Xa-uir 22052 Prog Mtto Jun-01-2010

REG. NUMBER / MATRICULA: XA-UIR

MANUFACTREDATE / FECHAFABRICACION:

03-Oct-07 REPORT DATE/ FECHA REPORTE: 21-Apr-10 30.0

MODEL/ MODELO : AGUSTA A109S TIME SINCE NEW T.S.N. TIME SINCE OVERHAUL T.S.O.

CYCLES SINCE NEW C.S.N.

CYCLES SINCE OVERHAUL C.S.O. 0

Manual Low Cycle Fatigue (LCF) Counting; TABLE 3,PW207C Engine Turbine/Turboshaft RotorComponents - Service Life

HOURS ALLOWED / HORAS PROMEDIO

EXTERNAL HOIST CYCLES

OWNER' S / PROPIETARIO: AEROLINEAS EJECUTIVAS S. A. DE C. V.

SERIAL / SERIE No.

Maintenance Program.Time/Calendar Limited Items Status.

AIRCRAFT / AERONAVE: 354.6 N/T 1240 N/T Flights Starts RapidTake-off

2½ Min. RatingExcursions CT 0

ENGINE / MOTOR 1: 354.6 N/T 548 N/T 0 0 0 0 0ENGINE / MOTOR 2: 354.6 N/T 548 N/T 0 0 0 0 0 PRINTED DATE 1-Jun-10

No. DATE / FECHA T. T. HRS C. T. T. T. HRS. T.S.O. T. T. HRS. T.S.O.

Components - Service Life

LIMITS / LIMITES

DATE / FECHACOMPONENT / COMPONENTE

NOTES &OBSERVATIONS /NOTAS YOBSERVACIONES

TIME REMAINING / TIEMPO REMANENTE

HOURS / HORAS CYCLES / CICLOSHOURS / HORAS CYCLES / CICLOS

NEXT DUE / PROXIMO CUMPLIMINETO

DATE / FECHA

CARGO HOOK HOURS

AIRCRAFT / AERONAVEREQUIREMENT / REQUERIMIENTO

DESCRIPTION / DESCRIPCION

22052

INSTALATION / INSTALACION

PCE-BH0141PCE-BH0128

HOURS / HORAS CYCLES / CICLOS DATE / FECHA

ITEM

SERIAL NUMBER / NUMERO DE SERIENAME / NOMBRE PART NUMBER / NUMERO

DE PARTE

ACUMULATE / ACUMULADO

AIRCRAFT OR COMPONENT / AERONAVE

O COMPONENTE


. 25 - EQUIPMENT/FURNISHING

001.- Rescue hoist cable. 1500 lifts or 4 years. Note 5 BL-9149 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 1500 4 YR RETIREMENT

002.- Hoist connecting plate assembly. Note 5 109-0718-11-113 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 181000 - RETIREMENT

. 32 - LANDING GEAR 003.- Main landing gear strut 109-0503-45-101 0250 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 8000 - RETIREMENT DELETED

004 M i l di t t 109 0503 45 102 0100 03 O t 07 0 0 0 0 0 NEW 354 6 8000

NOT APPLICABLE, EQUIPMENT NOT INSTALLED.


Section 04-10 Retirement lives. AMPI 0B-A-04-10-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-10-00-00A-000A-A (F.A.A.)CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )

DELETED FROM REV. 2 EASA &FAADELETED FROM REV 2 EASA &FAA


004.- Main landing gear strut 109-0503-45-102 0100 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 8000 - RETIREMENT DELETED

005.- Nose landing gear strut 109-0503-44-103 0487 26-Aug-08 163.0 621 0.0 0 191.6 - - 40000 - RETIREMENT - 40621 - - 39381 - S/N 0104 OFF

. 55 - STABILIZER 006.- Left elevator 109-0200-02-601 A7/0597 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3000.0 - - RETIREMENT 3000.0 - - 2645.4 - -007.- Right elevator 109-0200-02-602 A7/0590 03-Oct-07 0.0 0 0.0 NEW 354.6 - 6900.0 - - RETIREMENT 6900.0 - - 6545.4 - -008.- Torque tube clamp assembly 109-0210-03-13 MO.1204 03-Oct-07 0.0 0 0.0 NEW 354.6 - 4000.0 - - RETIREMENT 4000.0 - - 3645.4 - -009.- Torque tube clamp assembly 109-0210-03-13 MO.1219 03-Oct-07 0.0 0 0.0 NEW 354.6 - 4000.0 - - RETIREMENT 4000.0 - - 3645.4 - -

. 62 - MAIN ROTOR 010.- Blade (composite material), Note 3 709-0104-01-111 N212 03-Oct-07 0.0 0 0.0 NEW 354.6 - 8800.0 - - RETIREMENT 8800.0 - - 8445.4 - -011 Blade (composite material) Note 3 709 0104 01 111 P288 15 May 08 118 1 481 0 0 NEW 236 5 8800 0 RETIREMENT 8918 1 8563 5 S/N P276 OFF

DELETED FROM REV. 2 EASA &FAA


011.- Blade (composite material), Note 3 709-0104-01-111 P288 15-May-08 118.1 481 0.0 NEW 236.5 - 8800.0 - - RETIREMENT 8918.1 - - 8563.5 - - S/N P276 OFF

012.- Blade (composite material), Note 3 709-0104-01-111 P278 03-Oct-07 0.0 0 0.0 NEW 354.6 - 8800.0 - - RETIREMENT 8800.0 - - 8445.4 - -013.- Blade (composite material), Note 3 709-0104-01-111 P269 15-May-08 118.1 481 0.0 NEW 236.5 - 8800.0 - - RETIREMENT 8918.1 - - 8563.5 - - S/N P280 OFF

014.- Elastomeric bearing, Note 1 109-0111-04-101 LK1539 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 46000 - RETIREMENT - 46000 - - 44760 -

015.-Elastomeric bearing, Note 1, Each 50 FH, inspectelastomeric bearing. Refer to 0B-A-04-20-00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.

109-0111-04-101 LK1539 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 50.0 - - INSPECTION 350.0 - - -4.6 - -


017Elastomeric bearing, Note 1, Each 50 FH, inspectelastomeric bearing Refer to 0B A 04 20 00 00A 109 0111 04 101 LK1542 25 Nov 09 300 0 1056 0 0 0 0 54 6 50 0 INSPECTION 350 0 4 6


017.- elastomeric bearing. Refer to 0B-A-04-20-00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.



019.-Elastomeric bearing, Note 1, Each 50 FH, inspectelastomeric bearing. Refer to 0B-A-04-20-00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.



021.-Elastomeric bearing, Note 1, Each 50 FH, inspectelastomeric bearing. Refer to 0B-A-04-20-00-00A- 109-0111-04-101 LK1548 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 50.0 - - INSPECTION 350.0 - - -4.6 - -


021. elastomeric bearing. Refer to 0B A 04 20 00 00A000A-A. OR 0B-B-04-20-00-00A-000A-A.

109 0111 04 101 LK1548 25 Nov 09 300.0 1056 0.0 0.0 54.6 50.0 350.0 4.6

022.- Fixed swashplate assembly 109-0110-63-5 L86 03-Oct-07 0.0 0 0.0 NEW 354.6 - 19000.0 - - RETIREMENT 19000.0 - - 18645.4 - -023.- Hub 109-0111-03-109 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 89000 - RETIREMENT

024.- Hub 109-0111-03-113 N357 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 89000 - RETIREMENT - 89000 - - 87760 -025.- Lower fixed half-scissor 109-0110-60-1 MCR00266 03-Oct-07 0.0 0 0.0 NEW 354.6 - 20000.0 - - RETIREMENT 20000.0 - - 19645.4 - -026.- Rotating swashplate 109-0134-03-105 L81 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2300.0 - - RETIREMENT 2300.0 - - 1945.4 - -027.- Rotating swashplate greasing bolt 109-0110-90-107 L174 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -028.- Rotating swashplate greasing bolt 109-0110-90-107 L180 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -029.- Rotating swashplate locking ring 109-0134-11-103 M282 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1200.0 - - RETIREMENT 1200.0 - - 845.4 - -030 Sleeve 109 0110 21 3 MCR00249 03 Oct 07 0 0 0 0 0 NEW 354 6 15000 0 RETIREMENT 15000 0 14645 4

NOT APPLICABLE BY PART NUIMBET INSTALLED.


030.- Sleeve 109-0110-21-3 MCR00249 03-Oct-07 0.0 0 0.0 NEW 354.6 - 15000.0 - - RETIREMENT 15000.0 - - 14645.4 - -031.- Sleeve 109-0110-21-3 MCR00254 03-Oct-07 0.0 0 0.0 NEW 354.6 - 15000.0 - - RETIREMENT 15000.0 - - 14645.4 - -032.- Spherical sleeve 109-0110-04-1 L159 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -033.- Swashplate support 109-0110-05-101 L116 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -034.- Upper fixed half-scissor 109-0110-54-111 MCR00175 03-Oct-07 0.0 0 0.0 NEW 354.6 - 48000.0 - - RETIREMENT 48000.0 - - 47645.4 - -035.- Upper fixed half-scissor fitting 109-0110-38-1 M95 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3400.0 - - RETIREMENT 3400.0 - - 3045.4 - -


Planeación y Servicio alClienteNOTA: EL SIMBOLO ( - ) EN LAS CELDAS SIGNIFICA DATOS NO REQUERIDOS.

G.M.J.P. 1 de 39











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ITEM


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O COMPONENTE

Maintenance Program.Time/Calendar Limited Items Status.Maintenance Program.

Time/Calendar Limited Items Status.

. 63 - MAIN ROTOR DRIVE 036.- Aft rod, Note 3 109-0325-03-113 MO.512 03-Oct-07 0.0 0 0.0 NEW 354.6 - 13000.0 - - RETIREMENT 13000.0 - - 12645.4 - -037.- Aft rod, Note 3 109-0325-03-113 MO.513 03-Oct-07 0.0 0 0.0 NEW 354.6 - 13000.0 - - RETIREMENT 13000.0 - - 12645.4 - -038.- Case assembly 109-0442-01-127 N22 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3300.0 - - RETIREMENT 3300.0 - - 2945.4 - -039.- Central gear 109-0403-25-101 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 17000.0 - - RETIREMENT

040.- Central gear 109-0403-25-103 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 17000.0 - - RETIREMENT

041 - Flange adapter Note 3 109-0425-01-3 244 03-Oct-07 0 0 0 0 0 NEW 354 6 - - 40000 - RETIREMENT - 40000 - - 38760 -

CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )Section 04-10 Retirement lives. AMPI 0B-A-04-10-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-10-00-00A-000A-A (F.A.A.)

DELETED FROM REV. 2 FAADELETED FROM REV. 2 FAA

041.- Flange adapter, Note 3 109-0425-01-3 244 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 40000 - RETIREMENT - 40000 - - 38760 -042.- Flange adapter, Note 3 109-0425-01-3 N652 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 40000 - RETIREMENT - 40000 - - 38760 -043.- Flange adapter, Note 3 109-0425-01-3 P703 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 40000 - RETIREMENT - 40000 - - 38760 -044.- Flange adapter, Note 3 109-0425-01-3 P708 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 40000 - RETIREMENT - 40000 - - 38760 -045.- Forward rod, Note 3 109-0325-02-107 ILS4610G 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -046.- Forward rod, Note 3 109-0325-02-107 ILS4611G 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -047.- Idle gear 109-0403-24-101 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 30000.0 - - RETIREMENT

048.- Idle gear 109-0403-24-103 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 30000.0 - - RETIREMENT

049.- Input pinion 109-0403-23-101 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 30000.0 - - RETIREMENT

050.- Input pinion 109-0403-23-103 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 30000.0 - - RETIREMENT

051 - Lower fitting Note 3 109-0325-08-109 N1036 03-Oct-07 0 0 0 0 0 NEW 354 6 - 41000 0 - - RETIREMENT 41000 0 - - 40645 4 - -

DELETED FROM REV. 2 FAADELETED FROM REV. 2 FAADELETED FROM REV. 2 FAADELETED FROM REV. 2 FAA

051.- Lower fitting, Note 3 109-0325-08-109 N1036 03-Oct-07 0.0 0 0.0 NEW 354.6 - 41000.0 - - RETIREMENT 41000.0 - - 40645.4 - -052.- Lower fitting, Note 3 109-0325-08-109 N1037 03-Oct-07 0.0 0 0.0 NEW 354.6 - 41000.0 - - RETIREMENT 41000.0 - - 40645.4 - -053.- Lower fitting, Note 3 109-0325-08-109 N1038 03-Oct-07 0.0 0 0.0 NEW 354.6 - 41000.0 - - RETIREMENT 41000.0 - - 40645.4 - -054.- Lower fitting, Note 3 109-0325-08-109 N1039 03-Oct-07 0.0 0 0.0 NEW 354.6 - 41000.0 - - RETIREMENT 41000.0 - - 40645.4 - -055.- Lower fixed half-scissor support 109-0110-53-1 OSU 0024 03-Oct-07 0.0 0 0.0 NEW 354.6 - 17000.0 - - RETIREMENT 17000.0 - - 16645.4 - -056.- Main rotor shaft assembly, Note 3 & 4 109-0405-76-109 N384 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - RETIREMENT 10000.0 - - 9645.4 - -057.- Planetary carrier 109-0405-10-105 N62 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 100000 - RETIREMENT - 100000 - - 98760 -058.- Shaft assembly, Note 3 109-0425-41-1 P277 03-Oct-07 0.0 0 592.8 NEW 947.4 - - 134000 - RETIREMENT - 134000 - - 132760 -059.- Shaft assembly, Note 3 109-8412-02-1 P308 03-Oct-07 0.0 0 592.8 NEW 947.4 - - 78000 - RETIREMENT - 78000 - - 76760 -060.- Shaft assembly, Note 3 109-8412-02-3 P248 03-Oct-07 0.0 0 592.8 NEW 947.4 - - 78000 - RETIREMENT - 78000 - - 76760 -061 - Tail rotor drive gear 109-0403-04-3 - 03-Oct-07 0 0 0 0 0 NEW 354 6 - 17000 0 - - RETIREMENT DELETED FROM REV 2 FAA061.- Tail rotor drive gear 109-0403-04-3 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 17000.0 - - RETIREMENT

062.- Tail rotor drive pin 109-0403-05-111 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 14000.0 - - RETIREMENT

063.- Upper case assembly, 109-0402-45-101 N188 03-Oct-07 0.0 0 592.8 NEW 947.4 - - 9800 - RETIREMENT - 9800 - - 8560 -

DELETED FROM REV. 2 FAADELETED FROM REV. 2 FAA


G.M.J.P. 2 de 39











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LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



. 64 - TAIL ROTOR 064.- Blade 709-0160-48-101 N1288 03-Oct-07 0.0 0 1578.5 NEW 1933.1 - 10000.0 - - RETIREMENT 8421.5 - - 8066.9 - -065.- Blade 709-0160-48-101 N1302 03-Oct-07 0.0 0 1578.5 NEW 1933.1 - 10000.0 - - RETIREMENT 8421.5 - - 8066.9 - -066.- Elastomeric bushing, Note 2.- 709-0160V01-101 2918 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - RETIREMENT

067.-Elastomeric bushing, Note 2.- Each 200 FH,inspect elastomeric bushing. Refer to 0B-A-04-20-00 00A 000A A OR 0B B 04 20 00 00A 000A A

709-0160V01-101 2918 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )Section 04-10 Retirement lives. AMPI 0B-A-04-10-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-10-00-00A-000A-A (F.A.A.)

ON CONDITION

00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.

068.- Elastomeric bushing, Note 2.- 709-0160V01-101 2926 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - RETIREMENT

069.-Elastomeric bushing, Note 2.- Each 200 FH,inspect elastomeric bushing. Refer to 0B-A-04-20-00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.

709-0160V01-101 2926 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -


071.-Elastomeric bushing, Note 2.- Each 200 FH,inspect elastomeric bushing. Refer to 0B-A-04-20-00 00A 000A A OR 0B B 04 20 00 00A 000A A

709-0160V01-101 2888 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

ON CONDITION

ON CONDITION

00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.


073.-Elastomeric bushing, Note 2.- Each 200 FH,inspect elastomeric bushing. Refer to 0B-A-04-20-00-00A-000A-A. OR 0B-B-04-20-00-00A-000A-A.

