
BSC
SPL
SPL
SPL
SPL
BSC
SPL
NAT.
C
E
F
0
C
G
H
0
0
D
ORDEM
GLA357A030047800
GLA357A030047900
GLTT00X960006400
GLA324A030048000
GLA324A030048100
GLA324A030048200
GLA324A030048300
GLTT34A910000101
GLA336A940000800
GLTT36A990000101
FADT
LOWER FORWARD BEAM CAP, CWS 61-214, FOR FATIGUE CRACKS FROM FASTENER HOLES IN HORIZONTAL AND VERTICAL...
INSPECTION OF CENTER WING LOWER FORWARD BEAM CAP, CWS 61-214, FOR FATIGUE CRACKS FROM FASTENER HOLES IN HORIZONTAL AND VERTICAL...
INSPECTION OF CENTER WING LOWER FORWARD BEAM CAP, CWS 61-214, FOR FATIGUE CRACKS FROM FASTENER HOLES IN HORIZONTAL AND VERTICAL...
INSPECTION OF CENTER WING LOWER FORWARD BEAM CAP, CWS 61-214, FOR FATIGUE CRACKS FROM FASTENER HOLES IN HORIZONTAL AND VERTICAL...
INSTALLATION OF DUAL POWER SOURCE FOR ADI AC/EC/HC/JC/MC/NC/WC/C-130B/E/H/ AIRCRAFT
INSTALLATION OF DUAL POWER SOURCE FOR ADI AC/EC/HC/JC/MC/NC/WC/C-130B/E/H/ AIRCRAFT
INSTALLATION OF DUAL POWER SOURCE FOR ADI AC/EC/HC/JC/MC/NC/WC/C-130B/E/H/ AIRCRAFT
INSTALLATION OF DUAL POWER SOURCE FOR ADI AC/EC/HC/JC/MC/NC/WC/C-130B/E/H/ AIRCRAFT
INSTALLATION OF DUAL POWER SOURCE FOR ADI AC/EC/HC/JC/MC/NC/WC/C-130B/E/H/AIRCRAFT
INSPECTION AND INSTALLATION ANTI-ICING CONTROL VALVE P/N3290290-1 C-130 AIRCRAFT
INSPECTION AND INSTALLATION ANTI-ICING CONTROL VALVE P/N3290290-1 C-130 AIRCRAFT
TÍTULO
03/08/1989
03/08/1989
03/08/1989
02/02/1990
02/02/1990
02/02/1990
02/02/1990
02/02/1990
15/10/1992
15/10/1992
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
R
R
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
27/12/1990
20/04/1994
01/11/1994
29/06/1990
15/04/1991
15/08/1991
15/08/1991
30/06/1993
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL REMOTO
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
81Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1335
TCTO 1C-130-1335
TCTO 1C-130-1335
TCTO 1C-130-1338
TCTO 1C-130-1347
TCTO 1C-130-1351
TCTO 1C-130-1352
TCTO 1C-130-1352
TCTO 1C-130-1352
TCTO 1C-130-1353
TCTO 1C-130-1353
TCTO 1C-130-1359
TCTO 1C-130-1369
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
SPL
SPL
BSC
SPL
BSC
SPL
SPL
BSC
SPL
BSC
BSC
NAT.
E
F
G
F
0
D
0
C
D
0
C
0
0
ORDEM
GLA336A030048400
GLA336A030048500
GLA336A030048600
GLA332A940001901
GLA361A910013701
GLA372S950002801
GLA327A910001300
GLA327A910006701
GLA327A910006802
GLA331A910000700
GLA331A910015001
GLA361S910002901
GLA353A910006691
FADT
INSPECTION AND INSTALLATION ANTI-ICING CONTROL VALVE P/N3290290-1 C-130 AIRCRAFT
INSPECTION AND INSTALLATION ANTI-ICING CONTROL VALVE P/N3290290-1 C-130 AIRCRAFT
INSPECTION AND INSTALLATION ANTI-ICING CONTROL VALVE P/N3290290-1 C-130 AIRCRAFT
INSPECTION FOR INSTALLATION OF MAIN LANDING GEAR (MLG) SPLASH GUARDS, PART NO.3630008 C-130 AIRCRAFT
INSPECTION OF SOLID STATE SYNCHROPHASER AND ADAPTER, PART NO.774800-1, C-130B ANDSEBSEQUENT AIRCRAFT
INSPECTION AND REPLACEMENT OF STERER OIL SHUTOFF VALVE P/N 53230-1 WITH WHITTAKER OIL SHUTOFF VALVE P/N 132555-1 ON C-130 AIRCRAFT
INSPECTION FOR THE REMOVAL OF MAGNESIUM CASTING AILERONIDLER BELLCRANKS, P/N 339003, ON C-130 AIRCRAFT
INSPECTION FOR THE REMOVAL OF MAGNESIUM CASTING AILERONIDLER BELLCRANKS, P/N 339003, ON C-130 AIRCRAFT
INSPECTION FOR THE REMOVAL OF MAGNESIUM CASTING AILERONIDLER BELLCRANKS, P/N 339003, ON C-130 AIRCRAFT
INSPECTION OF ALL ELECTRONICTEST RECEPTACLES ON C-130B/E/H AIRCRAFT
INSPECTION OF ALL ELECTRONICTEST RECEPTACLES ON C-130B/E/H AIRCRAFT
INSPECTION OF CERTAIN HIGH TIME AIRCRAFT PROPELLERS, C-130 AIRCRAFT
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS
TÍTULO
15/10/1992
15/10/1992
15/10/1992
01/01/1993
22/06/1990
15/06/1993
16/07/1990
16/07/1990
16/07/1990
29/05/1990
29/05/1990
20/06/1990
31/03/1991
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
R
R
M
M
M
R
R
I
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/06/1994
30/06/1995
15/10/1997
30/09/1993
20/05/1994
10/03/1991
06/05/1991
15/03/1991
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
82Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1369
TCTO 1C-130-1369
TCTO 1C-130-1372
TCTO 1C-130-1372
TCTO 1C-130-1372
TCTO 1C-130-1373
TCTO 1C-130-1373
TCTO 1C-130-1373
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
BSC
SPL
SPL
BSC
SPL
SPL
NAT.
D
G
0
C
D
0
C
F
ORDEM
GLA353A030048800
GLA353A030048900
GLTT32A920000700
GLA332A030049000
GLTT32A920001402
GLA332A030049100
GLA332A930000901
GLA332A930000800
FADT
PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
INSPECTION OF MLG WHEEL WELLWL200 LATERAL STIFFENER/CHANNEL TO LONGERON FOR MISSING FASTENERS, SELECT C-130 AIRCRAFT
INSPECTION OF MLG WHEEL WELLWL200 LATERAL STIFFENER/CHANNEL TO LONGERON FOR MISSING FASTENERS, SELECT C-130 AIRCRAFT
INSPECTION OF MLG WHEEL WELLWL200 LATERAL STIFFENER/CHANNEL TO LONGERON FOR MISSING FASTENERS, SELECT C-130 AIRCRAFT
INSPECTION OF MLG WHEEL WELLSIDE PANEL ASSEMBLY AT BL61.625 BETWEEN FS517 TO FS588 FOR MISSING FASTENERS,SELECT C-130 AIRCRAFT
INSPECTION OF MLG WHEEL WELLSIDE PANEL ASSEMBLY AT BL61.625 BETWEEN FS517 TO FS588 FOR MISSING FASTENERS,SELECT C-130 AIRCRAFT
INSPECTION OF MLG WHEEL WELLSIDE PANEL ASSEMBLY AT BL61.625 BETWEEN FS517 TO FS588 FOR MISSING FASTENERS,SELECT C-130 AIRCRAFT
TÍTULO
31/03/1991
31/03/1991
14/06/1991
14/06/1991
14/06/1991
20/04/1992
20/04/1992
20/04/1992
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
M
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/05/1991
15/10/1993
14/06/1993
15/04/1993
30/08/1992
15/12/1993
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
83Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1373
TCTO 1C-130-1381
TCTO 1C-130-1381
TCTO 1C-130-1381
TCTO 1C-130-1381
TCTO 1C-130-1381
TCTO 1C-130-1382
TCTO 1C-130-1382
TCTO 1C-130-1382
TCTO 1C-130-1385
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
SPL
SPL
SPL
SPL
BSC
SPL
SPL
BSC
NAT.
