ENGINE MINI PACK - AJW Group

A J Walter Leasing Ireland Limited, One Spencer Dock, North Wall Quay, Dublin 1, Ireland

E: [email protected] W: www.ajw-aviation.com

ENGINE MINI PACK

Engine Model:CFM56-5B6/P

Engine Serial Number:575355

Condition:Serviceable, continued time September 2020

TSN: 40,525:18

CSN: 20,557

TSLSV: 12,458:18

CSLSV: 6,432

LLP Limiter: 4,443 – LPT

Last shop Visit: Air France – Feb 2016

Tag date September 2020

LocationIreland

Additional details For additional details on this unit please contact the AJW Engines Team.

mailto:[email protected]

Wasim.Akhtar

Typewritten text

T: 00 44 7552 812215

№

18/4 Pilotov st., St.Petersburg, 196210, Russian Federation 15А Leninskiy prospekt, Moscow, 119071, Russian Federation

tel.: +7 (812) 6 333 700, fax:+7 (812) 6 333 810 [email protected]

To whom it may concern

Engine Non Incident Statement

Subject: Non Incident Statement. Date: 29.05.2020 To whom it may concern: Engine Model: CFM56-5B5/P Engine Serial Number: 575355 Total time at Induction: 32097:33 Total Cycles at Induction: 16850 Total Time at Re-delivery: 40525:18 Total Cycles at Re-delivery: 20557

This Letter is to confirm that with regard to the above mentioned CFM56-5B5/P Engine bearing manufacturer serial number 575355, we hereby confirm that to the best of our knowledge the above mentioned Engine, together with its subparts and components, during its operation with “Rossiya airlines” JSC, from 7th February 2018 until 18th April 2020:

a) Has not been involved in any accident (according to I.C.A.O Annex 13 Paragraph B), serious incident(according to I.C.A.O Annex 13 chapter 1) or subjected to severe impact, stress, heat or fire.

b) Has not been operated by or obtained from any government or military entities.c) Has not had any parts acquired from any government or military source.d) Has not been immersed in salt water or otherwise exposed to corrosive agents outside normal operation.

Furthermore, during the time the above mentioned engine was operated by “Rossiya airlines” JSC, we can confirm that this engine was not altered from its original approved Type Certificate or Type Design.

Igor Tylesov Maintenance Quality manager «Rossiya airlines» JSC Tel./Fax. +7(812) 6-333-950 E-mail: [email protected]

29.941029.05.2020

mailto:[email protected]

№

18/4 Pilotov st., St.Petersburg, 196210, Russian Federation 15А Leninskiy prospekt, Moscow, 119071, Russian Federation

tel.: +7 (812) 6 333 700, fax:+7 (812) 6 333 810 [email protected]

To whom it may concern

STATEMENT OF CONFORMITY

Engine Model: CFM56-5B5/P

MFR S/N 575355

Total time at induction: 32097:33 FH

Total cycles at induction: 16850 FC

Total time at re-delivery: 40525:18 FH

Total cycles at re-delivery: 20557 FC

This Letter is to confirm that with regard to the above mentioned CFM56-5B5/P Engine bearing manufacturer serial number 575355, we hereby confirm that to the best of our knowledge the above mentioned Engine, together with its subparts and components, during its operation with “Rossiya airlines” JSC, from 7th February 2018 until 18th April 2020:

1. Has been maintained in accordance with an approved Maintenance Program andin compliance with the manufacturer’s guidelines, standard practices and the applicable Civil Aviation regulatory requirements;

2. Has not been ETOPS operated, nor has the ETOPS status been modified;3. Has been operated using the following Oils and Fluids:

a. Oil – Mobil Jet Oil IIb. Hydraulic Fluid – HY JET 4A plus

4. Had no PMA or unapproved parts installed;5. Had no DER or non-TCH repairs or modifications incorporated;6. Has been operated with CIS or TS-1 Fuel;7. Had no abnormal occurrence, no operating limitation were reached or exceed in

accordance with the Engine manufacture and Aircraft Maintenance Manual; 8. Has not been subjected to operations within volcanic ash effected areas;

Furthermore, during the time the above mentioned engine was operated by “Rossiya airlines” JSC, we can confirm that this engine was operated at the following power ratings:

• 22000 Pounds of Thrust for 3101 Cycles• 23500 Pounds of Thrust for 606 Cycles

Igor Tylesov Maintenance quality manager “Rossiya airlines” JSC Tel./Fax.: +7(812) 6-333-950 E-mail: [email protected]

29.941129.05.2020

Part Number Serial Number TSN CSN TSR CSR TSLSV CSLSV

CFM56-5B5/P 575355 40 525:18 FH 20 557 FC 12 458:18 FH 6 432 FC 12 458:18 FH 6 432 FC

-5B5/P -5B6/P -5B5/P -5B6/P -5B5/P -5B6/P

213 FAN DISK 338-001-504-0 BB551369 40 525:18 20 557 3 101 17 456 30 000 30 000 9 443 9 443

211 BOOSTER SPOOL 338-001-906-0 DC094076 40 525:18 20 557 3 101 17 456 30 000 30 000 9 443 9 443

221 FAN SHAFT 338-010-601-0 DC055383 40 525:18 20 557 3 101 17 456 30 000 30 000 9 443 9 443

312 HPC FRONT SHAFT 1386M56P03 NCU30740 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

313 HPC STAGE 1/2 SPOOL 1558M31G07 FGB0AHF1 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

314 HPC STAGE 3 DISK 2116M23P01 XAEGD466 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

315 HPC STAGE 4/9 SPOOL 2048M20G04 GWN1032F 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

316 HPC REAR AIR SEAL 2116M25P01 GFF5J6AE 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

521 HPT FRONT SHAFT 2048M21P03 XAEGA327 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

522 HPT FRONT AIR SEAL 2116M20P02 TMT3TM14 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

525 HPT ROTOR DISK 1498M43P07 GWN10352 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

526 HPT REAR SHAFT 1864M90P04 TMTD1627 12 458:18 6 432 3 101 3 331 20 000 20 000 13 568 13 568

542 LPT STAGE 1 DISK 336-001-804-0 BB685786 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

543 LPT STAGE 2 DISK 336-001-909-0 BB725296 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

544 LPT STAGE 3 DISK 336-002-006-0 BB739408 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

545 LPT STAGE 4 DISK 336-002-105-0 BB712708 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

546 LPT CONICAL SUPPORT 338-077-502-0 BB472009 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

551 LPT SHAFT 338-010-005-0 BB635242 40 525:18 20 557 3 101 17 456 25 000 25 000 4 443 4 443

541 LPT CASE 338-117-452-0 DB675481 40 525:18 20 557 3 101 17 456 N/L N/L N/L N/L

561 LPT REAR FRAME 338-171-703-0 LA091763 40 525:18 20 557 3 101 17 456 25 000* 25 000* 4 443* 4 443*

N/L - not limited.