709-0160V01-101 2932 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

074.- Contol lever, Note 3 & 4 109-0040-48-117 22052 03-Oct-07 0.0 0 0.0 NEW 354.6 - 26000.0 - - RETIREMENT 26000.0 - - 25645.4 - -075.- Hub Assembly 109-0131-06-101 N61 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 12000 - RETIREMENT - 12000 - - 10760 -076.- Hub Assembly 109-0131-06-7 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 12000 - RETIREMENT

077.- Link assembly, Note 3 & 4 109-0040-47-1 22052-1 03-Oct-07 0.0 0 0.0 NEW 354.6 - 26000.0 - - RETIREMENT 26000.0 - - 25645.4 - -DELETED FROM REV. 2 FAA

ON CONDITION

078.- Link assembly, Note 3 & 4 109-0040-47-1 22052-2 03-Oct-07 0.0 0 0.0 NEW 354.6 - 26000.0 - - RETIREMENT 26000.0 - - 25645.4 - -079.- Retention Strap Assembly 109-8131-07-1 N1290 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 7200 - RETIREMENT - 7200 - - 5960 -080.- Retention Strap Assembly 109-8131-07-1 N1291 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 7200 - RETIREMENT - 7200 - - 5960 -081.- Retention Strap bolt 709-0160-47-101 N1229 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 22000 - RETIREMENT - 22000 - - 20760 -082.- Retention Strap bolt 709-0160-47-101 N1230 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 22000 - RETIREMENT - 22000 - - 20760 -083.- Strap plug 109-8131-06-1 N910 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 20000 - RETIREMENT - 20000 - - 18760 -084.- Strap plug 109-8131-06-1 N911 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 20000 - RETIREMENT - 20000 - - 18760 -085.- Strap pin 109-8131-08-1 N1118 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 20000 - RETIREMENT - 20000 - - 18760 -086.- Strap pin 109-8131-08-1 N1128 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 20000 - RETIREMENT - 20000 - - 18760 -087.- Supportr, Note 3 & 4 109-0040-49-5 22052 03-Oct-07 0.0 0 0.0 NEW 354.6 - 26000.0 - - RETIREMENT 26000.0 - - 25645.4 - -088.- Lever 109-0130-21-103 MO.253 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -089.- Shaft 109-0130-33-1 MO.226 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -090.- Double lever 109-0130-62-1 MO.197 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -091.- Rod 109-0133-04-109 MO.868 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -092.- Rod 109-0133-04-109 MO.869 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -093.- Lever assembly 109-0130-43-113 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT

094.- Lever assembly 109-0130-43-115 MO.296 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT 16000.0 - - 15645.4 - -095.- Lever assembly 109-0130-60-3 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 16000.0 - - RETIREMENT

096.- Lever 109-0130-60-109 MO.592 07-Mar-08 99.5 446 0.0 NEW 255.1 - 16000.0 - - RETIREMENT 16099.5 - - 15744.9 - - S/N MO.439




G.M.J.P. 3 de 39











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LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



. 65 - TAIL ROTOR DRIVE 097.- 90-degree gearbox gear, Note 3 109-0443-01-103 N248 03-Oct-07 0.0 0 0.0 NEW 354.6 - 41000.0 - - RETIREMENT 41000.0 - - 40645.4 - -098.- 90-degree gearbox pinion, Note 3 109-0433-01-107 N266 03-Oct-07 0.0 0 0.0 NEW 354.6 - 30000.0 - - RETIREMENT 30000.0 - - 29645.4 - -099.- Sleeve mounting 109-0435-31-1 20060842 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3300.0 - - RETIREMENT 3300.0 - - 2945.4 - -100.- Tail rotor shaft assembly 109-0445-08-117 N33 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50000.0 - - RETIREMENT 50000.0 - - 49645.4 - -101.- Tail rotor shaft assembly 109-0445-08-113 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50000.0 - - RETIREMENT

67 ROTOR FLIGHT CONTROL

Section 04-10 Retirement lives. AMPI 0B-A-04-10-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-10-00-00A-000A-A (F.A.A.)CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )


. 67 - ROTOR FLIGHT CONTROL 102.- Main rotor servo actuator 109-0110-42-134 4113 03-Jun-09 249.1 898 0.0 NEW 105.5 - 8000.0 - - RETIREMENT 8249.1 - - 7894.5 - - S/N 4057 OFF

103.- Main rotor servo actuator 109-0110-42-135 6084 28-Sep-07 29.3 148 0.0 NEW 325.3 - 8000.0 - - RETIREMENT 8029.3 - - 7674.7 - - S/N 6058 OFF

104.- Main rotor servo actuator 109-0110-42-136 8056 03-Oct-07 0.0 0 0.0 NEW 354.6 - 8000.0 - - RETIREMENT 8000.0 - - 7645.4 - -105.- Main rotor servo actuator attachment 28007GR90 4533 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -106.- Main rotor servo actuator attachment 28007GR90 4804 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -107.- Main rotor servo actuator attachment 28007GR90 4532 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - RETIREMENT 1000.0 - - 645.4 - -108.- Tail rotor servo actuator, Note 3 & 4 109-0040-51-103 1282 03-Oct-07 0.0 0 0.0 NEW 354.6 - 26000.0 - - RETIREMENT 26000.0 - - 25645.4 - -


G.M.J.P. 4 de 39











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LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



. 62 - MAIN ROTOR

109.-62-01 Elastomeric bearing, Note 1 Refer to 0B-A-04-10-00-00A-000A-A (EASA) / 0B-B-04-10-00-00A-000A-A (F.A.A.)

109-0111-04-101 LK1539 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 46000 - RETIREMENT - 46000 - - 44760 -

110.-62-01 Elastomeric bearing, Inspect for cracking,separation of shims, blowing, rubber powderand/or crumbs.


CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )Section 04-20 Mandatory inspections. AMPI 0B-A-04-20-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-20-00-00A-000A-A (F.A.A.)

and/or crumbs.













64 TAIL ROTOR . 64 - TAIL ROTOR

117.- 64-01 Elastomeric bushing, Inspect for cracking,blowing, rubber powder and/or crumbs 709-0160V01-101 2918 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -





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121.-21-01 Environmental control system.- Do adetailed visual inspection of hot air delivery pipefor condition, 0B-A-21-91-19-00A-281A-B

- - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 2 YR INSPECTION - - 25-Nov-11 - - 542.0

122.-21-02 Environmental control system.- Do ageneral visual inspection of external duct, 0B-A-21-91-18-00A-282A-A

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

Section 04-30 Certification maintenance requirements. AMPI 0B-A-04-30-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-30-00-00A-000A-A (F.A.A.)

Note 1.- This task is necessary all times you do a maintenance task in the areas where the external duct is installed.

CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )

123.-21-03 Environmental control system.- Do anoperation test of 1 and 2 SHUT-OFF switches forcorrect operation. 0B-A-21-91-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 8800.0 - - INSPECTION 8800.0 - - 8445.4 - -

124.-21-04 Environmental control system.- Do anoperation test of shut-off valves (SOV1, SOV2 andPRSOV). 0B-A-21-91-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 8800.0 - - INSPECTION 8800.0 - - 8445.4 - -

21-05 Environmental control system.- Do ageneral visual inspection of bolts that attach air Note 2 - This task is necessary all times you do a maintenance task in the areas where 125.- general visual inspection of bolts that attach airconditioning unit pylon to upper deck structure. 0B-A-21-91-03-00A-282A-A


126.-24-01 Electrical power system.- Do anOperational Check of ESS1 Circuit Breaker foropen circuit failure. 0B-A-24-61-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

127.-24-02 Electrical power system.- Do anOperational Check of ESS2 Circuit Breaker foropen circuit failure. 0B-A-24-61-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

Note 2.- This task is necessary all times you do a maintenance task in the areas where the air conditioning unit is installed.

128.-24-03 Electrical power system.- Do anOperational Check of Bus Tie Circuit Breaker foropen circuit failure. 0B-A-24-61-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

129.-

24-04 Electrical power system Do an OperationalCheck of Contacts A1/A2 of the Battery Bus foropen circuit failure 2000 0B-A-24-32-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

13024-05 Electrical power system.- Do anOperational Check of DC Essential B s 1 Diode 03 Oct 07 0 0 0 0 0 0 0 354 6 2000 0 INSPECTION 2000 0 1645 4130.- Operational Check of DC Essential Bus 1 Diodefor open circuit failure. 0B-A-24-61-00-00A-320C-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

131.-24-06 Electrical power system.- Do anOperational Check of DC Essential Bus 2 Diodefor open circuit failure. 0B-A-24-61-00-00A-320C-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 2000.0 - - INSPECTION 2000.0 - - 1645.4 - -

132.-

24-07 Electrical power system.- Do anOperational Check of Relay K7212 to verify thatthe contacts are not set to the emergency position.0B-A-24-61-00-00A-320D-A

- - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 2000.0 - 1 YR INSPECTION 2300.0 - 25-Nov-10 1945.4 - 176.7

0B A 24 61 00 00A 320D A

133.-

25-01 Rescue hoist system.- Do an OperationalCheck of Rescue Hoist Intermediate Up and DownLimit Switches to confirm automatic speedreduction. 0B-A-25-91-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

134.-

25-02 Rescue hoist system.- Do an OperationalCheck of Rescue Hoist Full-Out and Full-In LimitSwitches to confirm all operations areautomatically stopped.0B-A-25-91-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION Prior first use of day

Prior first use of day

automatically stopped.0B A 25 91 00 00A 320A A


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135.-

25-03 Rescue hoist system.- Do a General VisualInspection of Rescue Hoist Cable Cutter Cotter Pinto ensure cotter pin is correctly installed. 0B-A-25-91-01-00A-281A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

25-04 Rescue hoist system.- Do an Operational

CHAPTER 04-00 AIRWORTHINESS LIMITATIONS, E.A.S.A. APPROVED (Second issue : 2009-06-22 ) / F.A.A. APPROVED ((Second issue : 2009-06-22 )Section 04-30 Certification maintenance requirements. AMPI 0B-A-04-30-00-00A-000A-A (E.A.S.A.) / AMPI 0B-B-04-30-00-00A-000A-A (F.A.A.)


136.-

25 04 Rescue hoist system. Do an OperationalCheck of Rescue Hoist Cable Foul DetectionCircuit to ensure correct operation and that alloperations are automatically stopped. 0B-A-25-91-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

137.-25-05 Rescue hoist system.- Do a general visualinspection of complete cable length for damageand condition. 0B-A-25-91-01-00A-281A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

25-06 Rescue hoist system.- Do an Operational



138.-y

Check of hook assembly bearing for freedom ofrotation. 0B-A-25-91-01-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

139.-

25-07 Rescue hoist system.- Following use in asalt water environment, wash complete cablelength and hook assembly with fresh water, anddry using a clean lint free cloth. 0B-A-25-91-01-00A-258A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - - INSPECTION

25-08 Rescue hoist system - Do an Operational



140.-

25-08 Rescue hoist system.- Do an OperationalCheck of Cable Cut Switch to determine theexistence of dormant closed circuit failures of theswitch guard contact #2 and the push-buttoncontacts #1 and #2. 0B-A-25-91-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -

141.-

26-01 Fire detection system.- Do a check ofpressure-transducer alarm-switch contacts fordormant open circuit failures and integrity switchcontacts for closed circuit failures. 0B-A-26-11-01-00A-340A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 1400.0 - - INSPECTION 1400.0 - - 1045.4 - -

00A 340A A

142.-32-01 Landing gear.- Do an operation test of theemergency extension system. 0B-A-32-31-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 400.0 - - INSPECTION 400.0 - - 45.4 - -

143.-

63-01 Rotor brake system.- Do a general visualinspection of rotor brake disc for damage andcondition. If you find that disc is damaged, replaceit. 0B-A-63-51-03-00A-282A-A


63-02 Rotor brake system - Do an operation test

Note 3.- This task is necessary all times you do a maintenance task in the areas where the rotor brake is installed.

144.-63-02 Rotor brake system.- Do an operation testof pad microswitches for correct operation (4 off).0B-A-63-51-00-00A-320B-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 7000.0 - - INSPECTION 7000.0 6645.4 - -

145.-

63-03 Rotor brake system. Verify that ROTORBRAKE ON warning and ROTOR BRK cautionmessages are correctly generated and shown oncockpit EDU. 0B-A-63-51-00-00A-320A-A

- - 03-Oct-07 0.0 0 0.0 0.0 354.6 - 7000.0 - - INSPECTION 7000.0 6645.4 - -

Note.- 4 This task is necessary after 7000 FH maximum, if, during this period, the rotor brake has not been used.

Note.- 4 This task is necessary after 7000 FH maximum, if, during this period, the rotor brake has not been used.


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146.- 24-01 Starter generator #1 160SG139Q2-1 3012XL2 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - OVERHAUL 1000.0 - - 645.4 - -147.- 24-01 Starter generator #2 160SG139Q2-1 3013XL2 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - - OVERHAUL 1000.0 - - 645.4 - -

148.- 25-01 Rescue hoist 2000 lifts or 5 years. Use limitthat occurs first (Note 1) 109-0900-61-803 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - 2000 5 YR RETIREMENT

149.- 25-02 Cargo hook 200-216-00 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT

150.- 25-03 Cargo hook 109-0705V03-107 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT

151.- 25-04 Safety cargo hook 528-010-01 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT




CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-12-00-00A-000A-A Component overhaul schedule


152.- 25-05 Safety cargo hook 109-0705V03-105 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1000.0 - 5 YR RETIREMENT

153.- 63-01 Main transmission assembly 109-0400-03-113 P63 03-Oct-07 0.0 0 0.0 NEW 354.6 - 4800.0 - - OVERHAUL 4800.0 - - 4445.4 - -

154.- 63-01 Main transmission assembly 109-0400-03-119 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 4800.0 - - OVERHAUL

155.- 65-01 90-degree gearbox assembly 109-0440-01-123 P32 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3000.0 - - OVERHAUL 3000.0 - - 2645.4 - -156.- 67-01 Main rotor servoactuator assembly 109-0110-42-134 4113 03-Jun-09 249.1 898 0.0 NEW 105.5 - 1800.0 - - OVERHAUL 2049.1 - - 1694.5 - - S/N 4057 OFF

157.- 67-02 Main rotor servoactuator assembly 109-0110-42-135 6084 28-Sep-07 29.3 0 0.0 NEW 325.3 - 1800.0 - - OVERHAUL 1829.3 - - 1474.7 - - S/N 6058 OFF

158.- 67-03 Main rotor servoactuator assembly 109-0110-42-136 8056 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1800.0 - - OVERHAUL 1800.0 - - 1445.4 - -159.- 67-04 Tail rotor servoactuator assembly 109-0040-51-103 1282 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1800.0 - - OVERHAUL 1800.0 - - 1445.4 - -



CHAPTER 0B-A-05-13-00-00A-000A-A Discard time schedule160.- 18-01 Vibration absorber assembly 109-0823-29-105 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1200.0 - - OVERHAUL

161.- 18-01 Vibration absorber assembly 109-0823-29-106 ILS3012G 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1200.0 - - OVERHAUL 1200.0 - - 845.4 - -162.- 18-02 Vibration absorber assembly 109-0885-28-105 NOT APPLICABLE 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1200.0 - - OVERHAUL 1200.0 - - 845.4 - -

163.- 25-01 ELT battery pack. Note 1 EXP. BATT04/2012 455-5049-345 A00057 30-Apr-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 29-Apr-12 - - 697.7

164.- 25-01 ELT battery pack. By F.A.R. 91.207 455-5049-345 A00057 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7165.- 25-02 First aid kit. Note 2 999-9001-02-105 UNK 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7166.- 25-03 Rescue hoist cable cutter cartridge BL-11140-1 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT

167.- 25-03 Rescue hoist cable cutter cartridge BL-11140-1 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 9 YR RETIREMENT CARTRIDGE FROM DATEOF MANUFACTURE




168.- 26-01 Portable fire extinguisher A072A02 01-2007/04998 31-Jan-07 0.0 0 0.0 NEW 354.6 - - - 10 YR RETIREMENT - - 30-Jan-17 - - 2435.0 FROM DATE OFMANUFACTURE

169.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 31-May-06 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 30-May-21 - - 4016.2 FROM DATE OFMANUFACTURE

170.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION

171.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 31-May-06 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 30-May-21 - - 4016.2 FROM DATE OFMANUFACTURE

172.- 26-02 Fire extinguishing cartridges MAIN 30600-22 MD 05/06 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION

173.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 27-Feb-22 - - 4289.2 FROM DATE OFMANUFACTURE

174.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION

175.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 15 YR RETIREMENT - - 27-Feb-22 - - 4289.2 FROM DATE OFMANUFACTURE

176.- 26-02 Fire extinguishing cartridges ALTN 30600-22 MD 02/07 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 12 YR RETIREMENT - - 03-Oct-19 - - 3410.5 FROM DATE OFINSTALLATION

177.- 28-01 Fuel filter element KD651510 NOT APPLICABLE 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 1 YR RETIREMENT 700.0 - 25-Nov-10 345.4 - 176.7178.- 32-01 Snow ski restraint cables and bungee cords 109-0811-73-123 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT

179.- 32-01 Snow ski restraint cables and bungee cords 109-0811-73-125 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT

180.- 32-01 Snow ski restraint cables and bungee cords 109-0812-01-101 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT

181.- 32-01 Snow ski restraint cables and bungee cords 000-1034701/-02 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT

182.- 32-02 Slump pad bungee cords 109-0811-73-119 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2183.- 32-02 Slump pad bungee cords 109-0811-73-121 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2184.- 32-02 Slump pad bungee cords 109-0811-73-133 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR RETIREMENT - - 02-Oct-10 - - 123.2185.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1539 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7186.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1542 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7





g187.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1543 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7188.- 62-01 Elastomeric bearing. Note 2 109-0111-04-101 LK1548 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 02-Oct-12 - - 853.7189.- 63-01 Toothed belt. Note 3 109-0455-09-103 R300821 25-Nov-09 300.0 1056 0.0 NEW 54.6 - 800.0 - 2 YR RETIREMENT 1100.0 - 25-Nov-11 745.4 - 542.0 S/N P298821 OFF

190.- 63-01 Toothed belt. Note 3 109-0455-09-103 R300220 25-Nov-09 300.0 1056 0.0 NEW 54.6 - 800.0 - 2 YR RETIREMENT 1100.0 - 25-Nov-11 745.4 - 542.0 S/N P298822 OFF

191.- 64-01 Elastomeric bushing. Note 4 709-0160v01-101 2918 31-Dec-05 0.0 0 0.0 NEW 354.6 - - - 5 YR RETIREMENT - - 31-Dec-10 - - 212.7 FROM DATE OFMANUFACTURE




195.- 76-01 Engine out microswitch 83778324 - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 4000.0 - - OVERHAUL 4000.0 - - 3645.4 - -


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196.- 0B-A-05-41-00-01A-000A-A Airworthiness checks A109S 22052 03-Oct-07 0.0 0 0.0 0.0 0.0 0.0 - - - INSPECTION - - - - - - PREFLIGHT