F
0
C
E
F
G
0
D
F
0
ORDEM
GLA332A930001004
GLA332A910000800
GLA332A910001901
GLA332A910002002
GLA332A910002104
GLA332A910002205
GLTT28A920007600
GLA328A030049200
GLA328A030049300
GLA332A950000500
FADT
INSPECTION OF MLG WHEEL WELLSIDE PANEL ASSEMBLY AT BL61.625 BETWEEN FS517 TO FS588 FOR MISSING FASTENERS,SELECT C-130 AIRCRAFT
INSPECTION OF C-130 WINDOW ASSEMBLIES, MLG INSPECTION, PART NO.372339-3, NSN 9330-00-735-2346LG
INSPECTION OF C-130 WINDOW ASSEMBLIES, MLG INSPECTION, PART NO.372339-3, NSN 9330-00-735-2346LG
INSPECTION OF C-130 WINDOW ASSEMBLIES, MLG INSPECTION, PART NO.372339-3, NSN 9330-00-735-2346LG
INSPECTION OF C-130 WINDOW ASSEMBLIES, MLG INSPECTION, PART NO.372339-3, NSN 9330-00-735-2346LG
INSPECTION OF C-130 WINDOW ASSEMBLIES, MLG INSPECTION, PART NO.372339-3, NSN 9330-00-735-2346LG
INSPECTION OF AUXILIARY VENTVALVE CAN ASSEMBLY PART NO.3328439-1/2 ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL AIRCRAFT
INSPECTION OF AUXILIARY VENTVALVE CAN ASSEMBLY PART NO.3328439-1/2 ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL AIRCRAFT
INSPECTION OF AUXILIARY VENTVALVE CAN ASSEMBLY PART NO.3328439-1/2 ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL AIRCRAFT
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
TÍTULO
20/04/1992
28/06/1991
28/06/1991
28/06/1991
28/06/1991
28/06/1991
15/09/1991
15/09/1991
15/09/1991
11/07/1991
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
M
R
R
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/12/1993
15/09/1991
29/10/1992
28/02/1993
10/10/1993
28/02/1993
01/11/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
84Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1385
TCTO 1C-130-1385
TCTO 1C-130-1397
TCTO 1C-130-1397
TCTO 1C-130-1397
TCTO 1C-130-1398
TCTO 1C-130-1400
TCTO 1C-130-1411
TCTO 1C-130-1411
TCTO 1C-130-1411
TCTO 1C-130-1420
TCTO 1C-130-1420
TCTO 1C-130-1420
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
BSC
SPL
SPL
SPL
BSC
BSC
SPL
SPL
BSC
SPL
SPL
NAT.
C
D
0
C
D
F
0
0
C
D
0
C
D
ORDEM
GLA332A950004701
GLA332A950004802
GLA336A940000700
GLA336A940002701
GLA336A950003602
GLA332A020041100
GLTT26A920000800
GLA328A930000700
GLA328A030049400
GLA328A030049500
GLA334A940000200
GLA334A940001701
GLA334A940001802
FADT
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF AIR FORCE PERSONNEL CLEARED FOR OPERATION OF ...
MODIFICATION OF BLEED AIR DUCT SYSTEM C-130 AIRCRAFT
MODIFICATION OF BLEED AIR DUCT SYSTEM C-130 AIRCRAFT
MODIFICATION OF BLEED AIR DUCT SYSTEM C-130 AIRCRAFT
INSPECTION OF C-130 MLG VERTICAL TORQUE SHAFT, PN 8372M2, AND HORIZONTAL TORQUE SHAFT, PN 8373M2.
INSPECTION AND REPLACEMENT OF FIRE EXTINGUISHER SQUIBS
INSPECTION OF THE LEFT-HAND EXTERNAL FUEL TANK BOOST PUMP WIRING FOR CORRECT TERMINATION ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL ...
INSPECTION OF THE LEFT-HAND EXTERNAL FUEL TANK BOOST PUMP WIRING FOR CORRECT TERMINATION ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL ...
INSPECTION OF THE LEFT-HAND EXTERNAL FUEL TANK BOOST PUMP WIRING FOR CORRECT TERMINATION ON ALL C-130 AIRCRAFT, EXCEPT A-MODEL ...
INSPECTION OF VOR/ILS COAXIAL CABLE FOR CHAFING, C-130 AIRCRAFT
INSPECTION OF VOR/ILS COAXIAL CABLE FOR CHAFING, C-130 AIRCRAFT
INSPECTION OF VOR/ILS COAXIAL CABLE FOR CHAFING,
TÍTULO
11/07/1991
11/07/1991
30/10/1993
30/10/1993
30/10/1993
15/04/1994
18/03/1992
18/11/1992
18/11/1992
18/11/1992
30/10/1993
30/10/1993
30/10/1993
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
31/03/1993
15/12/1993
10/01/1994
01/03/1994
15/09/1994
31/03/1993
15/02/1994
15/09/1994
15/09/1994
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
85Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1423
TCTO 1C-130-1430
TCTO 1C-130-1435
TCTO 1C-130-1435
TCTO 1C-130-1447
TCTO 1C-130-1447
TCTO 1C-130-1452
TCTO 1C-130-1456
TCTO 1C-130-1458
TCTO 1C-130-1463
TCTO 1C-130-1470
TCTO 1C-130-1470
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
SPL
BSC
SPL
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
C
0
C
0
0
0
0
0
0
ORDEM
GLA353A930001600
GLA395A930000201
GLA300A970004500
GLA300A970004601
GLA332A950000300
GLA332A950001601
GLA357A940002500
GLA332A940000300
GLA361S940002100
GLA361S940002001
GLA327A940000600
GLA327A940001100
FADT
C-130 AIRCRAFT
INSPECTION OF FUSELAGE STATION 617 UPPER BULKHEADS FOR CRACKS, C-130 AIRCRAFT
INSPECTION OF ELEVATOR AND LIFE RAFT CABLE FAIRLEAD, P/N 364176, C-130 AIRCRAFT
AIRCRAFT MODIFICATION TO ENABLE QUIK RETRIEVAL OF HUNG PARATROOPER
AIRCRAFT MODIFICATION TO ENABLE QUIK RETRIEVAL OF HUNG PARATROOPER
REPLACEMENT OF MAIN LANDING GEAR EMERGENCY SYSTEM DECALSON C-130E/H AIRCRAFT
REPLACEMENT OF MAIN LANDING GEAR EMERGENCY SYSTEM DECALSON C-130E/H AIRCRAFT
ONE TIME ULTRASONIC INSPECTION OF THE C-130 AIRCRAFT OUTER WING TRUSS MOUNT UPPER TANGS.