* LIMIT FOR FIRST INSPECTION PER SB 72-620

Anton Vlasov 25-May-2020

Powerplant Engineer

Rossiya Airlines JSC

Remaining cyclesTotal cycles category

ENGINE LLP STATUS REPORT

IIN Description Part Number Serial NumberTotal Flight

Hours

Total Flight

Cycles

Limit

CHG. 39 BORESCOPE INSPECTION CFM56-5

O. HARARI ISSUED BY: DATE: 15.12.2019

REF: ESM NDT MANUAL PART 7

AMM 72-00-00 Y. ALON APPROVED BY:

ESN: 575355 Inspection Date: 24.06.2020 Page 2 of 12

ISSUED:01.06.2011 REVISED:05.2020 WS: 360E0012

Low Pressure Compressor Module:

Location Port EA Findings Remarks

Fan Blades 36 3ea Fan blades with blend repair. See attached ROSSIYA

report

IAW AMM 72-00-00: Serviceable Not Serviceable







Low Pressure Compressor Module:


LPC Stage 2

Rotor

64 Normal



LPC Stage 3

Rotor

S0 70 Normal



LPC Stage 4

Rotor

S0 70 Normal



LPC Stage 5

Rotor

S0 68 Normal








High Pressure Compressor Module:


HPC Stage 1

Rotor

S1

S2

38 Normal



HPC Stage 2

Rotor

S2

S3

53 Normal



HPC Stage 3

Rotor

S3

S4

60 Several blades with coating missing on T/E within AMM limits.



HPC Stage 4

Rotor

S4

S5

68 Normal










HPC Stage 5

Rotor

S5

S6

75 Several blades with L/E erosion within AMM limits



HPC Stage 6

Rotor

S6

S7




HPC Stage 7

Rotor

S7

S8




HPC Stage 8

Rotor

S8

S9

80 Normal










HPC Stage 9

Rotor

S9 76 One blade with small dent on L/E area "B" within AMM limits.








Combustion Chamber Section: Location Port EA Findings Remarks

Outer Liner

& Dome

S10 to S15

1 Exhibiting slight missing material on deflectors within AMM limits



Inner Liner S10 to S15

1 Normal



Fuel Nozzles S10 to S15

20 Normal








Combustion Chamber Section:Location Port EA Findings Remarks

HPT Nozzle

Guide Vanes

S10 to S15

42 Several vans with short axial crack within AMM limits. Several vanes with coating missing on T/E within AMMA limits.








High Pressure Turbine Module: Location Port EA Findings Remarks

HPT Stage 1

Rotor

S16

S17 80 Several blades with coating missing on L/E within AMM

limits.



HPT Stage 1

Rotor Notch

S16

S17

Blade 1 Blade 20 Blade 40 Blade 60

2.25 2.25 2 2.25



HPT Shroud S16 Several segments with cracks within AMM limits








High Pressure Turbine Module:


LPT Nozzle S17 One vane has multiple intersected cracks within AMM limits. Repeat BSI check 200 cycles. According CFMI CSC case number: CSC/CFM/2020-06/00347-A

No change from

incoming BSI.








Low Pressure Turbine Module:


LPT Stage 1

Rotor

S16

S17 162 One blade with typical out of flush within AMM limits.



LPT Stage 2

Rotor

S18 150 Several blades with small dents on L/E area "E" within AMM limits.


TREE PICTURES ILLUSTRATE THE SAME DENT







Low Pressure Turbine Module:


LPT Stage 3

Rotor

S19 150 Normal



LPT Stage 4

Rotor

S20 134 Normal


Basic Engine Parameters: VQ-BAQ - A319 - OJSC Rossiya Airlines 20 Jan 2020 - 18 Apr 2020 (90 days)

Proprietary Information – Subject to Restrictions under the Terms

Basic Engine Parameters: VQ-BAQ - A319 - OJSC Rossiya Airlines 20 Jan 2020 - 18 Apr 2020 (90 days)

Proprietary Information – Subject to Restrictions under the Terms

64 75-31 VBV POSITION SENSOR VG22-01 YY031514-3 VG22-01 YY031514-365 75-31 VBV HYDRAULIC GEAR MOTOR 396800-12 YA017088-4 396800-12 YA017088-466 75-31 VBV STOP MECHANISM 3282970-4 YG092134-V 3282970-5 02143267 75-31 ACTUATOR-BALLSCREW MASTER 121666-13 YG200938 121666-13 YG20093868 75-31 ACTUATOR-BALLSCREW 121664-8 YG112410 121664-8 YG11241069 75-31 ACTUATOR-BALLSCREW 121664-8 YG107617 121664-8 YG10761770 75-31 ACTUATOR-BALLSCREW 121664-8 YG112367 121664-8 YG11236771 75-31 ACTUATOR-BALLSCREW 121664-8 YG107011 121664-8 YG10701172 75-31 ACTUATOR-BALLSCREW 121664-8 YG112408 121664-8 YG11240873 75-31 ACTUATOR-BALLSCREW 121664-8 YG112366 121664-8 YG11236674 75-31 ACTUATOR-BALLSCREW 121664-8 YG112382 121664-8 YG11238275 75-31 ACTUATOR-BALLSCREW 121664-8 YG112411 121664-8 YG11241176 75-31 ACTUATOR-BALLSCREW 121664-8 YG112403 121664-8 YG11240377 75-31 ACTUATOR-BALLSCREW 121664-8 YG107629 121664-8 YG10762978 75-31 ACTUATOR-BALLSCREW 121664-8 YG107631 121664-8 YG10763179 75-32 ACTUATOR 1211313-230 Not visible 1211313-230 Wasn't replaced80 75-32 ACTUATOR 1211313-230 APMMN071 1211313-230 APMMN07181 77-11 N1 SPEED SENSOR Not visible Not visible Wasn't replaced Wasn't replaced82 77-11 N2 SPEED SENSOR Not visible Not visible Wasn't replaced Wasn't replaced83 77-21 HARNESS-WIRING EGT UPPER Not visible Not visible Wasn't replaced Wasn't replaced84 77-21 HARNESS-WIRING EGT LOWER Not visible Not visible Wasn't replaced Wasn't replaced85 77-21 EGT COUPLING CA213-00 YC391932A CA213-00 YC391932A86 77-21 HARNESS-WIRING EGT 2TC LOW L/H TC315-01 YC4242550707Y TC315-01 YC4242550707Y87 77-21 HARNESS-WIRING EGT 2TC UP L/H TC315-01 YC42454-0707 TC315-01 YC42454-070788 77-21 HARNESS-WIRING EGT 2TC LOW R/H TC315-01 424543H-0707 TC315-01 424543H-070789 77-21 HARNESS-WIRING EGT 3TC UP R/H TC315-01 YC4324251-0903 TC315-01 YC4324251-090390 77-23 T3 TEMPERATURE SENSOR 8TC19AAR1 GDBV327G 8TC19AAR1 GDBV327G91 77-30 N2 VIBRATION SENSOR Not visible Not visible Wasn't replaced Wasn't replaced92 77-31 BEARING NO.1 VIBRATION SENSOR Not visible Not visible Wasn't replaced Wasn't replaced93 79-11 OIL TANK 24F5202 YT096424-E 24F5202 YT096424-E94 79-21 INDICATOR-VISUAL 1605100-01 YU061976-9 1605100-01 YU061976-995 79-21 LUBRICATION UNIT 337-075-105-0 10184 337-075-105-0 1018496 79-21 OIL FILTER DIFF. PRESSURE SWITCH QA07638ISS1 Not visible Wasn't replaced Wasn't replaced97 79-21 FUEL/OIL HEAT EXCHANGER 11-841193-4 YY081178-A 11-841193-4 YY081178-A98 79-31 OIL QUANTITY TRANSMITTER 74-110-10 AAR0321 74-110-10 AAR032199 79-32 OIL TEMPERATURE TRANSMITTER Not visible Not visible Wasn't replaced Wasn't replaced