197.- 0B-A-05-41-00-01A-000A-A Airworthiness checks A109S 22052 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 100.0 - - INSPECTION 400.0 - - 45.4 - -

198.- 0B-A-05-41-00-01A-000A-A Airworthiness checks A109S 22052 03-Oct-07 0.0 0 0.0 0.0 0.0 0.0 400.0 - - INSPECTION 400.0 - - 45.4 - -

199 - 0B A 05 41 00 01A 000A A Airworthiness checks A109S 22052 03 Oct 07 0 0 0 0 0 0 0 0 0 0 0 800 0 - - INSPECTION 800 0 445 4

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-41-00-00A-000A-A Standard inspection program



201.- 0B-A-05-41-00-02A-000A-A 100-hour inspections A109S 22052 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 100.0 - - INSPECTION 400.0 - - 45.4 - - Tolerance 10hours

202.-0B-A-05-41-00-02A-000A-A 100-hour inspections.62-02 (For pitch change links with more than 800hours) Pitch change links (removal required)

A109S 22052 03-Oct-07 0.0 0 0.0 0.0 354.6 354.6 800.0 - - INSPECTION 800.0 - - 445.4 - INITIAL

0B A 05 41 00 02A 000A A 100 hour inspections203.-

0B-A-05-41-00-02A-000A-A 100-hour inspections.62-02 (For pitch change links with more than 800hours) Pitch change links (removal required)

A109S 22052 - 800.0 - 0.0 0.0 -445.4 -445.4 100.0 - - INSPECTION 900.0 - - 545.4 - SUBSEQUENT

204.- 0B-A-05-41-00-03A-000A-A 400-hour inspections A109S 22052 03-Oct-07 0.0 0 0.0 0.0 354.6 354.6 400.0 - - INSPECTION 400.0 - - 45.4 - - Tolerance 10hours



207.- 0B-A-05-41-00-06A-000A-A 12-month inspections A109S 22052 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7 Tolerance 3monthsmonths

208.- AIRCRAFT REWEIHGHT BY F.A.A. FAR 135 & D.G.A.C.NOM-043/2-SCT3-2001 A109S 22052 07-Sep-07 0.0 0 0.0 0.0 354.6 354.6 - - 3 YR INSPECTION - - 06-Sep-10 - - 97.2 PART A LOG

BOOK

209.- ALTIMETER INSPECTION BY F.A.A. FAR 91.411 3A67-32-20F-05-1KR 1044549 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 PART B LOGBOOK

210.- ALTIMETER INSPECTION BY F.A.A. FAR 91.411 3A43-22-20F-05-1FU 1044838 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 PART B LOGBOOK

211.- ALTIMETER INSPECTION BY F.A.A. FAR 91.411 3A43-22-20F-05-1FU 1044754 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 PART B LOGBOOK

212.- PITOT/STATIC INSPECTION BY F.A.A. FAR 91.411 109-0720-61-103 (PITOT TUBE ASSY) - 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 PART B LOG

BOOK

213.- ATC TRANSPONDER INSPECTION BY F.A.A. FAR 91.413 066-01141-0101 3383 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 S/N 3219 OFF

214.- ATC TRANSPONDER AND ENCODER ALTIMETERALTIMETER INSPECTION BY F.A.A. FAR 91.411 A109S 22052 29-Jun-09 249.1 898 0.0 0.0 105.5 105.5 - - 2 YR INSPECTION - - 29-Jun-11 - - 393.0 PART B LOG

BOOK

215.- INSPECTION ELT BY FAR 91.207 455-5049-345 A00057 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

216.- COMPASS CALIBRATION BY D.G.A.C. NOM-043/2-SCT3-2001 C 2300L4-24B AG-2403 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

217.- COMPASS CALIBRATION BY D.G.A.C. NOM-043/2-SCT3-2001 C 2300L4-24B AG-2407 25-Nov-09 300.0 1056 0.0 0.0 54.6 54.6 - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7


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218.- 00-01 Obey with the requirements for inspectionsof optional equipment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

219.-

24-01 Starter-generators. Examine brushes (onlyif APC standard or XL brushes are installed) forwear. Examine commutator contacts for wear,pitting and burnings.

160SG139Q2-1 3012XL2 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 300.0 - - INSPECTION 600.0 - - 245.4 - -

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-44-00-00A-000A-A Special inspections

Obey with the requirements for inspections of optional equipment.

220.-

24-01 Starter-generators. Examine brushes (onlyif APC standard or XL brushes are installed) forwear. Examine commutator contacts for wear,pitting and burnings.

160SG139Q2-1 3013XL2 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 300.0 - - INSPECTION 600.0 - - 245.4 - -

221.-29-01 Hydraulic pumps Examine splines ofexternal drive shafts for wear (hydraulic pump P/N109-0760-42-103 only).

109-0760-42-103 BH304 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - INSPECTION 1600.0 - - 1245.4 - -

22229-01 Hydraulic pumps Examine splines of

t l d i h ft f (h d li P/N 109 0760 42 103 BH303 03 O t 07 0 0 0 0 0 NEW 354 6 1600 0 1600 0 1245 4222.- external drive shafts for wear (hydraulic pump P/N109-0760-42-103 only).

109-0760-42-103 BH303 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - INSPECTION 1600.0 - - 1245.4 - -

223.-32-01 Landing gear actuators (helicopters whichoperate over sea and/or in high humidity),Examine for corrosion and damage.

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 900.0 - 3 YR INSPECTION 900.0 - 02-Oct-10 545.4 - 123.2

224.-32-02 Landing gear actuators (helicopters whichdo not operate over sea and/or in high humidity)Examine for corrosion and damage.

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1800.0 - 6 YR INSPECTION 1800.0 - 02-Oct-13 1445.4 - 1219.0

225.-

62-01 Main rotor dampers Examine for conditionand unusual play of bearings. Note 2.- 2 Only ifyou apply the extended and progressive inspectionprograms.

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 25.0 - - INSPECTION

226.- 62-02 Main rotor dampers Examine for condition andexcessive play of bearings. 109-0112-39-103 0228 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 150.0 - - INSPECTION 450.0 - - 95.4 - - S/N 0244 OFF

227.- 62-02 Main rotor dampers Examine for condition andexcessive play of bearings. 109-0112-39-103 0526 28-Jan-10 318.3 1116 0.0 0.0 36.3 - 150.0 - - INSPECTION 468.3 - - 113.7 - -

228.- 62-02 Main rotor dampers Examine for condition andexcessive play of bearings. 109-0112-39-103 0707 28-Jan-10 318.3 1116 0.0 0.0 36.3 - 150.0 - - INSPECTION 468.3 - - 113.7 - -

229 - 62-02 Main rotor dampers Examine for condition and 109-0112-39-103 0957 17-Mar-10 328 4 1150 0 0 0 0 26 2 - 150 0 - - INSPECTION 478 4 - - 123 8 - - S/N 0747 OFF

NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.

229.- pexcessive play of bearings. 109-0112-39-103 0957 17-Mar-10 328.4 1150 0.0 0.0 26.2 - 150.0 - - INSPECTION 478.4 - - 123.8 - - S/N 0747 OFF

230.-62-03 Swashplate duplex bearing (pitch change links androtating scissors disconnection necessary) Examine for noiseand roughness of rotation.

- - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 2 YR INSPECTION 700.0 - 25-Nov-11 345.4 - 542.0

231.- 62-04 Main rotor dampers Remove from helicopter and sendto Manufacturer for special inspection. 109-0112-39-103 0228 25-May-09 249.1 898 329.1 NEW 434.6 - 1200.0 - - INSPECTION 1449.1 - - 1094.5 - - S/N 0244 OFF

232.- 62-04 Main rotor dampers Remove from helicopter and sendto Manufacturer for special inspection. 109-0112-39-103 0526 28-Jan-10 318.3 1116 0.0 REPAIRED 36.3 - 1200.0 - - INSPECTION 1518.3 - - 1163.7 - -

VER FAA 8130-3 PARADETERMINAR EL TIEMPOTOTAL DEL DAMPER

233.- 62-04 Main rotor dampers Remove from helicopter and sendto Manufacturer for special inspection. 109-0112-39-103 0707 03-Oct-07 0.0 0 0.0 REPAIRED 354.6 - 1200.0 - - INSPECTION 1200.0 - - 845.4 - -


234.- 62-04 Main rotor dampers Remove from helicopter and sendto Manufacturer for special inspection. 109-0112-39-103 0957 17-Mar-10 328.4 1150 0.0 NEW 26.2 - 1200.0 - - INSPECTION 1528.4 - - 1173.8 - -



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235.-62-05 Main rotor blades (removal necessary) Examine bladeand its bushings for wear, nicks and conditions. Examinecontact areas with grips for condition.

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -

236.- 62-06 Main rotor head control levers (removal necessary)Examine for condition, damage and wear. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -

62 07 M i t bl d i ( l ) E i

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-44-00-00A-000A-A Special inspections

237.-62-07 Main rotor blade grips (removal necessary) Examinefor condition, damage and wear. Examine contact areas withblades for condition and washer bondage.


238.-62-08 Main rotor flapping and drop restraint mechanism(removal necessary) Examine for condition, damage andwear.


239.- 62-09 Main rotor head and installation components (removalnecessary) Do a detailed examination. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -

240.- 62-10 Hub floating ring Examine for wear. Examine DUwashers and internal Teflon shim for debonding - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2400.0 - - INSPECTION 2400.0 - - 2045.4 - -washers and internal Teflon shim for debonding.

241.-62-11 Swashplate (removal and disassembly necessary)Examine duplex bearing for damage and corrosion. Examineteflon rings for wear. Examine swashplate guides and pivotsleeve slots for damage and wear.


242.- 63-01 Main transmission chip detectors Do operational test . - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR INSPECTION 500.0 - 25-Nov-10 145.4 - 176.7

243.- 63-02 Freewheel units (removal necessary) Examinecomponents and tracks for wear and damage. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1200.0 - - INSPECTION 1200.0 - - 845.4 - -

244.- 63-03 Hydraulic pump drive quill, Examine for wear. 109-0760-42-103 BH304 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - INSPECTION 1600.0 - - 1245.4 - -

245.- 63-03 Hydraulic pump drive quill, Examine for wear. 109-0760-42-103 BH303 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - INSPECTION 1600.0 - - 1245.4 - -

246.- 64-01 Tail rotor Do a check for correct dynamic balance. - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

247.-64-02 Blade elastomeric bushings and related hub contactareas (blade removal necessary) Examine for condition,fretting and wear. Note 3.- Only if you apply the standardinspection program.

- - 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

64-03 Blade retention bolts (removal necessary) Examine for248.-

64-03 Blade retention bolts (removal necessary) Examine forcondition, corrosion and nicks. Note 3.- Only if you apply thestandard inspection program.

- - 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

249.-64-04 Bushings on flapping axis. Examine for wear and localdebonding of teflon lining. Note 3.- Only if you apply thestandard inspection program.

- - 08-Dec-08 193.6 716 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -

250.- 65-01 90-degree gearbox chip detector Do operational test. - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR INSPECTION 500.0 - 25-Nov-10 145.4 - 176.7

251.-65-02 90-degree gearbox Examine gearing teeth for unusualprints, pitting, scoring, damage. Examine and bearings for - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - INSPECTION 1600.0 - - 1245.4 - -251. p , p g, g, g gfreedom rotation and roughness.

03 Oct 07 0.0 0 0.0 NEW 354.6 600 0 1600.0 1245.4


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252.- 29-01 Utility hydraulic system accumulators (2 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Fill with nitrogen 500.0 - 25-Nov-10 145.4 - 176.7

253.- 29-02 Flight control hydraulic system accumulators (2 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Fill with nitrogen 500.0 - 25-Nov-10 145.4 - 176.7

254.- 32-01 Main landing gear strut torque links - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Grease 500.0 - 25-Nov-10 145.4 - 176.7

255.- 32-02 Nose landing gear strut torque links and steeringsupport - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Grease 500.0 - 25-Nov-10 145.4 - 176.7

256 32 03 M i l di t t (2 ff) 25 Nov 09 300 0 1056 0 0 0 0 54 6 1 YR Fill ith it 25 Nov 10 176 7

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-45-00-00A-000A-A Servicing

256.- 32-03 Main landing gear struts (2 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Fill with nitrogen - - 25-Nov-10 - - 176.7257.- 32-03 Main landing gear struts (2 off) - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - Fill with fluid 1600.0 - - 1245.4 - -258.- 32-04 Nose landing gear strut - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Fill with nitrogen - - 25-Nov-10 - - 176.7259.- 32-04 Nose landing gear strut - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 1600.0 - - Fill with fluid 1600.0 - - 1245.4 - -260.- 32-05 Landing gear wheel tires (3 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Fill with nitrogen 500.0 - 25-Nov-10 145.4 - 176.7

261.- 32-06 Wheel bearings (Note 2.- Only when the helicopteroperates in salt laden atmosphere. ) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR Grease - - 25-Nov-10 - - 176.7

262.- 62-01 Main rotor blade (4 off) (Note 2.- Only when thehelicopter operates in salt laden atmosphere. ) - - 11-Mar-08 99.5 446 0.0 NEW 255.1 - - - 7 DAYS Apply surface protection Note 2.- Only when the helicopter operates in salt laden atmosphere.

263.- 62-02 Main rotor floating ring and droop stop plates - - 17-Mar-10 341.5 1177 0.0 -8.5 13.1 - 50.0 - 3 MO Grease 400.0 - 16-Jun-10 45.4 - 14.8

264.- 62-03 Swashplate (3 places) - - 17-Mar-10 341.5 1177 0.0 -8.5 13.1 - 50.0 - 3 MO Grease 400.0 - 16-Jun-10 45.4 - 14.8265.- 63-01 Main transmission - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 1 YR Change of oil 700.0 - 25-Nov-10 345.4 - 176.7

266.- 64-01 Tail rotor pitch change mechanism duplex bearing - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 2 YR Grease 700.0 - 25-Nov-11 345.4 - 542.0

267.- 65-01 90-degree gearbox - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - 6 MO Change of oil 400.0 - 26-May-10 45.4 - -5.9

268.- 65-02 Tail rotor drive shaft bearings (7 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 300.0 - - Grease 600.0 - - 245.4 - -

269.- 67-01 Main rotor servo actuators (3 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 200.0 - 1 YR Grease 500.0 - 25-Nov-10 145.4 - 176.7

270.- 67-02 Main rotor servo actuator levers (3 off) - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 1 YR Apply surface protection 700.0 - 25-Nov-10 345.4 - 176.7

271.- 67-03 Tail rotor servo actuator lever - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 400.0 - 1 YR Apply surface protection 700.0 - 25-Nov-10 345.4 - 176.7

272.- 71-01 Engines (2 off) Note 3. Refer to the enginemaintenance manual for the oil change interval. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - Change of oil Note 3. Refer to the engine maintenance manual for the oil change interval.


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273.- 00-01 Obey with the requirements for inspectionsof optional equipment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

274.-

18-01 Vibration absorber-to-fuselage attachmentbolts, Examine for correct torque. (Note 1 If youfound that the torque is not in the approved limits,do a torque check again after 5 thru 10 hours offlight ) 5 thru 10 hours of flight when the

- - 10-Sep-07 8.3 8 0.0 NEW 346.3 - 10.0 - - INSPECTION COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )

Obey with the requirements for inspections of optional equipment.

CHAPTER 0B-A-05-51-00-00A-000A-A Out of phase inspections – General

flight.) 5 thru 10 hours of flight, when thehelicopter is new, or after the installation of avibration absorber.

275.- 32-01 Wheel half rims Examine for cracks andcorrosion. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

276.- 52-01 Emergency jettison mechanism Examinefor correct operation. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

53-01 Tail boom attachment bolts Examine forcorrect torque. (Note 1 If you found that the torque

At each removal of a cockpit door.

After each removal of a wheel tire.

277.- is not in the approved limits, do a torque checkagain after 5 thru 10 hours of flight.) 5 thru 10hours of flight, when the helicopter is new, or afterthe installation of the tail boom.

- - 10-Sep-07 8.3 8 0.0 NEW 346.3 - 10.0 - - INSPECTION

278.-62-01 Tape on leading edges of main rotor blades(if installed) Examine for proper adhesion,condition, wrinkles, lifting or breaking at edges.


COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.

Before the first flight of a day.

279.-

62-02 Main rotor head ring nut bolts Examine forcorrect torque. (Note 1 If you found that the torqueis not in the approved limits, do a torque checkagain after 5 thru 10 hours of flight.) 5 thru 10hours of flight, when the helicopter is new, or afterthe installation of the main rotor.


280.- 62-03 Blade pins Examine for condition, nicksand wear. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

63 01 U t i tt h t t

After each removal of a main rotor blade.


281.-

63-01 Upper cover-to-main case attachment nutsExamine for correct torque. (Note 1 If you foundthat the torque is not in the approved limits, do atorque check again after 5 thru 10 hours of flight.)5 thru 10 hours of flight, when the helicopter isnew, or after the installation of the maintransmission.


282.- 63-02 Fan pulleys Examine for condition,damage and wear. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

283 63-03 Fan bearings Examine for excessive play 03 Oct 07 0 0 0 0 0 NEW 354 6 INSPECTION


After each removal of a fan belt

After each removal of a fan belt.

283.- g p yand roughness. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

284.-

65-01 Mounting sleeve attachment bolts Examinefor correct torque. (Note 1 If you found that thetorque is not in the approved limits, do a torquecheck again after 5 thru 10 hours of flight.) 5 thru10 hours of flight, when the helicopter is new, orafter the installation of the 90-degree gearbox.


After each removal of a fan belt.