INSPECTION AND REPLACEMENT OF C-130 NLG STEERING COLLARBOLTS, NSN 5306-00-087-9565,PART NO.NAS1308-10
INSPECTION OF ALL C-130 AIRCRAFT PROPELLER VALVE HOUSING (P/N714325-7) RECORDS FOR CERTAIN SERIAL NUMBERS TO IDENTIFY POSSIBLE...
INSPECTION OF ALL C-130 AIRCRAFT PROPELLER BLADE RECORDS FOR CERTAIN SERIAL NUMBERS TO IDENTIFY POSSIBLEMANUFACTURING DEFECTS.
ONE TIME INSPECTION OF VISCOUS DAMPER BRACKET ASSEMBLY (P/N 3303564-1) ON AILERON BOOST PACK, ON ALL C-130 AIRCRAFT.
ONE TIME INSPECTION OF VISCOUS DAMPER BRACKET
TÍTULO
22/11/1992
19/03/1993
12/01/1995
12/01/1995
20/05/1994
20/05/1994
29/12/1993
03/03/1994
04/03/1994
30/03/1994
07/06/1994
07/06/1994
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
M
M
R
I
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/10/1995
17/01/1995
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
86Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1474
TCTO 1C-130-1474
TCTO 1C-130-1476
TCTO 1C-130-1478
TCTO 1C-130-1483
TCTO 1C-130-1491
TCTO 1C-130-1493
TCTO 1C-130-1501
TCTO 1C-130-1504
TCTO 1C-130-1504
TCTO 1C-130-1512
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
BSC
BSC
BSC
BSC
BSC
BSC
BSC
SPL
BSC
NAT.
0
C
0
0
0
0
0
0
0
C
0
ORDEM
GLA329A940000500
GLA329A020010400
GLA332A940000400
GLA332A960001500
GLA324A950001100
GLA327A950000400
GLA324A980002200
GLA351A950003900
GLA325A950005100
GLA325A950005201
GLA353A020012500
FADT
ASSEMBLY (P/N 3303564-1) ON AILERON BOOST PACK, ON ALL C-130 AIRCRAFT.
INSPECTION OF C-130 AIRCRAFTAUXILIARY HYDRAULIC BOOST PUMP RELAY.
INSPECTION OF C-130 AIRCRAFTAUXILIARY HYDRAULIC BOOST PUMP RELAY.
INSPECTION OF C-130 AIRCRAFTNOSE LANDING GEAR STEERING ACTUATORS, P/N 695568-5.
INSPECTION OF C-130 AIRCRAFTAUXILIARY HYDRAULIC SYSTEM PUMP SUPPLY LINE.
INSPECTION OF TRANSFORMER RECTIFIER (TR) BLEEDER RESISTORS FOR PROPER RESISTANCE, LOOSE SHUNTS ANDPROPER GROUNDING ON C-130 ...
ONE TIME INSPECTION OF C-130AIRCRAFT AILERON BOOST PACK VISCOUS DAMPER BRACKET ASSEMBLY P/N 3303564-1.
INSTALLATION OF HIGH RELIABILITY MAINTENANCE FREEBATTERIES IN SELECTED C-130 AIRCRAFT
INSPECTION OF THE C130 AIRCRAFT BULKHEAD SPLICE CHANNEL LOCATED AT FUSELAGE STATION 477 AN BUTT LINE FORCRACKS
REPLACEMENT OF C130 AIRCRAFTPARATROP DOOR COUNTER BALANCE SYSTEM
REPLACEMENT OF C130 AIRCRAFTPARATROP DOOR COUNTER BALANCE SYSTEM
REPLACEMENT OF RIVETS WITH STEEL HI-LOC FASTENERS ON C-130 AIRCRAFT STATIC LINE RETRIEVER WINCH SUPPORT BRACKETS.
TÍTULO
15/04/1994
15/04/1994
26/08/1994
17/11/1994
09/01/1995
23/02/1995
27/09/1995
25/05/1995
18/07/1995
19/03/1996
22/09/1995
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
R
M
M
M
M
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/09/1994
19/03/1996
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
87Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1515
TCTO 1C-130-1516
TCTO 1C-130-1525
TCTO 1C-130-1526
TCTO 1C-130-1540
TCTO 1C-130-1549
TCTO 1C-130-1573
TCTO 1C-130-1575
TCTO 1C-130-1575
TCTO 1C-130-1586
TCTO 1C-130-1587
TCTO 1C-130-1587
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
SPL
NAT.
0
0
0
0
0
0
0
0
0
0
0
C
ORDEM
GLA357A960000400
GLA355A960002200
GLA371S960000100
GLA355A020002500
GLA300A020014100
GLA300S970001600
GLA341A020075300
GLA330S970001300
GLA330S030049700
GLA300S970001701
GLA300A970001800
GLA361A970001900
FADT
ONE TIME INSPECTION OF C-130AIRCRAFT NACELLE (HORSE COLLAR AREA) AND DRY BAY DRAINS AND DRAIN LINES FOR OBSTRUCTIONS
INSPECTION OF C-130 AIRCRAFTHORIZONTAL STABILIZER LEADING EDGES FOR CRACKS
INSPECTION OF C-130 ENGINE GIMBLE YOKE ASSEMBLY P/N 363895-5 OR 363895-7
INSPECTION AND INSTALLATION OF AFT EMPENNAGE CONDESATIONDRAIN HOLES
INSPECTION OF C-130 MAIN LANDING GEAR EMERGENCY EXTENSION WRENCH, PART NUMBERS LH100 AND 697308-1.
INSPECTION OF C-130 ANTI-SKID CONTROL BOXES FOR CORRECT PART NUMBERS, 42-109-1A (LOCKHEED 697398-3), 42-109, 42-109A...
REPLACEMENT OF STAINLESS STEEL BLEED AIR DUCTS WITH INCONEL DUCTS ON C-130 AIRCRAFT.
ADDITION OF WATER DRAIN HOLEIN C-130 AIRCRAFT POWER PLANT-ENGINE AIR INCET SCOOP, ANTI-ICE LIP ASSEMBLY,P/N 351576
ADDITION OF WATER DRAIN HOLEIN C-130 AIRCRAFT POWER PLANT-ENGINE AIR INCET SCOOP, ANTI-ICE LIP ASSEMBLY,P/N 351576
INSPECTION OF C-130 AIRCREFTPROPELLER RECORDS FOR IDENTIFICATION OF CERTAIN SERIAL NUMBERED BLADES
REPLACEMENT OF C-130 PROPELLER SYNCROPHASER MOUNTBRACKET WING NUT SAFETY WIRE
REPLACEMENT OF C-130
TÍTULO
13/10/1995
17/10/1995
15/03/1996
03/07/1996
19/08/1996
13/09/1996
15/04/1997
29/01/1997
01/04/1997
14/04/1997
13/05/1997
13/05/1997
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
I
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/05/1997
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
88Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1587
TCTO 1C-130-1591
TCTO 1C-130-1593
TCTO 1C-130-1593
TCTO 1C-130-1602
TCTO 1C-130-1602
TCTO 1C-130-1605
TCTO 1C-130-1606
TCTO 1C-130-1626
TCTO 1C-130-1626
TCTO 1C-130-1626
TCTO 1C-130-1630
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
BSC
SPL
BSC
SPL
BSC
BSC
BSC
BSC
SPL
BSC
NAT.