100 80-11 AIR STARTER 3505582-65 YG336375-AC 3505582-28 YG441053-2101 80-11 STARTER VALVE 3291556-2 YG321649-8 3291556-2 YG321649-8102 80-13 LOWER STARTER DUCT Not visible Not visible Wasn't replaced Wasn't replaced103 80-13 UPPER STARTER DUCT 990998-74-107 1234 990998-74-107 1234104 72-63 ACCESSORY GEARBOX - AGB 338-089-702-0 WJ3177 338-089-702-0 WJ3177105 72-62 TRANSFER GEARBOX - TGB 338-089-601-0 VJ3529 338-089-601-0 VJ3529106 71-00 CORE NOZZLE 642-4001-501 7523001 642-4001-501 7523001107 71-00 CENTERBODY Not visible Not visible Wasn't replaced Wasn't replaced108 71-00 HARNESS - IDG POWER FEED 642W9817-501 832164404-1 642W9817-501 832164404-1109 71-00 MID-STAGE "T" DUCT ASSY 642-5503-501 1511 642-5503-501 1511110 71-00 HP BLEED "T" DUCT ASSY 642-5511-503 913 642-5511-503 913111 71-00 LOWER HP BLEED DUCT ASSY 642-5501-501 912 642-5501-501 912112 71-00 UPPER HP BLEED DUCT ASSY 642-5508-503 916 642-5508-503 916113 71-00 HARNESS N1 VIBRATION SENSOR 642W9818-503 No S/N Wasn't replaced Wasn't replaced114 30-21 LOWER CORE ANTI-ICE BLEED DUCT 14495-507 K-75201 14495-507 K-75201115 30-21 UPPER CORE ANTI-ICE BLEED DUCT 238-0602-503 1245 238-0602-503 1245116 30-21 FWD ANTI-ICE BLEED DUCT 14495-505 K-50367 14495-505 K-50367117 74-11 IGNITION EXCITER BOX - UPPER 10-631045-2 UNJA6224 10-631045-2 UNJA6224118 74-11 IGNITION EXCITER BOX - LOWER 10-631045-2 UNJNG873 10-631045-2 UNJNG873

Anton Vlasov 09.May.2020Powerplant engineer"Rossiya Airlines" JSC

Part Number Serial Number Part Number Serial Number

1 24-11 IDG 740119H 3332 740119H 06502 24-21 QAD ADAPTER 740123A 3315 740123A 42023 29-11 EDP 3031863-001 60420378 3031863-001 604203784 29-11 EDP PRESSURE SWITCH Not visible Not visible Wasn't replaced Wasn't replaced5 29-13 HYDRAULIC FILTER ASSY QA06305 RL8-3779 QA06305 RL8-37796 30-21 ANTI-ICE VALVE 327155-3 2868 327155-3 28687 36-11 IP CHECK VALVE 2293B020000 02351 2293B020000 021348 36-11 HP REGULATING VALVE 6773B020000 0362 6773B020000 03629 36-11 BP REGULATING VALVE 6773E010000 02623 6773E010000 02623

10 71-21 FWD ENGINE MOUNT 642-2000-25 P2275 642-2000-25 P227511 71-22 AFT ENGINE MOUNT 642-2300-3 P1681 642-2300-3 P168112 73-11 FUEL PUMP 724400-2 YA007523-8 724400-2 YA007523-813 73-11 SERVO FUEL HEATER 45731-1382 YB003893-H 45731-1382 Y8003893-H14 73-11 DOWNSTREAM FUEL FILTER FA00914D YY016707-A FA00914D YY016707-A15 73-11 FUEL RETURN VALVE 8910-332 YP049010-D 8910-332 EM550063-316 73-11 IDG OIL COOLER 45731-1391 YB006233-A 45731-1391 YB006233-A17 73-11 NOZZLE-FUEL 6840023M1 PCY3979A 6840023M1 PCY3979A18 73-11 NOZZLE-FUEL 6840023M1 PHCB1533 6840023M1 PHCB153319 73-11 NOZZLE-FUEL 6840023M1 PHCB7853 6840023M1 PHCB785320 73-11 NOZZLE-FUEL 6840023M1 PCY498D3 6840023M1 PCY498D321 73-11 NOZZLE-FUEL 6840023M1 PCY5999P 6840023M1 PCY5999P22 73-11 NOZZLE-FUEL 6840023M1 PCY9180J 6840023M1 PCY9180J23 73-11 NOZZLE-FUEL 6840023M1 PCY676E1 6840023M1 PCY676E124 73-11 NOZZLE-FUEL 6840023M1 PCY4736P 6840023M1 PCY4736P25 73-11 NOZZLE-FUEL 6840023M1 PCY4928M 6840023M1 PCY4928M26 73-11 NOZZLE-FUEL 6840023M1 PCY9551T 6840023M1 PCY9551T27 73-11 NOZZLE-FUEL 6840023M1 PCY2592M 6840023M1 PCY2592M28 73-11 NOZZLE-FUEL 6840023M1 PCY514D6 6840023M1 PCY514D629 73-11 NOZZLE-FUEL 6840023M1 PCY513D3 6840023M1 PCY513D330 73-11 NOZZLE-FUEL 6840023M1 PCY9193T 6840023M1 PCY9193T31 73-11 NOZZLE-FUEL 6840023M1 PCY3388K 6840023M1 PCY3388K32 73-11 NOZZLE-FUEL 6840023M1 PCY4505T 6840023M1 PCY4505T33 73-11 NOZZLE-FUEL STARTER 6840023E16 PCYFT837 6840023E16 PCYFT83734 73-11 NOZZLE-FUEL STARTER 6840023E16 OHPK2015 6840023E16 OHPK201535 73-11 NOZZLE-FUEL STARTER 6840023E16 PCYPS413 6840023E16 PCYPS41336 73-11 NOZZLE-FUEL STARTER 6840023E16 PHCFN751 6840023E16 PHCFN75137 73-21 HPTCC THERMOCOUPLE 910-00510 TCC02058 910-00510 TCC0205838 73-21 ECU 2123M56P01 LMDN2338 2123M56P01 LMDN233839 72-00 ID PLUG FOR CFM56-5B6P 390-611-501-0 Not visible Missing Missing40 73-21 HMU 8061-526 WYGB2710 8061-536 WYGB005541 73-21 SENSOR-TEMP T12 RP198-02 DH914939 RP198-02 DH91493942 73-21 SENSOR T25 RP216-00 YC056623 RP216-00 YC05662343 73-21 AC GENERATOR STATOR 87006-9 HTL15702 87006-9 HTL1570244 73-21 AC GENERATOR ROTOR 85465-2 HTLR9340 85465-2 HTLR934045 73-21 FUEL FLOW TRANSMITTER 8TJ167GHH1 GDB5642M 8TJ167GHH1 GDB5642M46 73-21 HARNESS-WIRING J7 Not visible Not visible Wasn't replaced Wasn't replaced47 73-21 HARNESS-WIRING J8 Not visible Not visible Wasn't replaced Wasn't replaced48 73-21 HARNESS-WIRING J9 Not visible Not visible Wasn't replaced Wasn't replaced49 73-21 HARNESS-WIRING J10 Not visible Not visible Wasn't replaced Wasn't replaced50 73-21 HARNESS-WIRING J11 Not visible Not visible Wasn't replaced Wasn't replaced51 73-21 HARNESS-WIRING CJ11R Not visible Not visible Wasn't replaced Wasn't replaced52 73-21 HARNESS-WIRING CJ11L Not visible Not visible Wasn't replaced Wasn't replaced53 73-21 HARNESS-WIRING J12 Not visible Not visible Wasn't replaced Wasn't replaced54 73-21 HARNESS-WIRING CJ12R Not visible Not visible Wasn't replaced Wasn't replaced55 73-21 HARNESS-WIRING CJ12L Not visible Not visible Wasn't replaced Wasn't replaced56 73-21 HARNESS-WIRING J13 Not visible Not visible Wasn't replaced Wasn't replaced57 73-21 HARNESS-WIRING CJ13 Not visible Not visible Wasn't replaced Wasn't replaced58 73-22 HARNESS-WIRING DPM 320-298-101-0 YH576563-K 320-298-101-0 YH576563-K59 74-21 LEAD ASSY-IGNITION R/H 9043110-16 KU5969 9043110-16 KU596960 74-21 LEAD-ASSY-IGNITION L/H 9043110-16 KU5967 9043110-16 KU596761 75-21 AIR TRANSIENT VALVE 3291390-2 GRTM8138 3291390-2 GRTM813862 75-22 LPTACC VALVE C25175000-1 YR016089-4 C25175000-1 YR016089-463 75-23 TURBINE CLEARANCE CONTROL VALVE 329695-6 WC13967-5 329695-6 WC13967-5