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285.-

71-01 Exhaust ejector-to-saddle attachmentbolts Examine for correct torque. (Note 1 If youfound that the torque is not in the approved limits,do a torque check again after 5 thru 10 hours offlight.) 5 thru 10 hours of flight, when thehelicopter is new, or after the installation of anengine exhaust ejector.

- - 10-Sep-07 8.3 8 0.0 NEW 346.3 - 10.0 - - INSPECTION COMPIED WITH SPECIAL INSPECTION AT 8:20 HRS, SEP-10-2007 BY AGUSTA.

CHAPTER 0B-A-05-51-00-00A-000A-A Out of phase inspections – GeneralCHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )

engine exhaust ejector.

286.- 71-02 Engine fitting-to-engine mountattachment nuts Examine for correct torque. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

287.- 71-03 Engine mount-to-fuselage attachmentnuts Examine for correct torque. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

288.- 71-04 Engine mount supports Examine forcorrosion, wear and elongation of bolt holes. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

Before each removal of an engine.

After each removal of an engine.

CHAPTER 0B A 05 70 01 00A 000A A S h d l d/ h d l d i ti R t b k t

After each removal of an engine.

289.- Rotor brake Examine for leaks. SIP -Airworthiness check - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

290.- Rotor brake Examine for leaks. EIP - 50 hours /30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

291.- Rotor brake Examine for leaks. PIP - 50 hours /30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

292.- Disk flange support Examine for security. SIP -100 hours

- - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

293.- Disk flange support Examine for security. EIP -200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

CHAPTER 0B-A-05-70-01-00A-000A-A Scheduled/unscheduled inspections - Rotor brake system



NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.200 hours

294.- Disk flange support Examine for security. PIP -200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

295.- Rotor brake linings Examine for wear. SIP - 400hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 400.0 - - INSPECTION 400.0 - - 45.4 - -

296.- Rotor brake linings Examine for wear. EIP - 400hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 400.0 - - INSPECTION

297.- Rotor brake linings Examine for wear. PIP - 400hours - PH 1 - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 400.0 - - INSPECTION

298.- Rotor brake control cable Do operation test. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7




298.- Rotor brake control cable Do operation test. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

299.- Rotor brake control cable Do operation test. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

300.- Rotor brake control cable Do operation test. PIP - 12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.



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301.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. SIP - 100 hours - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

302.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. EIP - 200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

303 Bleed air lines, pipes, joints and fittings. Examine 03 Oct 07 0 0 0 0 0 NEW 354 6 200 0 INSPECTION



NOT APPLICABLE AIRCRAFT IN STANDAR PROGRAM

CHAPTER 0B-A-05-70-02-00A-000A-A Scheduled/unscheduled inspections - Environmental control system

303.- , p p , j gfor condition and security. PIP - 200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

304.- Bleed air overtemperature switch. Do function test.SIP - 100 hours - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

305.- Bleed air overtemperature switch. Do function test.EIP - 200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

306.- Bleed air overtemperature switch. Do function test.PIP - 200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

307.- Environmental control system. Do operation test. SIP - 12months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7




308.- Environmental control system. Do operation test. EIP - 12months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

309.- Environmental control system. Do operation test. PIP - 12months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

310.-

Heat exchanger Do detailed examination SI - 400hours (Note 1.- Only after the first 400 hours ofoperations. Subsequently do the inspection at 200hours interval.)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 400.0 - - INSPECTION 400.0 - - 45.4 - - INITIAL

Heat exchanger Do detailed examination SI - 400hours (Note 1 - Only after the first 400 hours of



311.- hours (Note 1.- Only after the first 400 hours ofoperations. Subsequently do the inspection at 200hours interval.)

- - - 400.0 - 0.0 NEW -45.4 - 200.0 - - INSPECTION 600.0 - - 245.4 - - SUBSEQUENT

312.- Heat exchanger (Note 2.- Heat exchangeroverhaul interval 3000 hours.) - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3000.0 - - OVERHAUL 3000.0 - - 2645.4 - -

313.- Turbine - blower (Note 3) Lubricate SER - 600hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 600.0 - - SERVICE 600.0 - - 245.4 - -

314.- Turbine - blower (Note 3.- Turbine-blower overhaulinterval 5000 hours.) - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 5000.0 - - OVERHAUL 5000.0 - - 4645.4 - -

CHAPTER 0B-A-05-70-03-00A-000A-A Scheduled/unscheduled inspections - Cabin heating and ventilation system

315.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. SIP - 100 hours - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

316.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. EIP - 200 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

317.- Bleed air lines, pipes, joints and fittings. Examinefor condition and security. PIP - 200 hours - PH C - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION

318.- Cabin heating and ventilation system. Do operation test. SIP -12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7



12 months

319.- Cabin heating and ventilation system. Do operation test. EIP -12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

320.- Cabin heating and ventilation system. Do operation test. PIP -12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

321.- Flexible duct external to hot air delivery tube.Examine for damage. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

322.- Hot air delivery tube (flexible duct removalnecessary). Do a detailed inspection. SI - 2 years - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 2 YR INSPECTION - - 25-Nov-11 - - 542.0

OPI - When you do a maintenance operation in an area adjacent to the flexible duct.




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323.- ELT case and antenna. Examine for correct installation. SIP -12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

324.- ELT case and antenna. Examine for correct installation. EIP - 12months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

325.- ELT case and antenna. Examine for correct installation. PIP - 12months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

326 - Battery pack Examine for corrosion SIP - 12 months - - 25-Nov-09 300 0 1056 0 0 0 0 54 6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176 7


CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-70-04-00A-000A-A Scheduled/unscheduled inspections - Emergency locator transmitter system


326.- Battery pack. Examine for corrosion. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

327.- Battery pack. Examine for corrosion. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

328.- Battery pack. Examine for corrosion. PIP - 12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

329.- Controls and crash sensor. Do operation test. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

330.- Controls and crash sensor. Do operation test. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

331.- Controls and crash sensor. Do operation test. PIP - 12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION





332.- Antenna. Do a check of radiated signal. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

333.- Antenna. Do a check of radiated signal. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

334.- Antenna. Do a check of radiated signal. PIP - 12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

335.- Engine compartment fire extinguishing system. Do operationtest. SIP - 12 months - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

336.- Engine compartment fire extinguishing system. Do operation test. EIP -12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

337.- Engine compartment fire extinguishing system. Do operation test. PIP -12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION





CHAPTER 0B-A-05-70-05-00A-000A-A Scheduled/unscheduled inspections - Engine compartment fire extinguishing system

12 months PH I

338.- Bottle cartridge. Do bridge wire resistance test. SI - 3 years - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 3 YR INSPECTION - - 02-Oct-10 - - 123.2

339.- Bottles. Weigh. SI - 12 months 27300-1 1042 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7340.- Bottles. Weigh. SI - 12 months 27300-1 1046 25-Nov-09 300.0 1056 0.0 0.0 54.6 - - - 1 YR INSPECTION - - 25-Nov-10 - - 176.7

341.-

Bottles. Do hydrostatic test SI - 5 years (Note 1.- To do thehydrostatic test, refer to the instructions printed on the decalsof the bottles. The bottles must be removed from thehelicopter. Refer to 0B-A-26-21-01-00A-520A-A and 0B-A-26-22-01-00A-520A-A.)

27300-1 1042 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 5 YR HYDROSTATIC TEST - - 28-Feb-12 - - 636.7

342.-

Bottles. Do hydrostatic test SI - 5 years (Note 1.- To do thehydrostatic test, refer to the instructions printed on the decalsof the bottles. The bottles must be removed from thehelicopter. Refer to 0B-A-26-21-01-00A-520A-A and 0B-A-26-22-01-00A-520A-A.)

27300-1 1046 28-Feb-07 0.0 0 0.0 NEW 354.6 - - - 5 YR HYDROSTATIC TEST - - 28-Feb-12 - - 636.7

343.-Bottles. Do operation test of discharge heads tomake sure that they operate when necessary. SI -10000 h

27300-1 1042 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -

344.-Bottles. Do operation test of discharge heads tomake sure that they operate when necessary. SI -10000 h

27300-1 1046 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -10000 h

345.- FIRE EXT circuit breakers. Do operation test fordormant open circuit failures. SI - 10000 h - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 10000.0 - - INSPECTION 10000.0 - - 9645.4 - -

346.-

Fire extinguisher control panel. Do operation testof BTL switch and ENG 1 and ENG 2 lighted push-button switches for open circuit failures. This tomake sure that they operate when necessary. SI -10000 h



G.M.J.P. 16 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



347.- Landing/search light. Examine for condition andsecurity. SIP - Airworthiness check - - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - -

348.- Landing/search light. Examine for condition andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

349.- Landing/search light. Examine for condition andsecurity. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION


CHAPTER 0B A 05 70 07 00A 000A A S h d l d/ h d l d i ti R h i t i t ll ti

CHAPTER 0B-A-05-70-06-00A-000A-A Scheduled/unscheduled inspections - Landing/search light system



350.-Hoist mount, fittings and adjacent fuselage area.Examine for condition, damage and security. SIP -Airworthiness check


351.-Hoist mount, fittings and adjacent fuselage area.Examine for condition, damage and security. EIP -50 hours / 30 days

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

352.-Hoist mount, fittings and adjacent fuselage area.Examine for condition, damage and security. PIP -50 hours / 30 days



CHAPTER 0B-A-05-70-07-00A-000A-A Scheduled/unscheduled inspections. Rescue hoist installation



353.- Hoist. Examine for oil leaks. SIP - Airworthinesscheck - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

354.- Hoist. Examine for oil leaks.. EIP - 50 hours / 30days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

355.- Hoist. Examine for oil leaks.. PIP - 50 hours / 30days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

356.-Hoist motor and cable cutter electricalconnections. Examine for condition and security.SIP - Airworthiness check


Hoist motor and cable cutter electrical





357.-Hoist motor and cable cutter electricalconnections. Examine for condition and security.EIP - 50 hours / 30 days


358.-Hoist motor and cable cutter electricalconnections. Examine for condition and security.PIP - 50 hours / 30 days


359.-

Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed. This to present hookmovement when helicopter is in flight. SIP -Airworthiness check

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.



Airworthiness check

360.-

Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed. This to present hookmovement when helicopter is in flight. EIP - 50hours / 30 days


361 -

Hoist hook and spring bumper. Examine to makesure that hook is safety homed and spring bumpersufficiently compressed This to present hook - - 03-Oct-07 0 0 0 0 0 NEW 354 6 - 50 0 - 30 DAYS INSPECTION


NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.361.- sufficiently compressed. This to present hookmovement when helicopter is in flight. PIP - 50hours / 30 days


362.- Hoist cable attaching screw. Examine for security.SIP - Airworthiness check - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

363.- Hoist cable attaching screw. Examine for security.EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

364.- Hoist cable attaching screw. Examine for security.PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION






G.M.J.P. 17 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



365.- Step bar protection. Examine for condition andsecurity. SIP - Airworthiness check - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

366.- Step bar protection. Examine for condition andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

367.- Step bar protection. Examine for condition andit PIP 50 h / 30 d - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION


CHAPTER 0B-A-05-70-07-00A-000A-A Scheduled/unscheduled inspections. Rescue hoist installation




367. security. PIP - 50 hours / 30 days 03 Oct 07 0.0 0 0.0 NEW 354.6 50.0 30 DAYS INSPECTION

368.-Manual cable cutter, operator harness andharness ring. Examine for condition. SIP - 100hours


369.-Manual cable cutter, operator harness andharness ring. Examine for condition. EIP - 200hours


370.-Manual cable cutter, operator harness andharness ring. Examine for condition. PIP - 200hours - PH C

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 200.0 - - INSPECTION NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.




371.-Hoist support frame assembly and back-upstructure. Do a detailed visual examination forcracks, corrosion and damage. SIP - 100 hours


372.-Hoist support frame assembly and back-upstructure. Do a detailed visual examination forcracks, corrosion and damage. EIP - 200 hours


373

Hoist support frame assembly and back-upstructure. Do a detailed visual examination for 03 O t 07 0 0 0 0 0 NEW 354 6 200 0 INSPECTION


NOT APPLICABLE AIRCRAFT IN STANDAR PROGRAM


373.- structure. Do a detailed visual examination forcracks, corrosion and damage. PIP - 200 hours -PH C


374.- Hoist cable cut circuit breakers. Do an operationtest to detect open circuit failures. SIP - 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION

375.- Hoist cable cut circuit breakers. Do an operationtest to detect open circuit failures. EIP - 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION

376.- Hoist cable cut circuit breakers. Do an operationtest to detect open circuit failures PIP 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION




NOT APPLICABLE, AIRCRAFT IN STANDAR PROGRAM.test to detect open circuit failures. PIP - 800 hours

377.- Hoist cable cut isolation relays. Do an operationtest to detect open circuit failures. SIP - 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION

378.- Hoist cable cut isolation relays. Do an operationtest to detect open circuit failures. EIP - 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION

379.- Hoist cable cut isolation relays. Do an operationtest to detect open circuit failures. PIP - 800 hours - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 800.0 - - INSPECTION




380.-Hoist cable cut (pilot cyclic stick grip). Do anoperation test to detect open circuit failures. SIP -800 hours


381.-Hoist cable cut (pilot cyclic stick grip). Do anoperation test to detect open circuit failures. EIP -800 hours


382.-Hoist cable cut (pilot cyclic stick grip). Do anoperation test to detect open circuit failures. PIP -800 hours






G.M.J.P. 18 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



383.- Rescue hoist installation Do a detailed inspection. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

384.- Cable swaged ball end. Examine for security of attachment. - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - - INSPECTION

385.-Hoist hook assembly. Examine for defect,corrosion and binding. OPI - Every month, 25 liftsor 50 flight hours. Use limit that occurs first (Note 1)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 25 - INSPECTION

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-70-07-00A-000A-A Scheduled/unscheduled inspections. Rescue hoist installation


OPI - After last flight of the day (if hoist used)

OPI - After last flight of the day (if hoist is used)

g ( )

386.-

Hoist cable. Examine for defect. Make sure thatcable is correctly wound on drum. OPI - Everymonth, 25 lifts or 50 flight hours. Use limit thatoccurs first (Note 1)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 25 - INSPECTION

387.-Hoist tension roller. Examine for wear and defects.OPI - Every 6 months, 400 lifts or 100 flight hours.Use limit that occurs first (Note 1)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.


388.-

Hoist tension roller and overrunning clutchassemblies. Examine for correct operation andwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 400 6 MO INSPECTION

389.-Hoist cable guide. Examine for wear. OPI - Every 6 months, 400 lifts or 100 flight hours. Use limit thatoccurs first (Note 1)


390Hoist chain. Examine for correct tension. OPI -E 6 th 400 lift 100 fli ht h U 03 O t 07 0 0 0 0 0 NEW 354 6 100 0 400 6 MO S C O


NOT APPLICABLE EQUIPMENT NOT INSTALLED


390.- Every 6 months, 400 lifts or 100 flight hours. Uselimit that occurs first (Note 1)


391.-Hoist pressure rollers. Examine for corrosion andwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)


392.-Hoist level wind shaft and follower. Examine forwear. OPI - Every 6 months, 400 lifts or 100 flighthours. Use limit that occurs first (Note 1)





393.-Hoist. Examine for correct oil level. OPI - Every 6months, 400 lifts or 100 flight hours. Use limit thatoccurs first (Note 1)


394.- Hoist, hook and cable. Wash. OPI - Every month - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION

395.- Rescue hoist installation. Do an operation test.OPI - Every 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION





G.M.J.P. 19 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



396.- Cargo hook emergency release control. Dooperation test. SIP - Airworthiness check - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

397.- Cargo hook emergency release control. Dooperation test. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

398.- Cargo hook emergency release control. Do - - 03-Oct-07 0 0 0 0 0 NEW 354 6 - 50.0 - 30 DAYS INSPECTION


CHAPTER 0B-A-05-70-08-00A-000A-A Scheduled/unscheduled inspections - Cargo hook, safety cargo hook and rear view mirror CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )


NOT APPLICABLE, EQUIPMENT NOT INSTALLED.398.- operation test. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

399.- Safety cargo hook emergency release control. Dooperation test. SIP - Airworthiness check - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

400.- Safety cargo hook emergency release control. Dooperation test. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

401.- Safety cargo hook emergency release control. Dooperation test. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION





402.-Cargo hook components and electricalconnections. Examine for condition and security.SIP - Airworthiness check


403.-Cargo hook components and electricalconnections. Examine for condition and security.EIP - 50 hours / 30 days


404.-Cargo hook components and electricalconnections. Examine for condition and security.PIP - 50 hours / 30 days


Safety cargo hook components and electrical




405.-Safety cargo hook components and electricalconnections. Examine for condition and security.SIP - Airworthiness check


406.-Safety cargo hook components and electricalconnections. Examine for condition and security.EIP - 50 hours / 30 days


407.-Safety cargo hook components and electricalconnections. Examine for condition and security.PIP - 50 hours / 30 days





408.- Rear view mirror. Examine for condition andsecurity. SIP - Airworthiness check - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 100.0 - - INSPECTION

409.- Rear view mirror. Examine for condition andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

410.- Rear view mirror. Examine for condition andsecurity. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

411.- Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. SIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.




412.- Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. EIP - 12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

413.-Cargo hook support frame, supports and adjacent fuselageareas. Examine for corrosion and damage. PIP - 12 months -PH I

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

414.-Safety cargo hook crossbeam, supports and adjacentfuselage areas. Examine for corrosion and damage. SIP - 12months


415.-Safety cargo hook crossbeam, supports and adjacentfuselage areas. Examine for corrosion and damage. EIP - 12months

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION NOT APPLICABLE, EQUIPMENT NOT INSTALLED.