C
0
0
C
0
D
0
0
0
0
C
0
ORDEM
GLA361A970004101
GLA339A970006000
GLA320A020014300
GLA326A020014400
GLA321A020015200
GLA321A020015400
GLA357A020016300
GLA321A020020300
GLA321A020004200
GLA321A020004201
GLA336A020006800
GLA327A020003800
FADT
PROPELLER SYNCROPHASER MOUNTBRACKET WING NUT SAFETY WIRE
REPLACEMENT OF C-130 PROPELLER SYNCROPHASER MOUNTBRACKET WING NUT SAFETY WIRE
INSPECTION OF THE STOVEPIPE ASSEMBLY AND CIRCUIT BREAKERPANEL ON C-130 AIRCRAFT
INSPECTION OF HANDLES FOR LOOSEOR MISSING HARWARE ON C-130 AICRAFT.
INSPECTION OF HANDLES FOR LOOSEOR MISSING HARWARE ON C-130 AICRAFT.
INSPECTION OF C-130 AICRAFT FLIGHT DECKAND CARGO COMPARTMENT AUXILIARY VENT VALVES PART NUMBER 398650-1-1.
INSPECTION OF C-130 AICRAFT FLIGHT DECKAND CARGO COMPARTMENT AUXILIARY VENT VALVES PART NUMBER 398650-1-1.
INSPECTION OF C-130 AICRAFT CENTER WING LOWER SURFACE PANELS ENGINE DRAG FITTINGS AND FOOTED RIB YAW TECHNICALORDER 1C-130A-36 IN
INSPECTION OF C-130 AICRAFT FLIGHT DECK AND CARGO COMPARTMENT AUXILIARY VEK VALVES PART NUMBER 398550-1-1.
REPLACEMENT OF STAINLESS STEEL BLEED AIR DUCTS ON C-130 AIRCRAFT
REPLACEMENT OF STAINLESS STEEL BLEED AIR DUCTS ON C-130 AIRCRAFT
REPLACEMENT OF STAINLESS STEEL BLEED AIR DUCTS ON C-130 AIRCRAFT
INSPECTION OF C130 AIRCRAFT CENTER AND OUTER WING FLAP
TÍTULO
13/05/1997
01/07/1997
30/07/1997
30/07/1997
10/10/1997
10/10/1997
23/10/1997
04/11/1997
15/10/1999
15/10/1999
15/10/1999
21/01/1998
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
M
M
M
M
M
I
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/05/1997
17/09/1997
17/10/1997
12/01/2000
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
89Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1636
TCTO 1C-130-1639
TCTO 1C-130-1640
TCTO 1C-130-1644
TCTO 1C-130-1650
TCTO 1C-130-1658
TCTO 1C-130-1660
TCTO 1C-130-1679
TCTO 1C-130-1693
TCTO 1C-130-1710
TCTO 1C-130-1722
TCTO 1C-130-1725
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
0
0
0
0
0
0
0
0
0
ORDEM
GLA364A030004200
GLA353A020005400
GLA320A020012600
GLA327A020006500
GLA352A020018500
GLA324A020019800
GLA324A020070900
GLA320A020009100
GLA354A020012800
GLA327A020005600
GLA376A020006100
GLA357A020008800
FADT
CONNECTING LINK ASSEMBLIES (LINK)...
ONE TIME INSPECTION FOR CHAFING OF INSTRUCTION PILOT'S INTER COM/INTERPHONEWIRING
"INSPECTION OF C-130 AIRCRAFT LOWER BULKHEAD CAPSLOCATED BETWEEN FS 245 AND FS 737 FOR CORROSION".
INSPECTION OF STATIC LINE RETRIEVAL WINCHES FOR PROPERADJUSTMENT OF SLIP CLUTCH ASSEMBLIES
INSPECTION OF C130 AIRCRAFT FLAP JACKS CREW COUPLING CHAIN FOR PROPER MASTER LINKINSTALLATION
INPECTION OF AICRAFT CREW DOOR(...) SYSTEM LOCKING SPRING FOR PROPER INSTALLATION.
INSPECTION OF AICRAFT AND SCNS SEALEND LEAD ACID BATTEERY(SLAB) FOR ALL C-130AICRAFT.
INSPECTION OF WINDOW HEATINGCIRCUIT FOR CORRECT ELECTERICAL SOURCE CONNECTION ON C-130 AIRCRAFT
INSPECTION OF C-130 AIRCRAFTCARGO HANDLING SYSTEM RIGHT HAND DETENT LATCH FOR MISSING SET SCREWS
INSPESTION OF C-130 AICRAFT ENGINE TRUN MOUNT BARREL NUST FOR INDENTICATION.
INSPECTION OF ELEVATOR CONTROL COLUMN SLEEVING ON C-130 AIRCRAFT
INSPECTION OF ENGINE THROTTLE AND CONDITION LEVERTENSION REGULATOR SERIAL NUMBERS ON C-130 AIRCRAFT
INSPECTION OF C-130 AIRCRAFT
TÍTULO
20/05/1998
05/05/1998
05/06/1998
04/08/1998
21/07/1999
18/09/1999
21/03/2000
02/02/1999
05/05/1999
13/07/2000
19/11/1999
06/12/1999
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
M
M
M
M
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
90Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1736
TCTO 1C-130-1736
TCTO 1C-130-1739
TCTO 1C-130-1752
TCTO 1C-130-1765
TCTO 1C-130-1768
TCTO 1C-130-1777
TCTO 1C-130-1787
TCTO 1C-130-1804
TCTO 1C-130-1804
TCTO 1C-130-1811
TCTO 1C-130-1828
TCTO 1C-130-1828
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
BSC
SPL
BSC
BSC
BSC
BSC
BSC
REV
BSC
BSC
REV
NAT.
0
C
0
D
0
0
0
0
0
C
0
0
C
ORDEM
GLA300A020013400
GLA370A020013500
GLA332A020008500
GLA354A020071600
GLA354A020071701
GLA329A020008701
GLA324A020071200
GLA322A020013200
GLA353A040014300
GLA353A040014800
GLA327A050001800
GLA357A030010101
GLA357A030018301
FADT
NUMBER TWO AND NUMBER THREE DRY BAY DRAIN TROUGHS FOR LEAKS
INSPECTION OF T56 THROTLE CONTROL ARMS ON C-130 AIRCRAFT
INSPECTION OF T56 THROTLE CONTROL ARMS ON C-130 AIRCRAFT
"INSPECTION OF NOSE LANDING GEAR STEERING CYLINDER ASSEMBLY ON C-130 AIRCRAFT".
REPLACEMENT OF C-130 AIRCRAFT ENGINE TRUSS MOUNTS
INSTALLATION OF C-130 AIRCRAFT CENTER WINGUPPER TRUSS MOUNT LUG ATTACHMENT NUT PLATES AT CERTER WING STATION 178.782
INSPECTION OF ALL C-130 AIRCRAFT FOR WATERMAN TYPE HYDRAULIC FLOW REGULATORS
INSPECTION OF ALL 28VDC RECEPTACLES ON C-130 AIRCRAFT FOR CORRECT WIRE INSTALLATION
"INSPECTION OF THE AUTOPILOTWIRE BUNDLE FOR CHAFFING/SCHORCHING ON C-130AIRCRAFT".