ESN575355 ENGINE LRU LISTING

Accessory Part NameATAItemIncoming Outgoing

Israel Aerospace Industries Ltd. BEDEK AVIATION GROUP Ben Gurion International Airport 70100 Israel

Page: 4 of 5

WS: 999AIR0001

FAA CRS No. MK1Y325K EASA APPROVAL No. 145.00

4. The following accessories / parts were not received:

Item Description Typical PN

1. HOSE D0001037900000

2. UNION D7101002320000

3. DUCT (pneumatic system 71-00-02 305) 9909873-103

4. HOSE (pneumatic system 71-00-02-01 40) 110560-17

5. HOSE (pneumatic system 71-00-02-01 70) 110551-503

6. NUT (4 EA) ( AFT ENGINE 050A ) SL4001-16

7. RETAINER (4 EA) ( AFT ENGINE 060A ) SLR4001-16B

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Document-Number Type Rev Compl/Eff Date A|C Subject Status1994-272 AD 03 Mandatory

07.Oct.1995COMP BEARING 3 AFT AIR OIL SEAL P/N 1364M71G02 INSPECTION OF HPC 1-2 SPOOL Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 1997-06-01 AD 0 (Same header)Original Document RequirementPerform BEFORE 2200/C for the first timeThereafter perform in an interval of 2200/C

Complete document sign-up hierarchy1994-272/AD Rev.03 BEARING 3 AFT AIR OIL SEAL P/N 1364M71G02 INSPECTION OF HPC 1-2 SPOOL Not Applicable

Document-Number Installed in affected Rotable Status> CFM56-5A-72-0440/SB(Rev.: 2 Issued by: CFMI)

No affected rotable installed Not Applicable

> CFM56-5B-72-0064/SB* Rev.2 FLEXIBLE BORESCOPE INSPECTION OF THE HPC STAGE 1 DISK BORE FORWARDCORNER FOR RUBS/SCRATCHES

Not Applicable

1997-06-01 AD 00 Mandatory03.Jun.1997

COMP BEARING 3 AFT AIR OIL SEAL P/N 1364M71G02 INSPECTION OF HPC 1-2 SPOOL Not Applicable

Reference(s) (Document No/Doc-Type/Revision)EASA AD 1994-272 AD 03 (Same header)

Complete document sign-up hierarchy1997-06-01/AD Rev.00 BEARING 3 AFT AIR OIL SEAL P/N 1364M71G02 INSPECTION OF HPC 1-2 SPOOL Not Applicable



> CFM56-5B-72-0064/SB* Rev.2 FLEXIBLE BORESCOPE INSPECTION OF THE HPC STAGE 1 DISK BORE FORWARDCORNER FOR RUBS/SCRATCHES

Not Applicable

Document-Number Type Rev Compl/Eff Date A|C Subject Status

For P/N: `CFM56-5B5P` S/N: `575355` (ENGINE ASSY)Selection: AIRWORTHINESS DIRECTIVE

produced by www.swiss-as.comAMOS

Modification Control Report E120068 09:00

17.Apr.2020Page 1/35

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25.Feb.1998COMP AGB/TGB GEAR SHAFT REPLACEMENT Cancelled (Cancelled)

Replacement InformationThis Document SUPERSEDES 1997-354/AD Rev.3This Document has been CANCELLED BY 1998-097/AD Rev.00

1997-354 AD 3 Mandatory24.Feb.1998

COMP AGB/TGB GEAR SHAFT REPLACEMENT Superseded (Superseded)

Replacement InformationThis Document has been SUPERSEDED BY 1997-354/AD Rev.4

1998-003 AD 03 Mandatory22.Dec.2001

COMP ESM CHAPTER 05 LLP LIST REVISION LPT CASE LIFE REDUCTION 5B1/2P, -5B2/2P,-5B3/2P,- 5B4/2P

Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 1998-02-04 AD 00 (Same header)


For P/N: `CFM56-5B5P` S/N: `575355` (ENGINE ASSY)Selection: AIRWORTHINESS DIRECTIVEFor P/N: `CFM56-5B5P` S/N: `575355` (ENGINE ASSY)Selection: AIRWORTHINESS DIRECTIVE



17.Apr.2020Page 2/35

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25.Feb.1998COMP AGB (STARTER SHAFT) / TGB (INPUT BEVEL GEAR) Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 1998-10-11 AD 00 (Same header)Replacement InformationThis Document CANCELS 1997-354/AD Rev.4Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy1998-097/AD Rev.00 AGB (STARTER SHAFT) / TGB (INPUT BEVEL GEAR) Not Applicable

Replacement InformationThis Document CANCELS 1997-354/AD Rev.4



> CFM56-5B-72-0211/SB*Rev.01

GEARSHAFT CLUSTER SPUR ASSY (31X71 TOOTH) REPLACEMENT Not Applicable by Serial Number /Special Text: Not applicable due toAGB P/N installed and for ESN





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Document-Number Type Rev Compl/Eff Date A|C Subject Status1998-10-11 AD 00 Mandatory