G.M.J.P. 20 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



416.-Safety cargo hook crossbeam, supports and adjacentfuselage areas. Examine for corrosion and damage. PIP - 12months - PH I


417.- Cargo hook load measuring system. Do operation test. SIP -12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

418.- Cargo hook load measuring system. Do operation test. EIP -12 months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

C h k l d i t D ti t t PIP




CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-70-08-00A-000A-A Scheduled/unscheduled inspections - Cargo hook, safety cargo hook and rear view mirror

419.- Cargo hook load measuring system. Do operation test. PIP -12 months - PH I - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

420.-Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). SIP - 12 months


421.-Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hook - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION




y p gand send it to the Manufacturer fro overhaul.). EIP - 12 months

422.-

Cargo hook. Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). PIP - 12months - PH I


423.-

Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargoh k d d it t th M f t f h l ) SIP 12



NOT APPLICABLE, EQUIPMENT NOT INSTALLED.hook and send it to the Manufacturer fro overhaul.). SIP - 12months

424.-

Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). EIP - 12months


425.-

Safety cargo hook. Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargo - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION


NOT APPLICABLE, EQUIPMENT NOT INSTALLED.425. 1. If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). PIP - 12months - PH I

03 Oct 07 0.0 0 0.0 NEW 354.6 1 YR INSPECTION

426.-

Cargo hook Examine external surfaces for corrosion. This isvery important in attach lug areas of side plates (Note 1.- Ifyou find corrosion on the side plates, remove the cargo hookand send it to the Manufacturer fro overhaul.). SI - Everymonth (if cargo hook is used or is stored in a marineatmosphere)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION

Safet cargo hook E amine e ternal s rfaces for corrosion



427.-

Safety cargo hook Examine external surfaces for corrosion.This is very important in attach lug areas of side plates (Note1.- If you find corrosion on the side plates, remove the cargohook and send it to the Manufacturer fro overhaul.). SI - Everymonth (if cargo hook is used or is stored in a marineatmosphere)

- - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 MO INSPECTION

428.-Cargo hook installation. Do operation test ofisolation relays for closed circuit failures. SI - 2000hours


429.-Safety cargo hook installation. Do operation test ofisolation relays for closed circuit failures. SI - 2000 - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 2000.0 - - INSPECTION



NOT APPLICABLE, EQUIPMENT NOT INSTALLED.429. isolation relays for closed circuit failures. SI 2000hours

03 Oct 07 0.0 0 0.0 NEW 354.6 2000.0 O C , QU O S


G.M.J.P. 21 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



430.- Upper cutter. Examine for condition and security.SIP - Airworthiness check - - 08-Dec-08 193.6 716 0.0 NEW 161.0 - 100.0 - - INSPECTION

431.- Upper cutter. Examine for condition and security.EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

432.- Upper cutter. Examine for condition and security.PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

N tt E i f diti d l k d i




CHAPTER 0B-A-05-70-09-00A-000A-A Scheduled/unscheduled inspections - Wire strike protection system CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )

433.-

Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] SIP -100 hours

- - 08-Dec-08 193.6 716 0.0 NEW 161.0 - 100.0 - - INSPECTION

434.-

Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] EIP -200 hours




435.-

Nose cutter Examine for condition and locked inforward tilted position [1 CAUTION: Damage mayresult from landing gear retraction if the nosecutter is not locked in forward tilted position.] PIP -200 hours - PH C


436.-Particle separator air intake. Examine forcondition, foreign matter, damage and looseattaching hardware SIP Airworthiness check




CHAPTER 0B-A-05-70-10-00A-000A-A Scheduled/unscheduled inspections - Engine inlet particle separator system

attaching hardware. SIP - Airworthiness check

437.-Particle separator air intake. Examine forcondition, foreign matter, damage and looseattaching hardware. EIP - 50 hours / 30 days


438.-Particle separator air intake. Examine forcondition, foreign matter, damage and looseattaching hardware. PIP - 50 hours / 30 days




439.-Particle separator system tubing, shut-off valve,supports and locking devices. Examine for securityof installation and condition. SIP - 400 hours


440.-Particle separator system tubing, shut-off valve,supports and locking devices. Examine for securityof installation and condition. EIP - 400 hours


441.-Particle separator system tubing, shut-off valve,supports and locking devices. Examine for security - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 400.0 - - INSPECTION




of installation and condition. PIP - 400 hours - PH 3


G.M.J.P. 22 de 39











SERIAL / SERIE No.







LIMITS / LIMITES






DATE / FECHA

CARGO HOOK HOURS



22052




ITEM


DE PARTE



O COMPONENTE



442.-Fittings, restraint cables and bungee cords.Examine for damage and security. SIP -Airworthiness check


443.-Fittings, restraint cables and bungee cords.Examine for damage and security. EIP - 50 hours /30 days


Fittings restraint cables and bungee cords

CHAPTER 05-00 Scheduled/unscheduled maintenance (E.A.S.A./F.A.A. Second issue : 2009-06-22 )CHAPTER 0B-A-05-70-11-00A-000A-A Scheduled/unscheduled inspections - Snow ski installation



444.-Fittings, restraint cables and bungee cords.Examine for damage and security. PIP - 50 hours /30 days


445.- Restraint cables. Examine for corrosion. OPI - 12months - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

446.-

Snow skis. Examine for deformation. Payparticular attention to any permanent deformationto the cable supports (sheet metal parts),especially to any sheet metal layer separation inthe cable attachment area. OPI - 12 months





447.-

Snow skis. Examine for deformation. Payparticular attention to any permanent deformationto the cable supports (sheet metal parts),especially to any sheet metal layer separation inthe cable attachment area. CI - Hard landing


448Pads, fittings, steel ropes and bungee cords.E i f diti d it SIP 08 D 08 193 6 716 0 0 NEW 161 0 100 0

CHAPTER 0B-A-05-70-12-00A-000A-A Scheduled/unscheduled inspections - Slump pad installation

CI - Hard landing

NOT APPLICABLE EQUIPMENT NOT INSTALLED448.- Examine for condition and security. SIP -Airworthiness check


449.-Pads, fittings, steel ropes and bungee cords.Examine for condition and security. EIP - 50 hours/ 30 days


450.-Pads, fittings, steel ropes and bungee cords.Examine for condition and security. PIP - 50 hours/ 30 days


451.- Bungee cords support. Examine for distortions andsecurity SIP Airworthiness check - - 08-Dec-08 193.6 716 0.0 NEW 161.0 - 100.0 - - INSPECTION




NOT APPLICABLE, EQUIPMENT NOT INSTALLED.security. SIP - Airworthiness check

452.- Bungee cords support. Examine for distortions andsecurity. EIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

453.- Bungee cords support. Examine for distortions andsecurity. PIP - 50 hours / 30 days - - 03-Oct-07 0.0 0 0.0 NEW 354.6 - 50.0 - 30 DAYS INSPECTION

1. Visual inspection.Note 1 Refer to Maintenance Planning

CH 0B-A-20-60-01-00A-289A-A Corrosion control – Inspection of corrosion damage



454.-

Note 1.- Refer to Maintenance PlanningInformation publication (0B-A-AMPI-00-P) fordetailed inspection and preventive maintenancerequirements. Note 2.- These inspections should beaccomplished in conjunction with other requiredpreventive maintenance.

- - 25-Nov-09 300.0 1056 0.0 0.0 54.6 - 100.0 - - INSPECTION 400.0 - - 45.4 - - NEW REQ

455.-2 Scheduled inspection. Note.- This inspection should be accomplishedeach 200 h or 90 days (whichever occurs first).

- - 17-Mar-10 341.5 1177 0.0 -8.5 13.1 - 200.0 - 3 MO INSPECTION 550.0 - 16-Jun-10 195.4 - 14.8 NEW REQ


G.M.J.P. 23 de 39











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456.- ENVIROMENTAL ASSY 5833C000-005 1367 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

457.- HEAT EXCHANGER E.C.S. 8585C000-001 2355 03-Oct-07 0.0 0 0.0 NEW 354.6 - 3000.0 - * OVERHAUL 3000.0 - - 2645.4 - -458.- TURBINE BLOWER E.C.S. 1538D000-002 1384 03-Oct-07 0.0 0 0.0 NEW 354.6 - 5000.0 - * OVERHAUL 5000.0 - - 4645.4 - -459.- SHUTT-OFF CHECK VALVE LH 109-0711-09-103 1182AB 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

460.- SHUTT-OFF CHECK VALVE LH 109-0711-09-103 0006AB 14-Jan-08 211.3 764 0.0 REP 143.3 - ON CONDITION - REPLACEMENT S/N 1186AB OFF

461 RATE GYRO 7007453 902 06121572 03 Oct 07 0 0 0 0 0 NEW 354 6 ON CONDITION REPLACEMENT

CHAPTER 22 AUTO FLIGHT "ON CONDITION"ON CONDITION

CHAPTER 21 AIR CONDITIONING "ON CONDITION"ON CONDITION

ON CONDITION

ON CONDITION COMPONENTS

ON CONDITION

461.- RATE GYRO 7007453-902 06121572 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

462.- AIR DATA SENSOR D60350MK211212 000774-005 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

463.- F/D CONTROL PANEL 7000605-901 06123354 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

464.- HRLIPILOT ACTUATOR ASSY 109-0020-86-1 0611H688 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT





469.- SAS/FD CONTROL PANEL 109-0729-49-1 938 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

470.- F/D COMPUTER (TYPE FZ-702) 109-0900-56-101 0346 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

471 HELIPILOT COMPUTER N 1 (TYPE SP711) 109 0900 64 103 0761 03 O t 07 0 0 0 0 0 NEW 354 6 ON CONDITION

ON CONDITIONON CONDITION


ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

471.- HELIPILOT COMPUTER N.1 (TYPE SP711) 109-0900-64-103 0761 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

472.- HELIPILOT COMPUTER N.2 (TYPE SP711) 109-0900-64-103 0914 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

473.- VHF ANTENNA N.1 VFS 10-90-2 6134 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

474.- VHF ANTENNA N.2 VFS 10-90-2 6212 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

475.- ICS AMPLIFIER 251-002 1394 14-Jan-08 211.3 764 0.0 REP 143.3 - ON CONDITION - REPLACEMENT S/N 1567 OFF

476.- GNS 530 RECEIVER 010-00182-10 78417645 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

477.- GNS 430 COMM/NAV GPS UNIT CPLT 010-00139-10 011-0028-10

97139635 97139629 13-Mar-09 UNK UNK 0.0 OVH #¡VALOR! - ON CONDITION - REPLACEMENT SAME PART

NSTALLEDON CONDITION

ON CONDITION

ON CONDITIONON CONDITIONON CONDITIONON CONDITION

ON CONDITION

CHAPTER 23 COMMUNICATIONS "ON CONDITION"

ON CONDITION

478.- ICS CONTROL PANEL CPLT AA95-954TSO 2045 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

479.- ICS CONTROL PANEL PLT AA95-954TSO 2046 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

480.- CABIN AUDIO PANEL AA82-060 2153 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

481.- ICS CONTROL PANEL AA31-002 2417 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

482.- MAIN BATTERY 2778-1 S00615 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

483.- DC CONTROL BOX N.1 GCSG505-28-1 2254D 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

484.- DC CONTROL BOX N.2 GCSG505-28-1 2257D 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

485.- INVERTER N.1 PC 251A 26140 25-Jun-08 136.7 532 0.0 NEW 217.9 - ON CONDITION - REPLACEMENT S/N 25018 OFF

486.- INVERTER N.2 PC 251A 25101 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

ON CONDITIONON CONDITIONON CONDITION

ON CONDITION

CHAPTER 24 ELECTRICAL POWER "ON CONDITION"ON CONDITIONON CONDITION


486. INVERTER N.2 PC 251A 25101 03 Oct 07 0.0 0 0.0 NEW 354.6 ON CONDITION487.- DC ELECTRICAL BOX 109-0729-99-101 N367 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

488.- DETECTRO BOX 109-0900-19-101 90 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

489.- EMERGENCY LOCATRO TRANSMITTER ARTEXMOD. C406-2HM, CODE: AB2C4000E4002A9 455-5049-345 A00057 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT EXP BATT 04/2012

490.- FIRE DETECTOR ENGINE N.1 3001-38-450/170C3-6M 89061 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

ON CONDITION

CHAPTER 25 EQUIPMENT/FURNISHINGS "ON CONDITION"

ON CONDITION

CHAPTER 26 FIRE PROTECTION "ON CONDITION"

ON CONDITION


491.- FIRE DETECTOR ENGINE N.2 3001-38-450/170C3-6M 89074 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

492.- ENGINES FIRE EXTINGUISHER (MAIN) M/D02/07; I/D 06/07 27300-1 1042 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

493.- ENGINES FIRE EXTINGUISHER (ALT) M/D02/07; I/D 06/07 27300-1 1046 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

494.- PANEL FIRE EXTINGUER 109-0740V10-103 S07329302 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

495.- MAGNETIC BRAKE YAW 109-0021-17-1 12391 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

496.- MAGNETIC BRAKE PITCH 109-0021-18-1 12347 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

CHAPTER 27 FLIGHT CONTROLS "ON CONDITION"ON CONDITIONON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION

497.- MAGNETIC BRAKE ROLL 109-0021-18-1 12348 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT ON CONDITION


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498.- EJECTOR LH SM2259 1165 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

499.- EJECTOR RH SM2259 1154 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

500.- FUEL VALVE LH SM2677 1811 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

501.- FUEL VALVE RH SM2677 1869 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

502.- VALVE CROSS FEED SM2677 1866 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

503.- PUMP ASSY LH 109-0611-53-103 12BB221 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

504.- PUMP ASSY RH 109-0611-53-103 12BB206 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT


CHAPTER 28 FUEL "ON CONDITION"ON CONDITION



505.- PANEL FUEL CONTROL 109-0900-43-101 S07322729 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

506.- TANK ASSY LH, M/D 02/07; I/D 06/07 109-0900-69-105 009 06-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 078 OFF

507.- TANK ASSY RH, M/D 02/07; I/D 06/07 109-0900-69-106 068 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

508.- MAIN TANK UP REAR 109-0900-69-103 108 29-Jun-09 249.1 898 0.0 REP 105.5 - ON CONDITION - REPLACEMENT S/N 126 OFF

509.- PROBE FUEL Q.TY LH 109-0900-81-211 318 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

510.- PROBE FUEL Q.TY RH 109-0900-81-211 319 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

511.- PROBE FUEL Q.TY LH 109-0900-81-213 346 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

512.- PROBE FUEL Q.TY RH 109-0900-81-213 345 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

513.- PROBE FUEL Q.TY 109-0900-81-205 291 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

514.- FUEL CONTROL UNIT 109-0900-81-215 267A 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

ON CONDITION

ON CONDITION



ON CONDITION


515.- TRANSMITTER PRESSURE IMP. N.1 109-0729-24-129 AGAH0103 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

516.- TRANSMITTER PRESSURE IMP. N.2 109-0729-24-129 AGAH0106 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

517.- VALVE AND FILTER ASSY. N.1 109-0760-41-107 1934 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

518.- VALVE AND FILTER ASSY. N.2 109-0760-41-107 MM1333 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

519.- HYDRAULIC PUMP N.1 109-0760-42-103 BH304 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

520.- HYDRAULIC PUMP N.2 109-0760-42-103 BH303 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

521.- SWITCH LOW LEVER 109-0760-45-1 0629 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

522.- ACCUMULATOR ASSY N.1 109-0760-52-1 1985 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

523.- ACCUMULATOR ASSY N.2 109-0760-52-1 1984 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT


ON CONDITIONON CONDITIONON CONDITIONON CONDITIONON CONDITIONON CONDITION

CHAPTER 29 HYDRAULIC POWER "ON CONDITION"ON CONDITION

524.- VALVE 109-0763-56-103 1792 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

525.- VALVE 109-0763-56-103 1942 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

526.- WINDSHIELD WIPER 109-0700-36-1 00621 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

527.- WINDSHIELD WIPER 109-0700-36-2 00627 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

528.- DIGITAL CLOCK AT42510H 01685 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

529.- AURAL WARNING GENERATOR 109-0729-96-105 568 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

530 NOSE LANDING GEAR ACTUATOR 109 0500 10 109 0002 20 Nov 09 300 0 1056 0 0 REP 54 6 ON CONDITION REPLACEMENT S/N 0328 OFF

ON CONDITIONCHAPTER 32 LANDING GEAR "ON CONDITION"

ON CONDITION

ON CONDITION

CHAPTER 30 ICE AND RAI PROTECTION "ON CONDITION"ON CONDITIONON CONDITION

CHAPTER 31 INDICATING/RECORDING SYSTEMS "ON CONDITION"


530.- NOSE LANDING GEAR ACTUATOR 109-0500-10-109 0002 20-Nov-09 300.0 1056 0.0 REP. 54.6 - ON CONDITION - REPLACEMENT S/N 0328 OFF

531.- MAIN LANDING GEAR BRAKE RH 109-0500-14-101 5315 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

532.- MAIN LANDING GEAR BRAKE LH 109-0500-14-102 1939 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

533.- NOSE LANDING GEAR WHEEL 109-0500-15-1 3378 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

534.- MAIN LANDING GEAR WHEEL RH 109-0500-16-3 2543 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

535.- MIAN LANDING GEAR WHEEL LH 109-0500-16-3 2504 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

536.- WHEEL BRAKE CONTROL VALVE ASSY 109-0506-57-105 5141 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

537.- BRAKE SELECTOR VALVE 109-0506-63-103 468 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

538.- LANDING GEAR SELECTOR VALVE 109-0512-43-111 3287 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

539.- SHUTTLE VALVE N°1 109-0512-45-1 6296 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

540 SHUTTLE VALVE N°2 109 0512 45 1 6256 03 Oct 07 0 0 0 0 0 NEW 354 6 ON CONDITION REPLACEMENT ON CONDITION





540.- SHUTTLE VALVE N°2 109-0512-45-1 6256 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