INSPECTION OF FASTENERS IN UPPER FS 858.0 RING SEGMENT AND ATTACH FITTING
INSPECTION OF FASTENERS IN UPPER FS 858.0 RING SEGMENT AND ATTACH FITTING
INSPECTION OF AILERON CONTOLCABLE PULLEY ATTACH BRACKET FASTENERS
EDDY CURRENT INSPECTION OF CENTER WING LOWER FORWARD CORNER FITTING
EDDY CURRENT INSPECTION OF CENTER WING LOWER FORWARD CORNER FITTING
TÍTULO
30/08/2000
30/08/2000
15/08/2000
20/07/2000
16/10/2000
11/03/2000
15/03/2002
17/08/2001
06/05/2003
06/05/2003
30/06/2004
15/09/2002
15/09/2002
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
M
I
M
I
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/12/2000
02/03/2001
20/08/2003
28/03/2003
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
91Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-1856
TCTO 1C-130-1857
TCTO 1C-130-1871
TCTO 1C-130-1915
TCTO 1C-130-1963
TCTO 1C-130-1969
TCTO 1C-130-1975
TCTO 1C-130-1979
TCTO 1C-130-1979
TCTO 1C-130-1983
TCTO 1C-130-1983
TCTO 1C-130-1983
TCTO 1C-130-1997
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
SPL
BSC
SPL
SPL
BSC
NAT.
0
0
0
0
0
0
0
0
C
0
C
D
0
ORDEM
GLA327A040014900
GLA328A030029501
GLA357A040015000
GLA332A060000800
GLA324A070005700
GLA357A070003600
GLA332A070005100
GLA324A080001400
GLA324A090002600
GLA396A090002000
GLA396A110000600
GLA396A110000700
GLA354A080000300
FADT
"INSPECTION OF FLIGHT CONTROL CABLES CHAFFING AND PROPER ROUTING AT F.S. 477 RIGHT SIDE AND CORRECTION OFCABLE RUN IF NECESSARY".
INSPECTION OF FUEL BOOST PUMP ELECTRICAL GROUD AND BOND CONNECTION
"INSPECTION OF CENTER WING LOWER AFT SPAR CAP AT FS 597FROM WS 190 TO WS 214 (LEFT AND RIGHT)".
RELOCATION OF MAIN LANDIND GEAR DOWN LOCK INDICATION GROUNDS ON C-130 AIRCRAFT
INSPECTION OF AIRCRAFT BATTERIES ON C-130 AIRCRAFT
"INTERIM ROUTINE SAFETY INSPECTION OF LOWER FORWARD WING PANEL UNDER ARMPIT PANEL AT WS 71 FOR CRACKS".
INSPECTION FOR CORRECT HARDWARE INSTALLATION ON MAIN LANDING GEAR BALL SCREWASSEMBLY FRICTION WASHER, CAP NUT AND SPACER.
ONE TIME INSPECTION OF RH/LH
ONE TIME INSPECTION OF RH/LH
RELOCATION OF ELETRICAL CONDUIT PART NUMBER 02032363-9 ON SELECTD C-130 AIRCRAFT
RELOCATION OF ELETRICAL CONDUIT PART NUMBER 02032363-9 ON SELECTD C-130 AIRCRAFT
RELOCATION OF ELETRICAL CONDUIT PART NUMBER 02032363-9 ON SELECTD C-130 AIRCRAFT
INSPECTION OF EXTERNAL FUEL TANK AND PYLON (...) [P/N
TÍTULO
10/09/2003
24/09/2003
19/02/2004
01/09/2005
30/04/2007
29/06/2007
31/08/2007
13/12/2007
13/12/2007
04/08/2008
04/08/2008
04/08/2008
04/04/2008
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
M
M
M
M
I
M
I
I
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
21/03/2008
23/10/2008
09/12/2011
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BAS
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
92Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-2018
TCTO 1C-130-2018
TCTO 1C-130-2019
TCTO 1C-130-2020
TCTO 1C-130-2020
TCTO 1C-130-2029
TCTO 1C-130-2050
TCTO 1C-130-2056
TCTO 1C-130-2087
TCTO 1C-130-2109
TCTO 1C-130-2109
TCTO 1C-130-2111
TCTO 1C-130-2111
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
BSC
BSC
SPL
BSC
BSC
BSC
BSC
BSC
SPO
BSC
SPO
NAT.
0
C
0
0
C
0
0
0
0
0
C
0
C
ORDEM
GLA357A090000500
GLA357A090000600
GLA354A090000700
GLA354A090000800
GLA354A090000900
GLA354A100000600
GLA353A100000100
GLA332A100000200
GLA332A110000800
GLA326A120000900
GLA326A130000300
GLA352A130000100
GLA352A130000200
FADT
NAS636A32] (...) EXCEPT THOSE AIRCRAFT NOT EQUIPPED WITH EXTERNAL TANKS.
INSPECTION OF UPPER WING JOINT BARREL NUTS ON ALL AIRCRAFT, EXCEPT C-130J.
INSPECTION OF UPPER WING JOINT BARREL NUTS ON ALL AIRCRAFT, EXCEPT C-130J.
INSPECTION OF INFLIGHT REFUELING PYLON AFT MOUNTINGNUT ON ALL C-130 TANKER AIRCRAFT.
INSPECTION OF LOWER ENGINE MOUNT BARREL NUTS ON ALL C-130 AIRCRAFT.
INSPECTION OF LOWER ENGINE MOUNT BARREL NUTS ON ALL C-130 AIRCRAFT.
INSPECTION OF LOWER ENGINE TRUSS MOUNTS FOR PART NUMBER1452-126 BARREL NUTS ON ALL C-130 AIRCRAFT.
ISNPECTION OF SUPPORT ARM , NOSE LANDING GEAR STRUT DRAGBRACE ON AL C-130 AIRCRAFT
INSPECTION AND REPLACEMENT OF MAIN LANDING GEAR WHEEL TIE BOLTS PART NUMBER GY1810-60 ON C-130 AIRCRAFT THRU AF08-08607
INSPECTION OF MAIN LANDING GEAR FRICTION WASHER ON ALL C-13O AIRCRAFT
INSPECTION OF FIRE EXTINGUISHING TUBE ASSEMBLY
INSPECTION OF FIRE EXTINGUISHING TUBE ASSEMBLY
INSPECTION/REPAIR OF LEFT AND RIGHT PARATROOP DOOR FRAME AFT VERTICAL EDGE RADIUS, C-130 LEGACY AND J-MODEL
INSPECTION/REPAIR OF LEFT
TÍTULO
04/03/2009
04/03/2009
06/03/2009
06/03/2009
06/03/2009
15/05/2009
21/01/2010
12/02/2010
07/03/2011
23/11/2011
23/11/2011
09/12/2011
09/12/2011
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
I
M
M
I
M
M
M
M
M
I
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
05/03/2009
07/03/2009
06/12/2011
16/12/2011
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
E
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
93Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-2135
TCTO 1C-130-752
TCTO 1C-130-756
TCTO 1C-130-756
TCTO 1C-130-756
TCTO 1C-130-759
TCTO 1C-130-842
TCTO 1C-130-842
TCTO 1C-130-842
TCTO 1C-130-849
TCTO 1C-130-855
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
SPL
SPL
BSC
BSC
SPL
SPL
BSC
BSC
BSC
NAT.
0
000
C
D
000
000
C
D
000
0
000
ORDEM
GLA330A140000400
GLA372S900004600
GLA332A030019000
GLA332A030019100
GLA332A900002700
GLA332A900003200
GLTT25S700000101
GLA325A900000503
GLA325A900001200
GLA321A780000500
GLA371S900004300
FADT
AND RIGHT PARATROOP DOOR FRAME AFT VERTICAL EDGE RADIUS, C-130 LEGACY AND J-MODEL
INSPECTION OF PART NUMBER 351613-5/-6 BLEED AIR DIFFUSERS IN THE VERTICAL STABILIZER, C-130 AIRCRAFT
INSPECTION OF ENGINE TRUSS MOUNTS, C-130 AIRCRAFT
INSPECTION OF NOSE LANDING GEAR STRUT OUTER CYLINDER AND INSPECTION AND REWORK OFMAIN LANDING GEAR TORQUE STRUTS - C-130 ...