03.Jun.1998COMP ENGINES ARE EQUIPPED WITH A SPECIFIC ACCESSORY GEARBOX (AGB) STARTER

GEARSHAFT OR TRANSFER GEARBOX (TGB) INPUT BEVEL GEARNot Applicable

Reference(s) (Document No/Doc-Type/Revision)EASA AD F-1998-097 AD 0 (Same header)Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy1998-10-11/AD Rev.00 ENGINES ARE EQUIPPED WITH A SPECIFIC ACCESSORY GEARBOX (AGB) STARTER

GEARSHAFT OR TRANSFER GEARBOX (TGB) INPUT BEVEL GEARNot Applicable

Document-Number Installed in affected Rotable Status> CFM56-3-72-0861/SB(Rev.: 03 Issued by: CFMI)




> CFM56-5B-72-0211/SB*Rev.01

GEARSHAFT CLUSTER SPUR ASSY (31X71 TOOTH) REPLACEMENT Not Applicable by Serial Number /Special Text: Not applicable due toAGB P/N installed and for ESN





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31.Dec.1999COMP INTROD OF NEW FUEL PUMP AND INSP OF FUEL FILTER COVER ATTACH PARTS Ex Factory

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2000-15-01 AD 00 (Same header)Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy1998-427/AD Rev.02 INTROD OF NEW FUEL PUMP AND INSP OF FUEL FILTER COVER ATTACH PARTS Ex Factory

Document-Number Installed in affected Rotable Status> CFM56-5A-73-A0143/SB(Rev.: 00 Issued by: CFMI)


> CFM56-5B-73-0056/SB*Rev.02

INSPECTION OF FUEL FILTER COVER ATTACHMENT PARTS Not Applicable

> CFM56-5B-73-A0062/SB*Rev.01

INTRODUCTION OF A NEW FUEL PUMP WITH NEW FILTER COVER ATTACHMENT. Ex Factory

Reason for this StatusPN 724400-2 installed at manufacture.





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02.Oct.2000COMP INITIAL AND REPETITIVE VISUAL INSPECTIONS OF THE FUEL PUMP FILTER COVER

HELICOIL INSERTS AND BOLTS FOR DAMAGEEx Factory

Reference(s) (Document No/Doc-Type/Revision)EASA AD 1998-427 AD 2 (Same header)Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2000-15-01/AD Rev.00 INITIAL AND REPETITIVE VISUAL INSPECTIONS OF THE FUEL PUMP FILTER COVER

HELICOIL INSERTS AND BOLTS FOR DAMAGEEx Factory

Document-Number Installed in affected Rotable Status> CFM56-3-73-A0129/SB(Rev.: 00 Issued by: CFMI)


Document-Number Installed in affected Rotable Status> CFM56-5A-73-A0143/SB(Rev.: 00 Issued by: CFMI)


> CFM56-5B-73-A0062/SB*Rev.01

INTRODUCTION OF A NEW FUEL PUMP WITH NEW FILTER COVER ATTACHMENT. Ex Factory

Reason for this StatusPN 724400-2 installed at manufacture.

2000-294-IMP(B) AD 01 Mandatory24.Jul.2002

COMP INSPECTION OF FAN DISK, HPT DISK, HPT FRT AIR SEAL Superseded (Superseded)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2000-12-01 AD 00 (Same header)Replacement InformationThis Document has been SUPERSEDED BY 2002-390 IMP(B)/AD Rev.00





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11.Jun.2001COMP LIMITING ENGINES WITH CERTAIN NO. 4 BEARINGS TO ONE ON EACH AIRPLANE,

REPLACEMENT OF CERTAIN NO. 4 BEARINGSNot Applicable


Complete document sign-up hierarchy2001-11-05/AD Rev.00 LIMITING ENGINES WITH CERTAIN NO. 4 BEARINGS TO ONE ON EACH AIRPLANE,

REPLACEMENT OF CERTAIN NO. 4 BEARINGSNot Applicable



> CFM56-5B-72-A0392/SB*Rev.00

REDUCED INTERVAL FOR ELECTRICAL MASTER CHIP DETECTOR INSPECTION Not Applicable

> CFM56-5B-72-A0393/SB*Rev.00

ENGINE - LOW PRESSURE TURBINE SHAFT (72-55 -00)REPLACEMENT OF NO.4 ROLLERBEARI NG 305-355-717-0 IN A DEFECTIVE BATCH

Not Applicable

Document-Number Installed in affected Rotable Status> CFM56-7B-72-A0328/SB(Rev.: 01 Issued by: CFMI)








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26.May.2001COMP AIR STARTER - REPLACEMENT OF MAGNETIC DRAIN PLUG Not Applicable


Complete document sign-up hierarchy2001-177/AD Rev.00 AIR STARTER - REPLACEMENT OF MAGNETIC DRAIN PLUG Not Applicable



> CFM56-5B-80-0006/SB*Rev.02

REPLACEMENT OF THE MAGNETIC DRAIN PLUG 572-510-900 WITH MAGNETIC DRAINPLUG 572-8510-9152

Not Applicable

2001-207 AD 1 Mandatory23.Jun.2001

COMP #4 BEARING REPLACEMENT Cancelled (Cancelled)

Replacement InformationThis Document has been CANCELLED BY 2001-240/AD Rev.00





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25.Jun.2001COMP #4 BEARING REPLACEMENT Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2001-11-05 AD 00 (Same header)Original Document RequirementPerform WITHIN 75/H (effective from Effective Date 25.Jun.2001) for the first timeThereafter perform in an interval of 75/H

Complete document sign-up hierarchy2001-240/AD Rev.00 #4 BEARING REPLACEMENT Not Applicable



> CFM56-5B-72-A0392/SB*Rev.00

REDUCED INTERVAL FOR ELECTRICAL MASTER CHIP DETECTOR INSPECTION Not Applicable

> CFM56-5B-72-A0393/SB*Rev.00

ENGINE - LOW PRESSURE TURBINE SHAFT (72-55 -00)REPLACEMENT OF NO.4 ROLLERBEARI NG 305-355-717-0 IN A DEFECTIVE BATCH

Not Applicable









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Document-Number Type Rev Compl/Eff Date A|C Subject Status2002-02-13 AD 00 Mandatory COMP AIR STARTER - REPLACEMENT OF MAGNETIC DRAIN PLUG Not Applicable


Complete document sign-up hierarchy2002-02-13/AD Rev.00 AIR STARTER - REPLACEMENT OF MAGNETIC DRAIN PLUG Not Applicable



> CFM56-5B-80-0006/SB*Rev.02

REPLACEMENT OF THE MAGNETIC DRAIN PLUG 572-510-900 WITH MAGNETIC DRAINPLUG 572-8510-9152

Not Applicable

2002-13-03 AD 0 Mandatory COMP INSPECTION OF THE CRITICAL LIFE LIMITED PARTS Open (Next Shop Visit) / SpecialText: DO THE FPI OR ECI AT THENEXT PIECE PART LEVELEXPOSURE FOR THE PARTMENTIONED AT THIS AD

Reference(s) (Document No/Doc-Type/Revision)EASA AD 2002-390-IMP(B) AD 0 (Same header)Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