541.- HYDRAULIC LOCK NOSE LANDING GEAR 109-0512-46-105 0768 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

542.- HYDRAULIC LOCK MAIN LANDING GEAR LH 109-0512-46-105 0766 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

543.- HYDRAULIC LOCK MAIN LANDING GEAR LH 109-0512-46-105 0244 03-Sep-09 29.1 968 0.0 SVC 325.5 - ON CONDITION - REPLACEMENT S/N 0750 OFF

544.- PRESSURE SWITCH 109-0512-67-105 3881 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

545.- PRESSURE SWITCH (EMERG.) 109-0512-67-105 3351 15-May-08 118.1 UNK UNK TST - - ON CONDITION - REPLACEMENT S/N 3934 OFF

546.- LOW PRESSURE SWITCH 109-0512-107 2624 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

547.- ACCUMULATOR ASSY C/D 01/07 109-0512-70-109 00636 07-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 1039 OFF

548.- TRANSMITTER OIL PRESSURE 109-0729-24-129 AGAH149 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

549.- TRANSMITTER OIL PRESSURE 109-0729-24-129 AGAH146 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

550 MAIN LANDING GEAR ACTUATOR LH 109 0900 39 107 0625 03 Oct 07 0 0 0 0 0 NEW 354 6 ON CONDITION REPLACEMENT ON CONDITION


ON CONDITION

ON CONDITION



550.- MAIN LANDING GEAR ACTUATOR LH 109-0900-39-107 0625 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

551.- MAIN LANDING GEAR ACTUATOR RH 109-0900-39-107 0627 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT



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O COMPONENTE



552.- ANTICOLLISION LIGHT, LOWER 01-0770905-01 01252 05-Nov-08 190.7 703 0.0 NEW 163.9 - ON CONDITION - REPLACEMENT S/N 00826 OFF

553.- ANTICOLLISION LIGHT, UPPER 01-0770905-01 00546A 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

554.- SEARCHLIGHT 930-500-25-1 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

555.- VOR COUPLE DRC 20-04 6389 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

556.- VOR/LOC ANTENNA RIGHT DMN 48-5 01004 08-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 548 OFF

557 - VOR/LOC ANTENNA LEFT DMN 48-5 01006 08-Mar-08 99 5 446 0 0 NEW 255 1 - ON CONDITION - REPLACEMENT S/N 565 OFFON CONDITION

CHAPTER 33 LIGHTS "ON CONDITION"ON CONDITIONON CONDITIONON CONDITION

CHAPTER 34 NAVIGATION "ON CONDITION"ON CONDITIONON CONDITION


557.- VOR/LOC ANTENNA LEFT DMN 48-5 01006 08-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 565 OFF

558.- ANTENNA MARKER BEACON (TYPE DMN43-1) 261D913 19078 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

559.- M.B. CONTROL PANEL 109-0729-93-101 S07318164 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

560.- ADF CONVERTER (DIV-202A) 520-2020-001 24749 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

561.- TRANSPONDER ANTENNA DMNI-24 92704 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

562.- TRANSPONDER TRANSM/REC. (KT 73) 066-01164-0101 3383 08-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 3219 OFF

563.- ADF ANTENNA (KA-44B) 071-01234-0000 84209 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

564.- ADF RECEIVER (KX 87) 066-01072-0004 81315 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

565.- DME INDICATOR (KDI-574) 066-01069-0004 84798 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

566 - DME RECEIVER (KMD-706A) 066-01066-0025 16381 03-Oct-07 0 0 0 0 0 NEW 354 6 - ON CONDITION - REPLACEMENT



ON CONDITION

ON CONDITION


566.- DME RECEIVER (KMD-706A) 066-01066-0025 16381 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

567.- DME ANTENNA DMNI-24 92703 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

568.- M.B. RECEIVER (KMR-675) 066-01044-0000 5842 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

569.- VOR CONVERTER (KN-40) 066-01130-0801 11724 03-Oct-08 163.0 621 0.0 NEW 191.6 - ON CONDITION REPLACEMENT S/N 12754 OFF

570.- GPS ANTENNA 011-00147-00 60008525 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

571.- GPS ANTENNA 011-00147-00 60008206 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

572.- PITOT TUBE ASSY RH 109-0720-61-108 22826 08-Dec-08 193.6 716 0.0 INSPECTED 161.0 - ON CONDITION - REPLACEMENT S/N 22908 OFF

573.- PITOT TUBE ASSY LH 109-0720-61-107 22889 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

574.- AIRSPEED INDICATOR PILOT 109-0729-09-109 0436 29-Jun-09 249.1 898 0.0 INSPECTED 105.5 - ON CONDITION - REPLACEMENT S/N 0387 OFF

575.- VERTICAL SPEED INDICATOR COPILOT 4A58.22.40F.05.05.2EB 1042356 07-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 1044626 OFF


ON CONDITION



576.- COPILOT ALTIMETER INDICATOR 3A43-22-20F-05-1FU 1044754 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

577.- ENCODER ALTIMETER INDICATOR 3A67-32-20F-05-1KR 1044549 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

578.- VERTICAL SPEED INDICATOR PILOT 31230-1127 363026 29-Jun-09 249.1 898 0.0 OVH 105.5 - ON CONDITION - REPLACEMENT S/N 357650 OFF

579.- AIRSPEED INDICATOR COPILOT 64050-228-1 6386 29-Jun-09 249.1 898 0.0 INSPECTED 105.5 - ON CONDITION - REPLACEMENT S/N 8119 OFF

580.- DIRECTIONAL GYRO (TYPE C-14A) 2587193-43 06122777 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

581.- FLUX VALVE 2594484 0702H721 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

582.- FLUX VALVE COMPENSATOR 656767 0391 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT ON CONDITION


ON CONDITION

ON CONDITION

583.- TRAN. RECEI. RADAR ALT. (TYPE RT-300) 7001840-934 07030572 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

584.- RADIO ALTIMETER ANTENNA FWD. S67-2002-4 552-14212 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

585.- RADIO ALTIMETER ANTENNA AFT. S67-2002-4 552-14237 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

586.- GLIDE SLOPE ANTENNA RGS-10-48 11891 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

587.- GLIDE SLOPE COUPLER DGSC-20-02 4592 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

588.- GYRO COMPASS PANEL 109-0900-38-101 S07289392 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

589.- MISCELANEOUS PANEL 109-0900-46-109 S07303712 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

590.- MAGNETIC COMPASS PILOT C 2300L4-24B AG-2403 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

591.- MAGNETIC COMPASS N° 2 PILOT C 2300L4-24B AG-2407 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

592.- ATTITUDE IND STAND BY 501-1197-28 7089 07-Mar-08 99 5 446 0 0 NEW 255 1 - ON CONDITION - REPLACEMENT S/N 9423 OFF



ON CONDITION


592.- ATTITUDE IND. STAND BY 501-1197-28 7089 07-Mar-08 99.5 446 0.0 NEW 255.1 - ON CONDITION - REPLACEMENT S/N 9423 OFF

593.- EFIS PILOT EADI, F.T. ACCEPT. 06/07 109-0900-71-1A01 710 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

594.- EFIS COPILOT EADI, F.T. ACCEPT. 06/07 109-0900-71-1A01 711 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

595.- EFIS PILOT EHSI, F.T. 109-0900-71-1A01 708 22-Jan-10 313.4 1104 0.0 REPAIRED 41.2 - ON CONDITION - REPLACEMENT S/N 271 OFF

596.- EFIS COPILOT EHSI, F.T. ACCEPT. 06/07 109-0900-71-1A01 703 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT INTERCAMBIO WO#10277.1.2

597.- BASE UNIT KMD 540 066-04035-1101 8701 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

598.- PILOT ALTIMETTR INDICATOR 3A43-22-20F-05-1FU 1044838 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

599.- VERTICAL GYRO N° 1 46060-11 07-0211 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

600.- VERTICAL GYRO N° 2 501-1210-01 3156 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

601.- RECETRASM. RTC-497 (TAS) 805-10800-001 84689 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

ON CONDITION

ON CONDITION



ON CONDITION


601. RECETRASM. RTC 497 (TAS) 805 10800 001 84689 03 Oct 07 0.0 0 0.0 NEW 354.6 ON CONDITION REPLACEMENT

602.- ANTENNA NY-164 (TAS) 805-10890-001 85417 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT ON CONDITIONON CONDITION


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603.- COMPUTER IDS-DAU 109-0900-76-6A01 06010127 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

604.- IDS INDICATOR PLT 109-0900-76-2A01 05020104 29-Jun-09 249.1 898 0.0 MOD 105.5 - ON CONDITION - REPLACEMENT S/N 07050256 OFF

605.- IDS INDICATOR CPLT 109-0900-76-2A01 07050264 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

606.- FUSELAGE ASSY 109-0300-18-107 A7/052 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

607.- TAIL BOOM 109-0370-17-301 A7/048 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

608 - SUPPORT ASSY SYNCH ELEVATOR LH 109-0371-28-1 884 03-Oct-07 0 0 0 0 0 NEW 354 6 - ON CONDITION - REPLACEMENT


CHAPTER 40 INTEGRATION SYSTEMS "ON CONDITION"ON CONDITION COMPONENTS

ON CONDITION

CHAPTER 53 FUSELAGE "ON CONDITION"ON CONDITIONON CONDITIONON CONDITION608.- SUPPORT ASSY SYNCH. ELEVATOR LH 109-0371-28-1 884 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

609.- SUPPORT ASSY SYNCH. ELEVATOR RH 109-0371-28-1 883 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

610.- SPLIT CONE 109-0101-21-1 N385 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

611.- RING NUT MAST 109-0101-79-1 M494 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

612.- RING CONIC 109-0101-80-103 M268 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

613.- SLEEVE 109-0110-21-103 MCR00249 03-Oct-07 0.0 0 0.0 NEW 354.6 - 15000.0 - * REPLACEMENT 15000.0 - - 14645.4 - -614.- SLEEVE 109-0110-21-103 MCR00254 03-Oct-07 0.0 0 0.0 NEW 354.6 - 15000.0 - * REPLACEMENT 15000.0 - - 14645.4 - -615.- MAIN ROTOR HUB ASSY 109-0112-02-103 P114 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

616.- DAMPER 109-0112-39-103 0526 28-Jan-10 318.3 1116 0.0 REPAIRED 36.3 - ON CONDITION * REPLACEMENT S/N 0608 OFF



ON CONDITION

ON CONDITION

ON CONDITION

CHAPTER 65 ROTORS "ON CONDITION"

617.- DAMPER 109-0112-39-103 0707 17-Mar-10 328.4 1150 0.0 REPAIRED 26.2 - ON CONDITION * REPLACEMENT S/N 0609 OFF

618.- DAMPER 109-0112-39-103 0228 25-May-09 249.1 898 329.1 NEW 434.6 - ON CONDITION * REPLACEMENT S/N 0244 OFF

619.- DAMPER 109-0112-39-103 0957 17-Mar-10 328.4 1150 0.0 INSPECTED 26.2 - ON CONDITION * REPLACEMENT S/N 0488 OFF

620.- SWASHPLATE ASSY 109-0134-02-103 M147 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

621.- PITCH CHANGE LINK 109-0134-05-111 P745 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT



624.- PITCH CHANGE LINK 109-0134-05-111 P748 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

625.- DRIVE SHAFT ENGINE-TRANS. LH. 109-415-06-103 1039 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

626.- DRIVE SHAFT ENGINE-TRANS. RH. 109-415-06-103 1038 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT


ON CONDITION


ON CONDITION

ON CONDITION


626.- DRIVE SHAFT ENGINE TRANS. RH. 109 415 06 103 1038 03 Oct 07 0.0 0 0.0 NEW 354.6 ON CONDITION - REPLACEMENT

627.- T.R. DRIVE SHAFT N.2 SEZ 109-0420-05-109 P226 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

628.- T.R. DRIVE SHAFT N.3 SEZ 109-0420-05-111 P200589 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

629.- ROTOR BRAKE ASSY 109-0506-56-105 5063 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

630.- LOW PRESS. SWITCH 109-0600-36-109 3667 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

631.- TRANSMITTER OIL PRESSURE 109-0729-24-121 0714 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

632.- TAIL ROTOR HUB AND BLADE ASSY 109-0162-01-101 P200547 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

633.- TAIL ROTOR HUB ASSY 109-0162-01-103 P48 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION * REPLACEMENT

634.- BEARING DUPLEX 109-0133-05-101 09465 20-Nov-09 300.0 1056 0.0 INSPECTED 54.6 - ON CONDITION - REPLACEMENT S/N 07140 OFF

635.- TAIL ROTOR BEARING SLEEVE 109-0130-94-109 MO.334 20-Nov-09 300.0 1056 0.0 NEW 54.6 - ON CONDITION - REPLACEMENT S/N 07140 OFF

636 TACHOMETER GENERATOR EA6300V077 003 0701748 03 Oct 07 0 0 0 0 0 NEW 354 6 ON CONDITION REPLACEMENT


ON CONDITION

ON CONDITION

ON CONDITION

ON CONDITION



ON CONDITION

636.- TACHOMETER GENERATOR EA6300V077-003 0701748 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

637.- TRANSDUCER GM9271-X 2046 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT

638.- TRANSDUCER GM9271-X 2017 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

639.- ENGINE CONTROL LEVER 109-0630-61-109 07051 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

640.- ENGINE CONTROL PANEL 109-0900-55-101 364 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

641.- BLOWER OIL COOLER, LH 109-0455-01-101 01261 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

642.- BLOWER OIL COOLER, RH 109-0455-01-101 01260 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

643.- COOLER ASSY 109-0621-17-103 169 03-Oct-07 0 0 0 0 0 NEW 354 6 - ON CONDITION - REPLACEMENT


CHAPTER 76 ENGINE CONTROLS "ON CONDITION"

ON CONDITION

ON CONDITION

ON CONDITION

CHAPTER 79 OIL "ON CONDITION"ON CONDITIONON CONDITIONON CONDITION643.- COOLER ASSY 109-0621-17-103 169 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

644.- COOLER ASSY 109-0621-17-104 163 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

645.- TRANSDUCER PRESSURE ENGINE N.1 109-0729-24-117 2179 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

646.- TRANSDUCER PRESSURE ENGINE N.2 109-0729-24-117 2199 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

647.- KIT RADAR METEO (TYPE RDR-200) NOT APPLICABLE NOT APPLICABLE 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

648.- TRANSMITTER RADAR 071-01519-0101 10683 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

649.- ANTENNA RADAR 071-01549-0100 5225 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT

650.- RADAR PANEL 071-01438-0302 1512 18-Jun-08 130.8 520 0.0 INSPECTED 223.8 - ON CONDITION - REPLACEMENT S/N 2940 OFF

651.- KIT CHIP BURNER NOT APPLICABLE NOT APPLICABLE 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION - REPLACEMENT ON CONDITION

CHAPTER 95 OPTIONAL EQUIPMENT "ON CONDITION"ON CONDITIONON CONDITION

ON CONDITION

ON CONDITION



652.- POWER MODULE E 1070-2 1763 03-Oct-07 0.0 0 0.0 NEW 354.6 - ON CONDITION REPLACEMENT ON CONDITION


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. LH ENGINE PW207C S/N PCE-BH0141 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009.653.- LH ENGINE OVERHAUL; PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

654.- LH ENGINE OVERHAUL; reduction gearboxmodule RGB 3053005 RGB-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

655.- LH ENGINE OVERHAUL; turbomachinery moduleTM 3053006 TM-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

ENGINE INSPECTIONS LH

656.-

LH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTION 1750.0 - - 1395.4 - -

657.-

LH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The method

d t t d it th i i t th di ti f th O t

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTIONON CONDITION, from the results of the power assurance check or the engine health trend

monitoring.

used to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).

658.- LH ENGINE; POWER ASSURANCE CHECKS,Less than 175 hours CH. 71-00-00 PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - HOT SECTION INSPECTION 400.0 - - 45.4 - - EFECTUAR POR LA

TRIPULACIÓN

LH ENGINE; AIRWORTHINESS LIMITATIONS. 2.Automatic Low Cycle Fatigue (LCF) Counting. (4)

659.-

y g ( ) g ( )Every 40 to 50 hours, the operators must enter theaccumulated cycles for each LCF component inthe engine logbook. This data is obtained eitherfrom the helicopter display system or directly fromthe DCU using the Ground Base Software (GBS)program.

PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - 50.0 - - INSPECTION 350.0 - - -4.6 - - NEW REQ.