INSPECTION OF NOSE LANDING GEAR STRUT OUTER CYLINDER AND INSPECTION AND REWORK OFMAIN LANDING GEAR TORQUE STRUTS - C-130 ...
INSPECTION OF NOSE LANDING GEAR STRUT OUTER CYLINDER AND INSPECTION AND REWORK OFMAIN LANDING GEAR TORQUE STRUTS - C-130 ...
REMOVABLE PANEL FOR EMERGENCY EXTENSION OF NOSE GEAR, C-130 AIRCRAFT
INSPECTION AND REWORK OF RADOME SEAL RETAINER P/N 372176-17 ON RADOME P/N 389154-1, C-130B/E AIRCRAFT
INSPECTION AND REWORK OF RADOME SEAL RETAINER P/N 372176-17 ON RADOME P/N 389154-1, C-130B/E AIRCRAFT
INSPECTION AND REWORK OF RADOME SEAL RETAINER P/N 372176-17 ON RADOME P/N 389154-1, C-130B/E AIRCRAFT
INSTALLATION OF 35 TEMPERATURE CONTROL SYSTEM FLIGHT DECK WATER SEPARATOR,C-130 AIRCRAFT
INSPECTION AND SWAP-OUT OF
TÍTULO
01/02/2013
15/06/1966
26/09/1966
26/09/1966
26/09/1966
10/03/1972
10/04/1970
10/04/1970
10/04/1970
28/12/1976
05/04/1971
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
R
R
R
R
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
15/06/1966
25/10/1966
16/01/1967
26/09/1966
10/03/1972
09/06/1970
05/10/1970
10/04/1970
05/04/1971
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE/BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
94Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-860
TCTO 1C-130-860
TCTO 1C-130-860
TCTO 1C-130-860
TCTO 1C-130-863
TCTO 1C-130-864
TCTO 1C-130-876
TCTO 1C-130-907
TCTO 1C-130-909
TCTO 1C-130-909
TCTO 1C-130-909
TCTO 1C-130-909
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
SPL
BSC
BSC
BSC
BSC
BSC
BSC
SPL
SPL
SPL
SPL
NAT.
C
D
000
000
000
000
000
000
C
D
E
F
ORDEM
GLA300S020000700
GLA324A820005702
GLA324A820000401
GLA324A820000402
GLA372S780002200
GLA324A900001600
GLA327A900008400
GLA327A800002100
GLA324A030021000
GLA324A030021100
GLA324A030021200
GLA324A030021300
FADT
ENGINE DRIVEN HYDRAULIC PUMPS ON C-130 SERIES AIRCRAFT
INSPECTION OF P/N D7271-3 SERIES CIRCUIT BREAKERS INSTALLED IN C-130B/E/H/P/N SERIES AIRCRAFT
INSPECTION OF P/N D7271-3 SERIES CIRCUIT BREAKERS INSTALLED IN C-130B/E/H/P/N SERIES AIRCRAFT
INSPECTION OF P/N D7271-3 SERIES CIRCUIT BREAKERS INSTALLED IN C-130B/E/H/P/N SERIES AIRCRAFT
INSPECTION OF P/N D7271-3 SERIES CIRCUIT BREAKERS INSTALLED IN C-130B/E/H/P/N SERIES AIRCRAFT
INSPECTION OF NO.1 AND NO.4 ENGINE TRUSS MOUNT UPPER ATTACH LUG FOR CRACKS - C-130B/E/H/P AIRCRAFT.
REPLACEMENT OF CIRCUIT BREAKERS, PART NO.7271-3 SERIES, INSTALLED IN C-130B/E/H/P/N SERIES AIRCRAFT
INSPECTION OF RUDDER ATTACH POINT BEARINGS, P/N MS20200KP10, ALL C-130 SERIES AIRCRAFT
INSPECTION OF AILERON FIXED TAB DEFLECTION, C-130 AIRCRAFT
INSPECTION OF TRIM SWITCH, P/N 4TF1-2 AND 4TF2-2, C-130AIRCRAFT
INSPECTION OF TRIM SWITCH, P/N 4TF1-2 AND 4TF2-2, C-130AIRCRAFT
INSPECTION OF TRIM SWITCH, P/N 4TF1-2 AND 4TF2-2, C-130AIRCRAFT
INSPECTION OF TRIM SWITCH, P/N 4TF1-2 AND 4TF2-2, C-130
TÍTULO
19/02/1971
19/02/1971
19/02/1971
19/02/1971
27/05/1971
12/08/1971
21/11/1971
03/12/1979
28/02/1974
28/02/1974
28/02/1974
28/02/1974
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
R
R
R
M
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
24/03/1971
27/05/1971
19/02/1971
19/02/1971
27/05/1971
12/08/1971
21/11/1971
03/12/1979
19/03/1974
16/04/1974
15/08/1974
18/10/1974
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
95Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-909
TCTO 1C-130-918
TCTO 1C-130-918
TCTO 1C-130-918
TCTO 1C-130-918
TCTO 1C-130-939
TCTO 1C-130-939
TCTO 1C-130-940
TCTO 1C-130-941
TCTO 1C-130-941
TCTO 1C-130-941
TCTO 1C-130-944
TCTO 1C-130-944
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
SPL
SPL
BSC
SPL
BSC
BSC
SPL
SPL
BSC
SPL
BSC
NAT.
0
C
D
E
000
C
000
000
C
D
000
C
000
ORDEM
GLA324A840000700
GLA327A800007801
GLTT27A800000202
GLA327A800007903
GLA327A800001900
GLA324A030021600
GLA324A790000400
GLTT72S770001700
GLA324A030021800
GLA324A030021700
GLA324A790000500
GLA326A030021900
GLTT26A770000400
FADT
AIRCRAFT
INSPECTION OF TRIM SWITCH, P/N 4TF1-2 AND 4TF2-2, C-130AIRCRAFT
INSPECTION OF BOLT, P/N NAS1104-35 OR EQUIVALENT, ATCABLE TENSION REGULATOR ELEVATOR CONTROL FOR PROPER INSTALLATION
INSPECTION OF BOLT, P/N NAS1104-35 OR EQUIVALENT, ATCABLE TENSION REGULATOR ELEVATOR CONTROL FOR PROPER INSTALLATION
INSPECTION OF BOLT, P/N NAS1104-35 OR EQUIVALENT, ATCABLE TENSION REGULATOR ELEVATOR CONTROL FOR PROPER INSTALLATION
INSPECTION OF BOLT, P/N NAS1104-35 OR EQUIVALENT, ATCABLE TENSION REGULATOR ELEVATOR CONTROL FOR PROPER INSTALLATION
INSPECTION OF FLIGHT STATIONCIRCUIT BREAKER PANELS, C-130 AIRCRAFT
INSPECTION OF FLIGHT STATIONCIRCUIT BREAKER PANELS, C-130 AIRCRAFT
IMPROVED SECURITY OF INNER REAR EXHAUST CONE
MODIFICATION OF ISOLATED DC BUS OFF INDICATOR CIRCUIT, C-130 AIRCRAFT
MODIFICATION OF ISOLATED DC BUS OFF INDICATOR CIRCUIT, C-130 AIRCRAFT
MODIFICATION OF ISOLATED DC BUS OFF INDICATOR CIRCUIT, C-130 AIRCRAFT
INSPECTION OF TURBINE OVERHEAT WARNING KEYERS, PART NO.834-00049
INSPECTION OF TURBINE
TÍTULO
28/02/1974
25/10/1974
25/10/1974
25/10/1974
25/10/1974
14/05/1976
14/05/1976
01/07/1976
18/03/1977
18/03/1977
18/03/1977
31/03/1977
11/05/1977
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
M
M
M
M
R
R
R
R
R
R
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
29/10/1974
07/11/1974
23/04/1975
25/10/1974
09/05/1976
14/05/1976
01/07/1976
19/04/1977
26/10/1977
18/03/1977
11/05/1977
11/05/1977
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
96Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-950
TCTO 1C-130-958
TCTO 1C-130-958
TCTO 1C-130-962
TCTO 1C-130-962
TCTO 1C-130-962
TCTO 1C-130-964
TCTO 1C-130-971
TCTO 1C-130-972
TCTO 1C-130-972
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
SPL
BSC
SPL
SPL
BSC
SPL
BSC
SPL
BSC
NAT.