No limitExp Date Togo---





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18.Sep.2002COMP ENGINE – TURBINE LOW PRESSURE - NEW LPT NOZZLE SEGMENTS STAGE 2 AND

STAGE 3 REWORKSB IAW SB 72-0241.R0 MAY 25, 2000Ex Factory


Complete document sign-up hierarchy2002-16-18/AD Rev.00 ENGINE – TURBINE LOW PRESSURE - NEW LPT NOZZLE SEGMENTS STAGE 2 AND

STAGE 3 REWORKSB IAW SB 72-0241.R0 MAY 25, 2000Ex Factory

> CFM56-5B-72-0328/SB* Rev.3 LPT BEHAVIOUR IMPROVEMENT IN OVERSPEED CONDITION BY INTRODUCTION OFNEW AND REWORKED LPT NOZZLE

Ex Factory

Document-Number Installed in affected Rotable Status> CFM56-7B-72-0241/SB(Rev.: 01 Issued by: CFMI)


2002-390 IMP(B) AD 00 Mandatory01.Aug.2002

COMP INSPECTION OF THE CRITICAL LIFE LIMITED PARTS Open (Next Shop Visit) / SpecialText: This AD must be done at eachpiece-part opportunity duringEngine Shop Visit.

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2002-13-03 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2000-294-IMP(B)/AD Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

No limitExp Date Togo---





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28.Sep.2002COMP LPT NOZZLE SEGMENTS STG 2 AND STG 3 REWORK Ex Factory

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2002-16-18 AD 0O (Same header)Original Document RequirementPerform BEFORE 25000/C

Complete document sign-up hierarchy2002-470/AD Rev.0 LPT NOZZLE SEGMENTS STG 2 AND STG 3 REWORK Ex Factory> CFM56-5B-72-0328/SB* Rev.3 LPT BEHAVIOUR IMPROVEMENT IN OVERSPEED CONDITION BY INTRODUCTION OF

NEW AND REWORKED LPT NOZZLEEx Factory



2003-02-04 AD 0 Mandatory27.Feb.2003

COMP ENGINE INDICATING-EGT HARNESSES AND COUPLINGS Superseded (Superseded)

Replacement InformationThis Document has been SUPERSEDED BY 2007-03-15/AD Rev.0





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14.Jun.2005COMP REMOVING AIR TURBINE STARTERS Not Applicable

Reference(s) (Document No/Doc-Type/Revision)EASA AD F-2003-456 AD 02 (Same header)Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2005-10-05/AD Rev.00 REMOVING AIR TURBINE STARTERS Not Applicable



> CFM56-5B-80-0011/SB*Rev.01

REWORK OF THE AIR TURBINE STARTER Not Applicable

2006-26-01 AD 0 Mandatory03.Jan.2007

COMP ENGINE FUEL FILTER REPLACEMENT. PMA FILTER PROHIBITION Part-Requirem.Contr.

Reason for this StatusAUTO ASSIGNED

2007-0036 AD 01 Mandatory27.Feb.2007

COMP POWER PLANT - FORWARD ENGINE MOUNT BOLTS - INSPECTION/REPLACEMENT/RETORQUE.

Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2007-06-05 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2007-0036-E/AD Rev.00





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27.Aug.2007COMP TRF LIFE LIMIT REDUCTION AND PERIODIC INSPECTION Part-Requirem.Contr.

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2009-18-01 AD 0 (Same header)Original Document RequirementPerform BEFORE 25000/C

Complete document sign-up hierarchy2007-0221/AD Rev.0 TRF LIFE LIMIT REDUCTION AND PERIODIC INSPECTION Part-Requirem.Contr.> CFM56-5B-72-0620/SB*Rev.04

INSPECTION OF TURBINE REAR FRAME ON SAC ENGINES Part-Requirem.Contr.

2007-03-15 AD 0 Mandatory19.Mar.2007

COMP REPLACEMENT OF SUSPECT EGT HARNESS OR EGT COUPLINGS Not Applicable

Reference(s) (Document No/Doc-Type/Revision)EASA AD F-2003-001 AD 3 (Same header)Original Document RequirementPerform BEFORE 3000/H

Complete document sign-up hierarchy2007-03-15/AD Rev.0 REPLACEMENT OF SUSPECT EGT HARNESS OR EGT COUPLINGS Not Applicable



> CFM56-5B-77-0008/SB* Rev.4 INSPECTION OR REPLACEMENT OF SUSPECT WIRING EGT HARNESS Not Applicable

2007-06-05 AD 00 Mandatory COMP POWER PLANT - FORWARD ENGINE MOUNT BOLTS - INSPECTION/REPLACEMENT/RETORQUE.

Not Applicable





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Document-Number Type Rev Compl/Eff Date A|C Subject Status2008-0227-E AD 0 Mandatory

24.Dec.2008COMP HPC INSPECTION/ REPLACEMENT FOR EGT MARGIN DETERIORATION/ STALLS Superseded (Superseded)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2009-01-01 AD 0 (Same header)Replacement InformationThis Document has been SUPERSEDED BY 2008-0228-E/AD Rev.0

2008-0228-E AD 0 Mandatory27.Dec.2008

COMP HPC INSPECTION/REPLACEMENT FOR EGT MARGIN DETERIORATION/STALLS Superseded (Superseded)

Replacement InformationThis Document SUPERSEDES 2008-0227-E/AD Rev.0This Document has been SUPERSEDED BY 2009-0088/AD Rev.0

2009-0088 AD 1 Mandatory08.May.2009

COMP ENGINE – HIGH PRESSURE COMPRESSOR (HPC) – INSPECTION /REPLACEMENTCORRECTED:ON THE 17-TH OF AUGUST 2010

Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2010-09-14 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2009-0088/AD Rev.0Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2009-0088/AD Rev.1 ENGINE – HIGH PRESSURE COMPRESSOR (HPC) – INSPECTION /REPLACEMENT

CORRECTED:ON THE 17-TH OF AUGUST 2010Not Applicable

Replacement InformationThis Document SUPERSEDES 2009-0088/AD Rev.0

> CFM56-5B-73-0229/SB* Rev.1 NEW SOFTWARE VERSION 5.B.R Not ApplicableReason for this StatusDue to higher part number of software is installed.