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. LH ENGINE PW207C S/N PCE-BH0141 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009.660.- BASIC ENGINE ACCESSORIES "P&W PARTS

CATALOGUE" PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - CHECK 3500.0 - - 3145.4 - -

661.- TORQUE PROBE AND SENSOR 3038223 CH2385 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -662.- SPEED SENSOR AND PROBES 3038224 CH2374 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -663.- SPEED SENSOR AND PROBES 3038225 CH2475 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -664.- ROTOR ACS. GENERATOR 3038627 2450 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -665.- STATOR-AC, GENERATOR 3038628 2097PA 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -


666.- GEARSHAFT-HLCL, 2STG, RDCN GRBX,74T 3043681-01 RWA6A892 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

667.- EXITER-IGNITION 3043937-03 CL071388 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

668.- FLOW DIVIDER ASSY 3044134-03 15143035 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

669.- HOUSING-REDUCTION G/BOX, FRONT 3044636-01 RWA84A749 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

670.- FUEL FILTER IMPEDING 3044899-03 HE1955 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -671.- THERMOCOUPLE IMMERSION, T6 3045344-02 EM101026 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -672.- CONTROL-ENGINE ELECTRONIC 3054275-04 07040007 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -673.- DATA COLLECTION UNIT 3054276-02 DP06-4048 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -674 Fuel Management Module (FMM) 3054277 01 15186810 30 Jul 07 0 0 0 0 0 NEW 354 6 3500 0 OVERHAUL 3500 0 3145 4674.- Fuel Management Module (FMM) 3054277-01 15186810 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

675.- WIRING HARNESS-ELECTRICAL ASSY 3054278-02 AA80300 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

676.- PUMP ASSY-OIL 3054344-01 RWA88A966 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

677.- GEARBOX ASSY-REDUCTION 3071639-01 RWA88A965 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -678.- TERM/WIRING HARNESS ASSY 3113579-04 EM100266 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

679.- CABLE ASSY-IGN. EXCITER TO IGNITER 3121144-02 CL070581 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -



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. LH ENGINE PW207C S/N PCE-BH0141 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATESep 25/2009. TABLE 1, Scheduled Maintenance Checks

681.-

LH (PW206C) Hot Section.- Compressor TurbineBlades (Pre-SB28069); Do a borescope inspectionof the compressor turbine blades for evidence ofblade shifting (Ref. 72-00-00, Engine, General -Inspection)

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 300.0 - - INSPECTION

LH (PW206C) Hot Section Power Turbine

NOT APPLICABLE BY ENGINE MODEL.


682.-

LH (PW206C) Hot Section.- Power TurbineBlades (Pre-SB28187 or Pre-SB28239); Do aborescope inspection of the power turbine bladesfor evidence of blade shifting (Ref. 72-00-00,Engine, General - Inspection)

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 300.0 - - INSPECTION

683.-

LH Engine Externals.- Wires of the ElectricalWiring Harness; Do a general visual check on thewires for evidence of chafing, cracks, corrosionand wear.

PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - - - 1 YR VISUAL CHECK - - 25-Nov-10 - - 176.7

LH E i E t l C t f th El t i l


684.-

LH Engine Externals.- Connectors of the ElectricalWiring Harness; Do a security check to verifyconnector security. Apply enhancer, electricalcontact (PWC05-256) to the speed/torqueconnectors P7, P9, P10 and sensors.0, (Ref. 73-21-40, ELECTRICALWIRING HARNESS - MAINTENANCEPRACTICES).

PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - - - 1 YR CHECK - - 25-Nov-10 - - 176.7

LH Engine Externals.- T6/T1 Wiring Harnesses;

685.-

g g ;Do a general visual check on the wires forevidence of chafing, cracks, corrosion and wear.Also verify if the nuts of the terminal junction aresecured. Do a heat response check on eachindividual probe. (Ref. 77-21-00, MGT SENSORSAND TRIM UNITS - INSPECTION/CHECK)


686.-LH Engine Externals.- Tubes; Do a general visualcheck on the tubes for security, fuel and/or oilleaks.


687.-

LH Engine Externals.- Air Inlet Screen; Do a visualcheck of the screen for blockage, damage and thatthe attaching hardware is serviceable (72-21-00,AIR INLET - INSPECTION/CHECK).

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - VISUAL CHECK 800.0 - - 445.4 - -

688.-

LH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):

PW207CNew heat shield:

Every 25 hours for the first 50 hours

30-Jul-07 0.0 0 0.0 NEW 354.6 - 25.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.

689.-


PW207CNew heat shield: in

service for more than 50 hours with no

cracks

30-Jul-07 50.0 0 0.0 NEW 304.6 - 100.0 - - VISUAL CHECK

690.-


PW207C Heat shield: with acceptable cracks 30-Jul-07 0.0 0 0.0 NEW 354.6 - 10.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.



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. LH ENGINE PW207C S/N PCE-BH0141 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATESep 25/2009. TABLE 1, Scheduled Maintenance Checks

691.-LH Oil .- Oil Filter; Remove and replace the oilfilter (Ref. 79-21-00, OIL SYSTEM(DISTRIBUTION) - MAINTENANCE PRACTICES).

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - REPLACEMENT 800.0 - - 445.4 - -

692.-LH Oil .- Chip Detector; Do an operational check ofthe chip detector (Ref. 79-31-00, OIL SYSTEM(INDICATING) MAINTENANCE PRACTICES)

PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - - - 1 YR OPERATIONAL CHECK - - 25-Nov-10 - - 176.7


(INDICATING) - MAINTENANCE PRACTICES).

693.-

LH (PW206C) Oil .- Oil Filler Cap (Pre-SB28222);Do an oil filler cap handle tension inspection (Ref.79-11-00, OIL SYSTEM (STORAGE) -MAINTENANCE PRACTICES).

PW207C PCE-BH0141 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

694.-LH Fuel.- Fuel Filter; Remove and replace thefuel filter (Ref. 73-21-50, FUEL PUMP FILTER -MAINTENANCE PRACTICES).



695.-

LH Fuel.- Fuel Nozzles; Clean and do a functionalcheck of the fuel nozzles (Ref. CMM 3040870).Inspect the fuel nozzle inlet screens. Ifcontamination is found, follow the Fuel ImpendingBy-Pass Indicator Activated fault isolation chart (Ref. 72-00-00).

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - FUNCTIONAL CHECK 800.0 - - 445.4 - -

696.-

LH (PW206C) Fuel.- Fuel Accumulator (Pre-SB28164); A general visual check for a bellowsfailure indication (through the pop-out indicator). If PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.an indication is present, replace the fuelaccumulator.

697.-LH Ignition.- Igniter Plug; Do a detailed visualcheck of the igniter plug for erosion (Ref. 74-11-00, ENGINE IGNITION - INSPECTION/CHECKS).


698.-LH Ignition.- Igniter Plug; Do a functional check toverify operating capabilities (Ref. 74-11-00,ENGINE IGNITION - INSPECTION/CHECKS).


699.-LH Ignition.- Ignition Cables; Do a general visualcheck on the wires for evidence of chafing, cracks,corrosion and wear.


700.-LH Power Management.- Electronic EngineControl (EEC); Do an EEC diode failure check(Ref. 73-21-20, EEC - INSPECTION/CHECKS).

PW207C PCE-BH0141 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - 1 YR CHECK

LH Power Management.- EEC/Fuel ManagementModule; Do a manual mode response check and

DELETED FROM MAINTENANCE MANUAL

701.- Module; Do a manual mode response check anddo an operational check of the alternate engineshutdown system. (Ref. applicable aircraft manual).

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - CHECK 800.0 - - 445.4 - -

702.-

LH FMM P3 Feed.- Inspect the P3 nipple on theoutput shaft cover for presence of debris (Ref. 73-21-10, FUEL MANAGEMENT MODULEINSPECTION CHECK).

PW207C PCE-BH0141 08-Dec-08 193.6 494 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - -


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. LH ENGINE PW207C S/N PCE-BH0141 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009. TABLE 2, Perform compressor washes as scheduled.

703.-LH ENGINE.- Compressor wash "Desalination";Continually salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - 1 DAY WASH

704.-LH ENGINE.- Compressor wash "Desalination";Frequently salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - WEECKLY WASH

Daily (increasewashing frequency to suit engine condition)

Weekly (increase washingfrequency to suit engine condition)


705.-LH ENGINE.- Compressor wash "Desalination";Occasionally salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - BIWEECKLY WASH


PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - 50.0 - - WASH 350.0 - - -4.6 - -


PW207C PCE-BH0141 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - WASH 400.0 - - 45.4 - -

Biweekly (increase washingfrequency to suit engine condition)

708.- LH ENGINE.- Performance recovery; Performancerecovery wash (Ref. 71-00-00) PW207C PCE-BH0141 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - - WASH

. PRATT & WHITNEY PE207C ENGINE 1 S/N PCE-BH0141 ; AIRWORTHINESS LIMITATIONS ISSUED DATE May 08/2009

. TABLE 2, PW207C Engines, Part Numbers for Automatic Life Cycle Counting709.- Data Collection Unit 3054276-01 - 30-Jul-07 0.0 0 0 NEW 548 - - - - REPLACEMENT

710.- Data Collection Unit (Post-SB28273) 3054276-02 - 30-Jul-07 0.0 0 0 NEW 548 - - - - REPLACEMENT

711.- LH Impeller 3058672-01 A0025A85 30-Jul-07 0.0 0 0 NEW 548 - - 15000 - REPLACEMENT - 15000 - - 14452 -

712 LH Compressor Turbine Disk 3048999 01 A00264H7 30 Jul 07 0 0 0 0 NEW 548 10000 REPLACEMENT 10000 9452

ON CONDITION

As required to suit engine operating conditions as indicated by engine condition trend monitoring system.

ON CONDITION

712.- LH Compressor Turbine Disk 3048999-01 A00264H7 30-Jul-07 0.0 0 0 NEW 548 - - 10000 - REPLACEMENT - 10000 - - 9452 -713.- LH Power Turbine Disk 3044188-01 A0026LHP 30-Jul-07 0.0 0 0 NEW 548 - - 15000 - REPLACEMENT - 15000 - - 14452 -

. TABLE 4, PW207C Engine Turbine/Turboshaft Rotor Components - Service Life714.- LH Impeller 3058672-01 A0025A85 30-Jul-07 0.0 0 0 0 0 - - 15000 - REPLACEMENT - 15000 - - 15000 -715.- LH Compressor Turbine Disk 3048999-01 A00264H7 30-Jul-07 0.0 0 0 0 0 - - 10000 - REPLACEMENT - 10000 - - 10000 -716.- LH Power Turbine Disk (Post-SB28187) 3044188-01 A0026LHP 30-Jul-07 0.0 0 0 0 0 - - 15000 - REPLACEMENT - 15000 - - 15000 -


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. RH ENGINE PW207C S/N PCE-BH0128 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009.717.- RH ENGINE OVERHAUL PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

718.- RH ENGINE OVERHAUL; reduction gearboxmodule RGB 3053005 RGB-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

719.- RH ENGINE OVERHAUL; turbomachinery moduleTM 3053006 TM-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

ENGINE INSPECTIONS RH

720.-

RH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTION 1750.0 - - 1395.4 - -

721.-

RH ENGINE HOT SECTION INSPECTION. Half theturbomachinery module TBO interval orOn condition, based on theresults of the engine trend monitoring (Ref. 71-00-00, POWERPLANT -FAULT ISOLATION). The HSI may also be "on condition" if theperformance health of the engine is monitored. To get a satisfactoryHSI "on condition" maintenance requirement, Operator's must keeprecords of the power assurance checks, either electronically or onpaper, and trend the data to monitor the engines health. The method

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 1750.0 - - HOT SECTION INSPECTIONON CONDITION, from the results of the power assurance check or the engine health trend

monitoring.paper, and trend the data to monitor the engines health. The methodused to trend monitor the engine is at the discretion of the Operator.However, P&WC recommends the use of the HECTM® (HelicopterEngine Condition Trend Monitoring) program (Ref. SIL PW200-003).

722.- RH ENGINE; POWER ASSURANCE CHECKS, Less than 175 hours CH. 71-00-00 PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - HOT SECTION INSPECTION 400.0 - - 45.4 - - EFECTUAR POR LA

TRIPULACIÓN

RH ENGINE; AIRWORTHINESS LIMITATIONS. 2.Automatic Low Cycle Fatigue (LCF) Counting (4)

723.-

Automatic Low Cycle Fatigue (LCF) Counting. (4)Every 40 to 50 hours, the operators must enter theaccumulated cycles for each LCF component inthe engine logbook. This data is obtained eitherfrom the helicopter display system or directly fromthe DCU using the Ground Base Software (GBS)program.

PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - 50.0 - - INSPECTION 350.0 - - -4.6 - - NEW REQ.


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. RH ENGINE PW207C S/N PCE-BH0128 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009.724.- BASIC ENGINE ACCESSORIES "P&W PARTS

CATALOGUE" PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - CHECK 3500.0 - - 3145.4 - -

725.- TORQUE PROBE AND SENSOR 3038223 CH2333 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -726.- SPEED SENSOR AND PROBES 3038224 CH2369 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -727.- SPEED SENSOR AND PROBES 3038225 CH2430 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -728.- ROTOR ACS. GENERATOR 3038627 2390 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -729.- STATOR-AC, GENERATOR 3038628 2029PA 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -


730.- GEARSHAFT-HLCL, 2STG, RDCN GRBX,74T 3043681-01 RWA64A884 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

731.- EXITER-IGNITION 3043937-03 CL070100 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

732.- FLOW DIVIDER ASSY 3044134-03 15093522 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

733.- HOUSING-REDUCTION G/BOX, FRONT 3044636-01 RWA69A025 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

734.- FUEL FILTER IMPEDING 3044899-03 HE1905 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -735.- THERMOCOUPLE IMMERSION, T6 3045344-02 EM98819 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -736.- CONTROL-ENGINE ELECTRONIC 3054275-04 06020041 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -737.- DATA COLLECTION UNIT 3054276-02 DP06-4488 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -738 Fuel Management Module (FMM) 3054277 01 15066127 30 Jul 07 0 0 0 0 0 NEW 354 6 3500 0 OVERHAUL 3500 0 3145 4738.- Fuel Management Module (FMM) 3054277-01 15066127 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

739.- WIRING HARNESS-ELECTRICAL ASSY 3054278-02 AA78791 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

740.- PUMP ASSY-OIL 3054344-01 RWA81A648 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -

741.- GEARBOX ASSY-REDUCTION 3071639-01 RWA81A647 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -742.- TERM/WIRING HARNESS ASSY 3113579-04 EM97636 30-Jul-07 0.0 0 0.0 NEW 354.6 - 3500.0 - - OVERHAUL 3500.0 - - 3145.4 - -




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. RH ENGINE PW207C S/N PCE-BH0128 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009. TABLE 1, Scheduled Maintenance Checks

745.-

RH (PW206C) Hot Section.- Compressor TurbineBlades (Pre-SB28069); Do a borescope inspectionof the compressor turbine blades for evidence ofblade shifting (Ref. 72-00-00, Engine, General -Inspection)

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 300.0 - - INSPECTION

RH (PW206C) Hot Section Power Turbine



746.-

RH (PW206C) Hot Section.- Power TurbineBlades (Pre-SB28187 or Pre-SB28239); Do aborescope inspection of the power turbine bladesfor evidence of blade shifting (Ref. 72-00-00,Engine, General - Inspection)

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - 300.0 - - INSPECTION

747.-

RH Engine Externals.- Wires of the ElectricalWiring Harness; Do a general visual check on thewires for evidence of chafing, cracks, corrosionand wear.


LH Engine Externals Connectors of the Electrical


748.-

LH Engine Externals.- Connectors of the ElectricalWiring Harness; Do a security check to verifyconnector security. Apply enhancer, electricalcontact (PWC05-256) to the speed/torqueconnectors P7, P9, P10 and sensors.0, (Ref. 73-21-40, ELECTRICALWIRING HARNESS - MAINTENANCEPRACTICES).

PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - - - 1 YR CHECK - - 25-Nov-10 - - 176.7

RH Engine Externals.- T6/T1 Wiring Harnesses;

749.-

g g ;Do a general visual check on the wires forevidence of chafing, cracks, corrosion and wear.Also verify if the nuts of the terminal junction aresecured. Do a heat response check on eachindividual probe. (Ref. 77-21-00, MGT SENSORSAND TRIM UNITS - INSPECTION/CHECK)


750.-RH Engine Externals.- Tubes; Do a general visualcheck on the tubes for security, fuel and/or oilleaks.


751.-

RH Engine Externals.- Air Inlet Screen; Do a visualcheck of the screen for blockage, damage and thatthe attaching hardware is serviceable (72-21-00,AIR INLET - INSPECTION/CHECK).


752.-

RH (PW206C) Engine Externals.- No. 5 BearingHeat Shield (Pre-SB28174); Do a general visualcheck of the heat shield for evidence of cracks asfollows (Ref. 72-00-30, INSPECTION):

PW207CNew heat shield:

Every 25 hours for the first 50 hours

30-Jul-07 0.0 0 0.0 NEW 354.6 - 25.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.

753.-


PW207CNew heat shield: in

service for more than 50 hours with no

cracks

30-Jul-07 50.0 0 0.0 NEW 304.6 - 100.0 - - VISUAL CHECK

754.-


PW207C Heat shield: with acceptable cracks 30-Jul-07 0.0 0 0.0 NEW 354.6 - 10.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.



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. RH ENGINE PW207C S/N PCE-BH0128 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009. TABLE 1, Scheduled Maintenance Checks

755.-RH Oil .- Oil Filter; Remove and replace the oilfilter (Ref. 79-21-00, OIL SYSTEM(DISTRIBUTION) - MAINTENANCE PRACTICES).


756.-RH Oil .- Chip Detector; Do an operational checkof the chip detector (Ref. 79-31-00, OIL SYSTEM(INDICATING) MAINTENANCE PRACTICES)

PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - - - 1 YR OPERATIONAL CHECK - - 25-Nov-10 - - 176.7


(INDICATING) - MAINTENANCE PRACTICES).

757.-

RH (PW206C) Oil .- Oil Filler Cap (Pre-SB28222);Do an oil filler cap handle tension inspection (Ref.79-11-00, OIL SYSTEM (STORAGE) -MAINTENANCE PRACTICES).

PW207C PCE-BH0128 03-Oct-07 0.0 0 0.0 NEW 354.6 - - - 1 YR INSPECTION

758.-RH Fuel.- Fuel Filter; Remove and replace thefuel filter (Ref. 73-21-50, FUEL PUMP FILTER -MAINTENANCE PRACTICES).



759.-

RH Fuel.- Fuel Nozzles; Clean and do a functionalcheck of the fuel nozzles (Ref. CMM 3040870).Inspect the fuel nozzle inlet screens. Ifcontamination is found, follow the Fuel ImpendingBy-Pass Indicator Activated fault isolation chart (Ref. 72-00-00).