000
C
0
C
D
0
D
0
C
000
ORDEM
GLTT32A770000700
GLA325A030022000
GLTT25A770000200
GLA353A780003001
GLTT00X980022700
GLA353A030022100
GLA353A780003402
GLA327A780000800
GLA327A030022400
GLA327A780000900
FADT
OVERHEAT WARNING KEYERS, PART NO.834-00049
INSPECTION/SERVICING OF MAINLANDING GEAR BALL SCREW PILLOW BLOCK ASSEMBLY, PART NO.8353-7, FOR PROPER LUBRICATION, C-130 AIRCRAFT
INSPECTION OF AUXILIARY RAMP, PART NO.7230881-10, NSN 1680-00-405-6842LG, FOR DELAMINATION, C-130 AIRCRAFT
INSPECTION OF AUXILIARY RAMP, PART NO.7230881-10, NSN 1680-00-405-6842LG, FOR DELAMINATION, C-130 AIRCRAFT
INSTALLATION OF WINDOW, UPPER CIRCUIT BREAKER DOOR ASSEMBLY, PART NO.372951-1 OR 378259-1, FUSELAGE STATION 241.0, C-130 AIRCRAFT
INSTALLATION OF WINDOW, UPPER CIRCUIT BREAKER DOOR ASSEMBLY, PART NO.372951-1 OR 378259-1, FUSELAGE STATION 241.0, C-130 AIRCRAFT
INSTALLATION OF WINDOW, UPPER CIRCUIT BREAKER DOOR ASSEMBLY, PART NO.372951-1 OR 378259-1, FUSELAGE STATION 241.0, C-130 AIRCRAFT
INSPECTION OF FRAME WEB IN AREA OF MANUAL GEARBOX LOWERMOUNTING BOLT HOLE, FUSELAGESTATION 517, W.L.245, C/JHC/KC-130H, ...
INSPECTION OF THROTTLE CABLETENSION REGULATORS, C-130 AIRCRAFT
INSPECTION OF ELEVATOR TORQUE TUBE COLLAR, PART NO.339732, C-130 AIRCRAFT
INSPECTION OF ELEVATOR
TÍTULO
05/11/1976
03/06/1977
01/07/1977
05/08/1977
05/08/1977
05/08/1977
15/11/1977
30/05/1978
28/01/1978
28/01/1978
V
V
V
V
V
V
V
V
V
V
ENQ.
M
R
R
R
M
R
R
R
R
R
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
05/11/1976
01/07/1977
26/08/1977
06/03/1978
09/02/1978
21/07/1978
28/01/1978
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
97Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-974
TCTO 1C-130-977
TCTO 1C-130-978
TCTO 1C-130-979
TCTO 1C-130-979
TCTO 1C-130-979
TCTO 1C-130-979
TCTO 1C-130-979
TCTO 1C-130-984
TCTO 1C-130-988
TCTO 1C-130-993
TCTO 1C-130-994
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
SPL
SPL
SPL
SPL
BSC
BSC
BSC
BSC
BSC
NAT.
000
000
000
C
D
E
F
000
0
000
000
000
ORDEM
GLA380S790004100
GLA329A780001000
GLA372S790003200
GLA325A790005401
GLA325A790005502
GLA325A790005603
GLA325A800007604
GLA325A790000700
GLA327A790001300
GLA324A790000600
GLA332S790001800
GLA332S790001900
FADT
TORQUE TUBE COLLAR, PART NO.339732, C-130 AIRCRAFT
MODIFICATION OF ENGINE STARTING CONTROL CIRCUITS, C-130 SERIES AIRCRAFT
INSPECTION OF MAIN LANDING GEAR HYDRAULIC SWIVEL JOINT,PART NO.210-2360, FOR CRACK,C-130 AIRCRAFT
INSPECTION OF TORQUEMETER ANTI-ICING SHROUDS C-130 AIRCRAFT - ALL SERIES
INSTALLATION OF STATIC LINE ANCHOR CABLE TURNBUCKLE LOCKASSEMBLY, C-130 AIRCRAFT
INSTALLATION OF STATIC LINE ANCHOR CABLE TURNBUCKLE LOCKASSEMBLY, C-130 AIRCRAFT
INSTALLATION OF STATIC LINE ANCHOR CABLE TURNBUCKLE LOCKASSEMBLY, C-130 AIRCRAFT
INSTALLATION OF STATIC LINE ANCHOR CABLE TURNBUCKLE LOCKASSEMBLY, C-130 AIRCRAFT
INSTALLATION OF STATIC LINE ANCHOR CABLE TURNBUCKLE LOCKASSEMBLY, C-130 AIRCRAFT
INSPECTION OF ALL C-130 SERIES AIRCRAFT RUDDER BOOSTER ASSEMBLIES, PART NO.364697-1 AND 372021-5, -7
INSPECTION OF FLIGHT STATIONCIRCUIT BREAKERS CHAFING ELECTRICAL WIRING HARNESS AND ADEL CLAMPS, C-130 AIRCRAFT
INSPECTION, REPAIR/REPLACEMENT OF MAIN LANDING GEAR BALLSCREW ASSEMBLY, C-130 AIRCRAFT
REMOVAL AND REPAIR/REPLACEMENT OF SUSPECTED MAIN LANDING GEAR CALCO BALLSCREW ASSEMBLY, PART NO.8353, C-130 AIRCRAFT
TÍTULO
13/10/1978
08/09/1978
13/10/1978
01/11/1978
01/11/1978
01/11/1978
01/11/1978
01/11/1979
31/12/1978
01/12/1978
31/01/1979
23/02/1979
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
R
R
R
R
R
R
M
M
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
13/10/1978
08/09/1978
13/10/1978
12/12/1978
15/02/1979
06/04/1979
24/08/1979
01/11/1979
01/12/1978
31/01/1979
23/02/1979
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
98Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TCTO 1C-130-996
TCTO 1C-130-996
TCTO 2J-T56-611
TCTO 2J-T56-611
TCTO 2J-T56-625
TCTO 2J-T56-627
TCTO 2J-T56-627
TCTO 2J-T56-636
TCTO 2J-T56-636
TCTO 2J-T56-646
TCTO 2J-T56-666
TCTO 35A2-2-9-513
TCTO 8-1-513
Nº PUB
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
SPL
BSC
BSC
SPL
SPL
BSC
SPL
SPL
SPL
BSC
BSC
BSC
BSC
NAT.