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08.May.2009COMP ENGINE – HIGH PRESSURE COMPRESSOR (HPC) – INSPECTION /REPLACEMENT Superseded (Superseded)


2009-0110 AD 0 Mandatory21.May.2009

COMP TIME LIMITS - LPT REAR FRAME - LIFE LIMIT / MANDATORY INSPECTION Not Applicable


Complete document sign-up hierarchy2009-0110/AD Rev.0 TIME LIMITS - LPT REAR FRAME - LIFE LIMIT / MANDATORY INSPECTION Not Applicable> CFM56-5B-72-0620_1/SB*Rev.04

INSPECTION OF TURBINE REAR FRAME ON SAC ENGINES Not Applicable

2009-0154-E AD 0 Mandatory17.Jul.2009

COMP HMU INSPECTION AND REPLACEMENT Not Applicable

Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2009-0154-E/AD Rev.0 HMU INSPECTION AND REPLACEMENT Not Applicable> > CFM56-5B-73-0238/SB*Rev.0

HYDROMECHANICAL UNIT VSV/VBV SCORED VALVES Not Applicable



> CFM56-5B-73-0238/SB* Rev.0 HYDROMECHANICAL UNIT VSV/VBV SCORED VALVES Not Applicable





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31.Dec.2009COMP REPLACEMENT OF STAGE 3 LPT DISKS PART NUMBER P/N 336-002-006-0 Not Applicable


Complete document sign-up hierarchy2009-0270/AD Rev.00 REPLACEMENT OF STAGE 3 LPT DISKS PART NUMBER P/N 336-002-006-0 Not Applicable> CFM56-5B-72-0733/SB*Rev.01

SUSPECT ST3 LPT DISK 336-002-006-0 REPLACEMENT Not Applicable



2009-11-02 AD 0 Mandatory23.Jun.2009

COMP CORRECTION - HPC 4-9 SPOOLS REMOVING FROM SERVICE Not Applicable

2009-18-01 AD 00 Mandatory01.Oct.2009

COMP TRF LIFE LIMIT REDUCTION AND PERIODIC INSPECTION Part-Requirem.Contr.

Reference(s) (Document No/Doc-Type/Revision)EASA AD 2007-221EASA AD 2009-110

ADAD

00

(Same header)(Same header)

Original Document RequirementPerform BEFORE 25000/C

Complete document sign-up hierarchy2009-18-01/AD Rev.00 TRF LIFE LIMIT REDUCTION AND PERIODIC INSPECTION Part-Requirem.Contr.> CFM56-5B-72-0620/SB*Rev.04

INSPECTION OF TURBINE REAR FRAME ON SAC ENGINES Part-Requirem.Contr.





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Document-Number Type Rev Compl/Eff Date A|C Subject Status2010-0212 AD 00 Mandatory COMP CFM56-5B ENGINES IF EQUIPPED WITH FAN BLADES SERIAL NUMBERS AS LISTED IN

CFM INTERNATIONAL CFM56-5B S/B 72-0777Not Applicable


Complete document sign-up hierarchy2010-0212/AD Rev.00 CFM56-5B ENGINES IF EQUIPPED WITH FAN BLADES SERIAL NUMBERS AS LISTED IN

CFM INTERNATIONAL CFM56-5B S/B 72-0777Not Applicable

> 72A1035/SB Rev.00 ENGINE - GENERAL - INSPECTION OF CFM56-5B FAN BLADES MID SPAN SHROUD Not Applicable> > CFM56-5B-72-0777/SB*Rev.02

FAN BLADE REPLACEMENT FOR MID SPAN SHROUD NON CONFORMING CONTOUR Not Applicable

2010-13-09 AD 00 Mandatory26.Jul.2010

COMP CFMINTERNATIONAL CFM56-5,-5B,AND-7B SERIES TURBOFAN ENGINES WITH STAGE3 LPT DISKS PART NUMBER P/N 336-002-006-0

Not Applicable


Complete document sign-up hierarchy2010-13-09/AD Rev.00 CFMINTERNATIONAL CFM56-5,-5B,AND-7B SERIES TURBOFAN ENGINES WITH STAGE

3 LPT DISKS PART NUMBER P/N 336-002-006-0Not Applicable

> CFM56-5B-72-0733/SB*Rev.01

SUSPECT ST3 LPT DISK 336-002-006-0 REPLACEMENT Not Applicable







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23.Jul.2012COMP ENGINE FUEL AND CONTROL – HYDRO-MECHANICAL UNITS – OPERATIONAL

LIMITATION.Superseded (Part-Requirem.Contr.)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2013-14-06 AD 00 (Same header)Replacement InformationThis Document has been SUPERSEDED BY 2017-0065/AD Rev.00Original Document RequirementPerform WITHIN 10000/H (effective from Effective Date 23.Jul.2012) for the first timeThereafter perform in an interval of 10000/H

Complete document sign-up hierarchy2012-0123/AD Rev.00 ENGINE FUEL AND CONTROL – HYDRO-MECHANICAL UNITS – OPERATIONAL

LIMITATION.Part-Requirem.Contr.




> CFM56-5B-73-0122/SB*Rev.12

USE OF CIS FUELS IN CFM56-5B ENGINES Part-Requirem.Contr.






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15.Mar.2012COMP FAN BLADE REPLACEMENT FOR MID SPAN SHROUD NON CONFORMING CONTOUR Not Applicable


Complete document sign-up hierarchy2012-02-03/AD Rev.00 FAN BLADE REPLACEMENT FOR MID SPAN SHROUD NON CONFORMING CONTOUR Not Applicable> CFM56-5B-72-0777/SB*Rev.02

FAN BLADE REPLACEMENT FOR MID SPAN SHROUD NON CONFORMING CONTOUR Not Applicable

2013-0050 AD 00 Mandatory19.Mar.2013

COMP POWERPLANT – CFM56-5/-5B – AFT ENGINE MOUNT RETAINERS – INSPECTION/REPLACEMENT.

Superseded (Not Applicable)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2014-14-06 AD 00 (Same header)Replacement InformationThis Document has been SUPERSEDED BY 2015-0021/AD Rev.00

Complete document sign-up hierarchy2013-0050/AD Rev.00 POWERPLANT – CFM56-5/-5B – AFT ENGINE MOUNT RETAINERS – INSPECTION/

REPLACEMENT.Not Applicable


> > RA32071-146/SB* Rev.02 NACELLE - ENGINE MOUNT INSPECTION OF AFT ENGINE MOUNT RETAINER Not ApplicableReason for this Statuscomplied with by previous operator





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03.Sep.2013COMP CLEANING, INSPECTION, AND REPAIR OF HMU CAUSED BY EXPOSURE TO TYPE TS-1

FUELPart-Requirem.Contr.

Reference(s) (Document No/Doc-Type/Revision)EASA AD 2012-0123EASA AD 2017-0065

ADAD

0000


Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2013-14-06/AD Rev.00 CLEANING, INSPECTION, AND REPAIR OF HMU CAUSED BY EXPOSURE TO TYPE TS-1

FUELPart-Requirem.Contr.



> CFM56-5B-73-0122/SB*Rev.12

USE OF CIS FUELS IN CFM56-5B ENGINES Part-Requirem.Contr.


2014-0130 AD 00 Mandatory03.Jun.2014

COMP ENGINE STATIONARY PARTS – LIFE LIMITS / MANDATORY INSPECTIONS Not Applicable

Reason for this StatusDue to AD 2014-130 requirements and in according with ESM CFM56-5B (TR) 05-0223 Item05-12-04 Stationary Life Limit Parts is identified as N/L (Not Limit)





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27.Aug.2014COMP REPETITIVE INSPECTION AND RETAINER REPLACEMENT FOR DULL FINISH

RETAINERSNot Applicable


Complete document sign-up hierarchy2014-14-06/AD Rev.00 REPETITIVE INSPECTION AND RETAINER REPLACEMENT FOR DULL FINISH

RETAINERSNot Applicable


2015-0021 AD 00 Recommended27.Feb.2015

COMP POWERPLANT – AFT ENGINE MOUNT RETAINERS – INSPECTION / REPLACEMENT. Superseded (Not Applicable)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2014-14-06 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2013-0050/AD Rev.00This Document has been SUPERSEDED BY 2016-0010/AD Rev.01Original Document RequirementPerform within an unlimited threshold.