760.-

RH (PW206C) Fuel.- Fuel Accumulator (Pre-SB28164); A general visual check for a bellowsfailure indication (through the pop-out indicator). If PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - VISUAL CHECK NOT APPLICABLE BY ENGINE MODEL.an indication is present, replace the fuelaccumulator.

761.-RH Ignition.- Igniter Plug; Do a detailed visualcheck of the igniter plug for erosion (Ref. 74-11-00, ENGINE IGNITION - INSPECTION/CHECKS).


762.-RH Ignition.- Igniter Plug; Do a functional check toverify operating capabilities (Ref. 74-11-00,ENGINE IGNITION - INSPECTION/CHECKS).


763.-RH Ignition.- Ignition Cables; Do a general visualcheck on the wires for evidence of chafing, cracks,corrosion and wear.


764.-RH Power Management.- Electronic EngineControl (EEC); Do an EEC diode failure check(Ref. 73-21-20, EEC - INSPECTION/CHECKS).

PW207C PCE-BH0128 03-Oct-07 0.0 0 0.0 0.0 354.6 - - - 1 YR CHECK

RH Power Management.- EEC/Fuel Management

DELETED FROM MAINTENANCE MANUAL

765.-

RH Power Management. EEC/Fuel ManagementModule; Do a manual mode response check anddo an operational check of the alternate engineshutdown system. (Ref. applicable aircraft manual).

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 0.0 354.6 - 800.0 - - CHECK 800.0 - - 445.4 - -

766.-

LH FMM P3 Feed.- Inspect the P3 nipple on theoutput shaft cover for presence of debris (Ref. 73-21-10, FUEL MANAGEMENT MODULEINSPECTION CHECK).

PW207C PCE-BH0128 08-Dec-08 193.6 494 0.0 -6.4 161.0 - 200.0 - - INSPECTION 400.0 - - 45.4 - - New req:


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. RH ENGINE PW207C S/N PCE-BH0128 ; 05-20-00 SCHEDULED MAINTENANCE CHECKS ISSUED DATE Sep 25/2009. TABLE 2, Perform compressor washes as scheduled.

767.-RH ENGINE.- Compressor wash "Desalination";Continually salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - 1 DAY WASH

768.-RH ENGINE.- Compressor wash "Desalination";Frequently salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - WEECKLY WASHWeekly (increase washing

frequency to suit engine condition)

Daily (increasewashing frequency to suit engine condition)


769.-RH ENGINE.- Compressor wash "Desalination";Occasionally salt-laden operating environment,Desalination wash (Ref. 71-00-00)

PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - BIWEECKLY WASH


PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - 50.0 - - WASH 350.0 - - -4.6 - -


PW207C PCE-BH0128 25-Nov-09 300.0 370 0.0 0.0 54.6 - 100.0 - - WASH 400.0 - - 45.4 - -

Biweekly (increase washingfrequency to suit engine condition)

772.- RH ENGINE.- Performance recovery; Performancerecovery wash (Ref. 71-00-00) PW207C PCE-BH0128 30-Jul-07 0.0 0 0.0 NEW 354.6 - - - - WASH

. PRATT & WHITNEY PE207C ENGINE 2 S/N PCE-BH0128; AIRWORTHINESS LIMITATIONS ISSUED DATE May 08/2009

. TABLE 2, PW207C Engines, Part Numbers for Automatic Life Cycle Counting773.- Data Collection Unit 3054276-01 - 03-Oct-07 0.0 0 0 NEW 548 - - - - REPLACEMENT

774.- Data Collection Unit (Post-SB28273) 3054276-02 - 03-Oct-07 0.0 0 0 NEW 548 - - - - REPLACEMENT

775.- LH Impeller 3058672-01 A0024WB5 03-Oct-07 0.0 0 0 NEW 548 - - 15000 - REPLACEMENT - 15000 - - 14452 -776.- LH Compressor Turbine Disk 3048999-01 A0025RLX 03-Oct-07 0.0 0 0 NEW 548 - - 10000 - REPLACEMENT - 10000 - - 9452 -

ON CONDITION

As required to suit engine operating conditions as indicated by engine condition trend monitoring system.

ON CONDITION

776. LH Compressor Turbine Disk 3048999 01 A0025RLX 03 Oct 07 0.0 0 0 NEW 548 10000 10000 9452777.- LH Power Turbine Disk 3044188-01 A00263A9 03-Oct-07 0.0 0 0 NEW 548 - - 15000 - REPLACEMENT - 15000 - - 14452 -

. TABLE 4, PW207C Engine Turbine/Turboshaft Rotor Components - Service Life778.- LH Impeller 3058672-01 A0024WB5 03-Oct-07 0.0 0 0 0 0 - - 15000 - REPLACEMENT - 15000 - - 15000 -779.- LH Compressor Turbine Disk 3048999-01 A0025RLX 03-Oct-07 0.0 0 0 0 0 - - 10000 - REPLACEMENT - 10000 - - 10000 -780.- LH Power Turbine Disk 3044188-01 A00263A9 03-Oct-07 0.0 0 0 0 0 - - 15000 - REPLACEMENT - 15000 - - 15000 -


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SB Number or Once orAD Number. Recurr Hrs Date Hrs Date Hrs Date Hrs Date

781.- BT-109S-26 MANDATORY 17-Apr-09 Once - 28-Feb-10 - -93.5

782.- BT-109S-31 MANDATORY 3-Aug-09 Once - 30-Sep-10 - 120.5 EN PROCESO WO#12300.1.2

APLICAR, INSTALADO N/P 109-0162-01-101 N/S P200547. REWORK OF THE TAIL ROTOR HUB AND BLADES ASSY P/N 109-0162-01-101. Within and not later than September 30, 2010.

Issue Date DescriptionTime Remaining

. AMENDMENTDate/Time Next Due

Metodo de CumplimientoInterval

NOTES &OBSERVATIONS

AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINS

TAIL ROTOR CONTROL ROD ASSY P/N 109-0032-14-105 "UNA TANTUM" (ONE TIME) INSPECTION FOR INTERFERENCE AND LEFT SIDE TUBES INSTALLATION P/N 109-0322-11-401 REWORK BY THE APPLICATION OF THE KIT P/N 109-0824-43-101.

PART II^: Within and not later than February 28, 2010. APLICAR PARTE II

783.- BT-109S-34 MANDATORY 16-Nov-09 Once - 30-Sep-10 - 120.5

784.- BT-109S-35 MANDATORY 11-Dec-09 Once 341.5 - 50 - - 391.5 30-Jun-10 36.9 28.5

785.- BT-109S-36 OPTIONAL 26-Apr-10 Once - - -

786 - BT-109S-36 OPTIONAL 26-Apr-10 Once - - -

APLICAR HAY GARANTIAREPLACEMENT OF THE EFIS P/N 109-0900-71-1A01 OR -2A01 (ASTRONAUTICS P/N 193850-1, -3, -101 AND -103). Within and not later than September 30, 2010.

APLICAR HAY GARANTIAMODIFICATION OF THE “BATT BUS” CIRCUIT BREAKER INSTALLATION.

REPLACEMENT OF THE FLIGHT DIRECTOR COMPUTER, BY MEANS OF THE APPLICATION OF KIT P/N 109-0824-44-101.

REPLACEMENT OF THE HELIPILOT COMPUTERS, BY MEANS OF THE APPLICATION OF

HELICOPTERS AFFECTED: The Agusta A109S helicopters up to S/N 22151 included. COMPLIANCE: At Operator’s option.APLICAR.

APLICAR, NO HAYGARANTIA.

HELICOPTERS AFFECTED: All Agusta A109S helicopters up to S/N 22151 included. COMPLIANCE: At Operator’s option. APLICAR, NO HAY786.- BT-109S-36 OPTIONAL 26-Apr-10 Once - - -

787.- SAIB SW-08-03 R2 RECOMMENDED 15-Jan-10 Once

788.- SAIB CE-10-11 R1 RECOMMENDED 14-Jan-10 Once

Recommendations for Rotorcraft During Icing Conditions

We highly recommend and strongly urge you to perform the following: • Review the aircraft Flight Manual for Limitations and Operations guidance in falling/blowing snow and/or icing. Many aircraft are prohibited from operating in known icing and/or falling and blowing snow. •

Perform basic airmanship and preflight by evaluating current and predicted weather briefings from the area Flight Service Station. AGREGAR UNA COPIA PARA LOS PILOTOS.

AGREGAR UNA COPIA PARA LOSPILOTOS.

Electrical: Fire Hazard in Resetting Circuit Breakers (C/Bs)

RECOMMENDED, The rules, either CAR 3, § 3.691 or 14 CFR § 23.1357, require the C/Bs that are essential for safety in flight be located and marked so they can be reset in flight. The rules do not require segregation of non-essential C/Bs. This SAIB references the most current “best

practices” for circuit breakers, the electrical system and aging wiring. It is important to note that many older aircraft may have little or no guidance on resetting policy in their airplane flight manuals AGREGAR UNA COPIA PARA LOS PILOTOS

AGREGAR UNA COPIA PARA LOSPILOTOS.

KITS P/N 109-0824-45-101 AND -103. APLICAR. GARANTIA.

789.- AD2010-04-16 39-16209 8-Mar-10 Once - Mar-10 - 3 MO - - 7-Jun-10 - 5.8

790.- SAIB CE-10-22 RECOMMENDED 26-Mar-10 Once

guidance on resetting policy in their airplane flight manuals. AGREGAR UNA COPIA PARA LOS PILOTOS.

This SAIB advises you of an airworthiness concern regarding all modification levels of Honeywell GNS Series Navigation Systems: GNS_XLS PRNAV, part number (P/N) 17960-0103-XXX; GNS_XLS Enhanced PRNAV, P/N 17960-0204-XXX; and GNS_XL PRNAV, P/N 18355-0102-0XXX.

Recommendations, After reviewing the above data, we recommend that you adhere steps in page 1. VERIFICAR POR EQUIPO INSTALADO. VERIFICAR POR EQUIPOINSTALADO.

AD applies to Type H1-10 AIR Halon 1211 (BCF) portable fire extinguishers manufactured by SICLI, having part number (P/N) 1708337B4 and having any serial number listed in Table 1 of this AD.

VERIFICAR POR EQUIPOINSTALADO.

791.- AD2010-07-02 39-16246 3-May-10 Once - May-10 - 30 MO - - 1-Nov-12 - 883.6

792.- P&WC S.B. No. A28280 R5 CATEGORY 3 25-Mar-10 Once 0.0 Apr-06 4000 - 4000.0 - 3452.0 -

793.- P&W SB28248 R1 CATEGORY 7 28-Oct-09 Once

TURBOSHAFT ENGINE COMPRESSOR DISC INSPECTION OF AND RETAINING NUT REPLACEMENT "ENGINE LH & RH"

CERTIFICAR, NO APLICA PORNUMERO DE SERIE DE LOS MOTOR.LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.

AD applies to Honeywell Primus II RNZ-850( )/-851( ) INUs installed on any aircraft, regardless of whether the aircraft has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD.


Effectivity PW207C Engines.. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR.TURBOSHAFT ENGINE CENTRIFUGAL IMPELLER - REPLACEMENT OF LH & RH APLICAR NO HAYGARANTIA

794.- P&WC S.B. No. 28285 R1 CATEGORY 5 4-Feb-10 OnceTURBOSHAFT ENGINE COMPRESSOR TURBINE STATOR ASSEMBLY - REPLACEMENT OF "LH & RH ENGINE"

Effectivity PW206C Engines which are before and include Serial No. PCE-BC0611, PW207C Engines which are before and include Serial No. PCE-BH0068. CATEGORY 5 - P&WC recommends to do this service bulletin when the engine is disassembled and access is available to the

necessary subassembly (i.e. module, accessories, components, or build groups). Do all spare subassemblies. CERTIFICAR, NO APLICA POR NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.

CERTIFICAR, NO APLICA PORNUMERO DE SERIE DE LOS MOTOR.LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.

GARANTIA


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795.- P&WC S.B. No. 28301 R3 CATEGORY 5 5-Feb-10 Once

AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINSNOTES &OBSERVATIONS. AMENDMENT Issue Date Description

Date/Time Interval

Effectivity PW206C Engines which are before and include Serial No. PCE-BC0763. PW207C Engines which are before and include Serial No. PCE-BH0281 and Serial No. PCE-BH0283 thru Serial No. PCE-BH0305.CATEGORY 5 - P&WC recommends to do this service bulletin when

the engine is disassembled and access is available to the necessary subassembly (i.e. module, accessories, components, or build groups). Do all spare subassemblies. CERTIFICAR, PCW SB28301 R2, JAN-23-2010, AT A/CT T.T. 318:30 HRS & 756 CYC BY PHOENIX ENGINE

SERVICE WO# 1081 AP 214769163 JONNIE B. SMITH.

CERTIFICAR, PCW JAN-23-2010, ATA/CT T.T. 318:30 HRS & 756 CYC BYPHOENIX ENGINE SERVICE WO# 1081AP 214769163 JONNIE B. SMITH.

Next Due Time RemainingMetodo de Cumplimiento

TURBOSHAFT ENGINE COMBUSTION CHAMBER LINER - REPLACEMENT OF "LH & RH ENGINE"


797.- P&WC S.B. No. 28305 R1 CATEGORY 7 8-Mar-10 OnceTURBOSHAFT ENGINE COMPRESSOR IMPELLER AND HOUSING SET - REPLACEMENT/MODIFICATION OF "ENGINE LH & RH"

Effectivity PW207C Engines which are before and include Serial No. PCE-BH0479. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.

APLICAR, NUMERO DE SERIE DE LOSMOTOR. LH S/N PCE-BH-0141, RH S/NPCE-BH-0128.

Effectivity: PW206C Engines which are before and include Serial No PCE BC0769 Serial No PCE BC0771 thru Serial No PCE BC0785 and

TURBOSHAFT ENGINE FUEL MANAGEMENT MODULE - REPLACEMENT OF "ENGINE LH & RH"

Effectivity PW206C Engines which are before and include Serial No. PCE-BC0774. PW207C Engines which are before and include Serial No. PCE-BH0328. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE

SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.



799.- P&WC S.B. No. 28310 R1 CATEGORY 7 21-Apr-10 Once

800 P&W SB28314 CATEGORY 7 10 Nov 09 Once

TURBOSHAFT ENGINE DISK BALANCING ASSEMBLY, COMPRESSOR TURBINE - REPLACEMENT OF "ENGINE LH & RH"

Effectivity, PW206B2 Engines. PW206C Engines. PW207C Engines. PW207D Engines. CATEGORY 7 - You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.


TURBOSHAFT ENGINE COMPRESSOR CENTRIFUGAL IMPELLER - REPLACEMENT OF "ENGINE LH & RH"

Effectivity: PW206C Engines which are before and include Serial No. PCE-BC0769, Serial No. PCE-BC0771 thru Serial No. PCE-BC0785 and Serial No. PCE-BC0787 thru PCE-BC0794. PW207C Engines which are before and include Serial No. PCE-BH0281, Serial No. PCE-BH0283 thru Serial No. Serial No. PCE-BH0305 and Serial No. PCE-BH0307 thru PCE-BH0376. CATEGORY 7 - You can do this service bulletin when

the supply of superseded parts is fully used. You can do this service bulletin when the supply of superseded parts is fully used. APLICAR, NUMERO DE SERIE DE LOS MOTOR. LH S/N PCE-BH-0141, RH S/N PCE-BH-0128.


TURBOSHAFT ENGINE REDUCTION GEARBOX HOUSING, REAR - Effectivity PW207C Engines which are before and include Serial No. PCE-BH0478. CATEGORY 5 - P&WC recommends to do this service

bulletin when the engine is disassembled and access is available to the necessary subassembly (i e module accessories components or build APLICAR NO HAY800.- P&W SB28314 CATEGORY 7 10-Nov-09 Once

801.- SAIB NE-10-28 RECOMMENDED 22-Apr-10 Once

802.- AD2010-09-04 39-16269 14-May-10 Once - May-10 - 14 DAYS - - 28-May-10 -

TURBOSHAFT ENGINE REDUCTION GEARBOX HOUSING, REAR REPLACEMENT/MODIFICATION OF LH & RH bulletin when the engine is disassembled and access is available to the necessary subassembly (i.e. module, accessories, components, or build

groups). Do all spare subassemblies. APLICAR.

TO PROVIDE THE FLIGHTCREW WITH PROCEDURES TO RECOVER FROM OR WORK AROUND THESE SOFTWARE ANOMALIES DURING FLIGHT.


C OGARANTIA

The FAA reminds owners and operators of aircraft that loose equipment on the glare shield or in the cockpit can present a hazard particularly AGREGAR UNA COPIA AL

TURBINE ENGINE OPERATION IN VOLCANIC ASH AIRSPAEC. TO HIGHLIGHT RECENT ACTIONS AND EMPHASIZE THE NEED FOR OPERATOR AWARENESS. AGREGAR UNA COPIA AL MANUAL DE VUELO DE LA AERONAVE.

AGREGAR UNA COPIA ALMANUAL DE VUELO DE LAAERONAVE.

803.- SAIB CE-10-35 RECOMMENDED 24-May-10 OnceThe FAA reminds owners and operators of aircraft that loose equipment on the glare shield or in the cockpit can present a hazard, particularly for aircraft with a windshield heater system installed where electrical terminal strips may be exposed and subject to short circuit. AGREGAR

UNA COPIA AL MANUAL DE VUELO DE LA AERONAVE.

AGREGAR UNA COPIA ALMANUAL DE VUELO DE LAAERONAVE.

Loose Equipment in the Flight Compartment and on Glare Shields


G.M.J.P. 39 de 39

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