C
000
0
E
E
0
F
C
D
0
0
000
000
ORDEM
GLA373S800005901
GLA373S800005800
GLA372S800005600
GLA372S800005501
GLA372S800005703
GLA372S840006900
GLA372S840007003
GLA372S820004701
GLA372S860002202
GLA372S840007100
GLA372S910005400
GLA325S830005300
GLA324A830001500
FADT
ONE-TIME INSPECTION OF NACELLE FUEL SUPPLY HOSE ASSEMBLY, C-130 AIRCRAFT ANDPOWER PACKAGES
ONE-TIME INSPECTION OF NACELLE FUEL SUPPLY HOSE ASSEMBLY, C-130 AIRCRAFT ANDPOWER PACKAGES
MODIFICATION OF POWER SECTION TO INCORPORATE DOWN-THE-SHAFT VENTING - T56-A-7 AND -7A ENGINES
MODIFICATION OF POWER SECTION TO INCORPORATE DOWN-THE-SHAFT VENTING - T56-A-7 AND -7A ENGINES
INCORPORATION OF BEARING TRAIN KEYBOCKS -T56 REDUCTION...
INSTALLATION OF EXTERNAL OILFILTER SYSTEM T56-A-7B AND -15 ENGINES.
INSTALLATION OF EXTERNAL OILFILTER SYSTEM T56-A-7B AND -15 ENGINES.
POSITIVE OIL SUPPLY TO TACHOMETER DRIVE GEAR BEARINGS G56-A-15 REDUCTION GEAR ASSEMBLY.
POSITIVE OIL SUPPLY TO TACHOMETER DRIVE GEAR BEARINGS G56-A-15 REDUCTION GEAR ASSEMBLY.
REWORK OF 656-9 AND-15 REDUCTION GEARBOX REAR HOUSING ASSEMBLIES
LOCAL FLUORESCENT PENETRANT INSPECTION OF BAR ASSY
SUSPECTION OF BOLTS, P/N'S AN1047, AN1C-20, AND AN14-23A, APPLICABLE TO B4 SERIES30
SAFETY TIME COMPLIANCE TECHNICAL ORDER-ONE TIME INSPECTION OF LAMP, PART NO.
TÍTULO
30/05/1979
30/05/1979
01/09/1967
01/09/1967
01/06/1972
15/07/1975
15/07/1975
02/04/1976
02/04/1976
28/02/1983
20/09/1989
28/11/1977
03/02/1983
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
M
M
M
M
R
R
R
R
R
R
R
M
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
20/09/1979
30/05/1979
12/07/1972
07/03/1980
25/11/1974
10/02/1982
25/02/1986
28/11/1977
03/02/1983
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL BASE
NÍVEL BASE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL GERAL
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
99Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
THO-1383C-GDW-88L
THO-1736C-JCW-88L
THO-574C-RSS-87L
TLX 061200Z
TLX 892478
TLX 892478
TLX L89G0447
TLX P121920Z
TLX P221018Z
TLX P312052Z
TLX PR131420Z
TLX R021440Z
TLX R021600Z
TLX R031415Z
TLX R101206Z
TLX R141902Z
Nº PUB
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
ALLISON TRANSMISSION, INC.
USAF
USAF
USAF
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
BSC
NAT.
0
0
0
000
000
000
0
000
000
000
0
000
000
000
000
000
ORDEM
GLA372S900006400
GLA372S910006100
GLA372S870001700
GLA328A830007200
GLA331A790008500
GLA370A780001700
GLA353A890006800
GLA351A830005600
GLA377A960002400
GLA376A890006100
GLA328A980001900
GLA332S890001300
GLA329S850008900
GLA361S040012000
GLA332S790005200
GLA300X790007000
FADT
MS25231-313.
SECOND STAGE T56 TURBINE WHELL FAILURES
T56 PROPELLER SHAFT VAERTICAL MOVEMENT AND END PLAY CHECK
T56 ENGINE ANTI-ICE AIR VALVE MAINTENANCE
FUEL TANK DIP STICKS
CAPACITANCE TYPE FUEL QUANTITY TEST SET
CAPACITANCE TYPE FUEL QUANTITY TEST SET
FUSELAGE - INSPECTION OF PRESSURIZED FAIRING SUPPORT STRUCTURE
MAINTENANCE ADVIDORY C-130 OUTER WING REMOVABLE DIAGONAL BRACE ATTACHMENT HOLES.
TORQUE INDICATORS
INSPECTION CRITERIA FOR C-130 AIRCRAFT THROTTLE AND CONDITION CABLES
C-130 TANKER FUEL PUMP DEFICIENCY
HANDLING AND DISTRIBUTION NOTICE - COMPLY WITH STATEMENT AND DESTROY BY ANYMETHOD THAT PREVEMNET DISCLOSURE OF THE CONTENTS...
USE OF GREASE TO LUBRICATE SEALS AND O-RINGS IN AIRCRAFT HYDRAULIC SYSTEMS.
C-130 INTERMEDIATE PROP CONTROL LINKAGE
INCORPORATES A DOUBLE-FLANGEDESIGN TO ACCOMODATE THE IMPOSED ALL STRESS WITHOUT INVOKING FAILURES
MAINTENANCE/ADVISORY MESSAGE
TÍTULO
18/05/1988
03/01/1989
27/01/1987
30/09/1983
07/07/1978
07/07/1978
19/05/1989
01/08/1983
01/02/1996
01/01/1989
01/11/1997
02/05/1989
01/01/1985
01/06/1996
01/08/1978
01/05/1976
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
V
ENQ.
R
R
R
I
M
M
M
I
I
M
M
M
I
R
R
I
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
30/09/1983
07/07/1978
07/07/1978
01/08/1983
01/02/1996
01/01/1989
02/05/1989
01/01/1985
01/06/1996
01/08/1978
01/05/1976
DT.ALTERAÇÃO PAR.
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
F
SISTEMA: -
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL GERAL
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL BASE
NÍVEL PARQUE
NÍVEL
PARQUE DE MATERIAL AERONÁUTICO DO GALEÃO
100Pag.: de
Data: 22/05/2018
ÍNDICE DE DIRETIVAS POR PROJETO
SISTEMA INTEGRADO DE LOGÍSTICA DE MATERIAL E DE SERVIÇOS
16:23:35
ENG0264R v.10.1
Hora:
100
C-130PROJETO:
TLX R161334Z
TLX R191408Z
TLX R201254Z
TLX R251830Z
TLX R291640Z
Nº PUB
LOCKHEED MARTIN CORPORATION³DBA LOCKHEED MARTIN
USAF
USAF
USAF
USAF
FABRICANTE
BSC
BSC
BSC
BSC
BSC
NAT.
000
000
000
000
000
ORDEM
GLA300S790007100
GLA373S810004900
GLA357A900007900
GLA332A900002300
GLA376A890006200
FADT
ON NOISE WARNING LABE
MAINTENANCE ADVISOTY MESSAGEON AVIATION LIFE SUPPORT EQUIPMENT
TEMPERATURE DATUM CONTROL AMPLIFIER
WING JACKING REQUIREMENTS FOR INSPECTION/RETORQUING WING ATTACH BOLTS
COMPLY WITH DYSTRIBUTION STATEMENT AND DESTROY ANY METHOD THAT WILL PREVENT DISCLOSURE OF THE...
MAINTENANCE ADVISORY; LUBRICATION REQUERIMENTS FOR7 BY 19 STAINLESS STEEL ENGINE THROTTLE/CONDITION CABLES FOR C-130 AIRCRAFT
TÍTULO
01/06/1976
01/12/1980
01/06/1990
25/09/1989
01/08/1989
V
V
V
V
V
ENQ.
M
I
I
R
M
CLA.
PERÍODO DA ANÁLISE: A3 -
DT.BÁSICO
01/06/1976
01/12/1980
01/06/1990
25/09/1989
01/08/1989
DT.ALTERAÇÃO PAR.
F
F
F
F
F
SISTEMA:
Total de registros: 1331
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