Complete document sign-up hierarchy2015-0021/AD Rev.00 POWERPLANT – AFT ENGINE MOUNT RETAINERS – INSPECTION / REPLACEMENT. Not Applicable

Replacement InformationThis Document SUPERSEDES 2013-0050/AD Rev.00This Document has been SUPERSEDED BY 2016-0010/AD Rev.01






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18.Mar.2015COMP POWERPLANT – FORWARD ENGINE MOUNT – INSPECTION. Superseded (Superseded)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2016-09-06 AD 00 (Same header)Replacement InformationThis Document has been SUPERSEDED BY 2017-0231/AD Rev.00

2016-0010 AD 01 Mandatory27.Jan.2016

COMP POWERPLANT – AFT ENGINE MOUNT RETAINERS – INSPECTION / REPLACEMENT Superseded (Repetitive)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2016-14-09 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2015-0021/AD Rev.00This Document has been SUPERSEDED BY 2017-0138/AD Rev.00Original Document RequirementPerform in an interval of 2/MT

Complete document sign-up hierarchy2016-0010/AD Rev.01 POWERPLANT – AFT ENGINE MOUNT RETAINERS – INSPECTION / REPLACEMENT Repetitive


> > RA32071-160/SB* Rev.01 REPETITIVE INSPECTION OF AFT ENGINE MOUNT INNER RETAINER RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

15.Dec.2020Perform initially before(F) 24.Nov.2015 /Interval(F):365/D

Exp Date Togo15.Dec.2020 242d, 15hPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O Remarks16.Dec.2019 39224:03/H 20'003/C 506065678 Was due at: 17.Feb.2020 PerfRev.:'01'

> > > RA32071-165/SB* Rev.00 NACELLE - ENGINE MOUNT - INSPECTION OF AFT ENGINE MOUNT INNER RETAINER Not Applicable





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01.Mar.2016COMP LOW PRESSURE TURBINE REAR FRAMES – INSPECTION / REPLACEMENT Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2016-02-04 AD 00 (Same header)Original Document RequirementPerform in an interval of 32000/C

Complete document sign-up hierarchy2016-0039/AD Rev.00 LOW PRESSURE TURBINE REAR FRAMES – INSPECTION / REPLACEMENT Not Applicable> CFM56-5B-72-0850/SB*Rev.01

INSPECTION OF TURBINE REAR FRAME ON CFM56-5B ENGINES Not Applicable

2016-02-04 AD 00 Mandatory COMP TURBINE REAR FRAME CFM56-5B ENGINES INSPECTION Not ApplicableReference(s) (Document No/Doc-Type/Revision)EASA AD 2016-0039 AD 00 (Same header)

Complete document sign-up hierarchy2016-02-04/AD Rev.00 TURBINE REAR FRAME CFM56-5B ENGINES INSPECTION Not Applicable> CFM56-5B-72-0850/SB*Rev.01

INSPECTION OF TURBINE REAR FRAME ON CFM56-5B ENGINES Not Applicable

2016-09-06 AD 00 Mandatory06.Jun.2016

COMP POWERPLANT – FORWARD ENGINE MOUNT – INSPECTION. Part-Requirem.Contr.

Reference(s) (Document No/Doc-Type/Revision)2015-0038 AD 01Replacement InformationThis Document terminates 2015-05-02/AD Rev.00Reason for this StatusAUTO ASSIGNED





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03.May.2017COMP HYDRO-MECHANICAL UNITS – OPERATIONAL LIMITATIONS Part-Requirem.Contr. / Special

Text: HMU has not to be exceeded10 000 engine hours since firstinstallation on an engine, or sincelast HMU overhaul, or since lastdelta-P valve replacement of theaffected HMU

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2013-14-06 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2012-0123/AD Rev.00

Complete document sign-up hierarchy2017-0065/AD Rev.00 HYDRO-MECHANICAL UNITS – OPERATIONAL LIMITATIONS Part-Requirem.Contr. / Special Text:

HMU has not to be exceeded 10 000engine hours since first installation onan engine, or since last HMU overhaul,or since last delta-P valve replacementof the affected HMU




> CFM56-5B-73-0122/SB*Rev.12

USE OF CIS FUELS IN CFM56-5B ENGINES Repetetive (Part-Requirem.Contr.)





17.Apr.2020Page 25/35

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O 506420843

RemarksHMU P/N 8061-536 S/N WYGB0055 installed.02.Aug.2019 37797:00/H 19'686/C

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of DocumentInterval(F):10'000/H

Exp Date TogoNo Limit 7271:42/H

47797:00/H

Wasim.Akhtar

Highlight

Please update the compliance and next due section as per the ajw comments in ajw open items list. Please add HMU PN & SN as well

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26.May.2017COMP RADIAL DRIVE SHAFT – REPLACEMENT Not Applicable


Complete document sign-up hierarchy2017-0084/AD Rev.00 RADIAL DRIVE SHAFT – REPLACEMENT Not Applicable> CFM56-5B-72-0934/SB*Rev.01

TGB ASSY - REPLACEMENT OF SUSPECTED BATCH OF RDS ASSY AND ASSOCIATEDRADIAL DRIVE SHAFT OUTER HOUSING

Not Applicable by Serial Number





17.Apr.2020Page 26/35

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10.Aug.2017COMP FORWARD ENGINE MOUNT MAIN BEAM SNOUT – REPLACEMENT Open


Complete document sign-up hierarchy2017-0132/AD Rev.01 FORWARD ENGINE MOUNT MAIN BEAM SNOUT – REPLACEMENT Open> > > RA32071-159/SB* Rev.00 BEARING ASSEMBLY, FORWARD ENGINE MOUNT INSPECTION AND REWORK OF

BEAM SNOUTOpen

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

10.Nov.2020 44720:00/H 25'206/CPerform initially within (effective fromEffective Date 01.Dec.2016) (F) 15000/H or10000/C or 1440/D

Exp Date Togo10.Nov.2020 207d, 15h

> RA32071-159/SB* Rev.00 BEARING ASSEMBLY, FORWARD ENGINE MOUNT INSPECTION AND REWORK OFBEAM SNOUT

Open


10.Nov.2020 44720:00/H 25'206/CPerform initially within (effective fromEffective Date 01.Dec.2016) (F) 15000/H or10000/C or 1440/D

Exp Date Togo10.Nov.2020 207d, 15h





17.Apr.2020Page 27/35

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16.Aug.2017COMP AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Superseded (Open)

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2017-04-10 AD 00 (Same header)Replacement InformationThis Document SUPERSEDES 2016-0010/AD Rev.01This Document has been SUPERSEDED BY 2017-0251/AD Rev.00

Complete document sign-up hierarchy2017-0138/AD Rev.00 AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Open





> > > RA32071-165/SB* Rev.00 NACELLE - ENGINE MOUNT - INSPECTION OF AFT ENGINE MOUNT INNER RETAINER Not Applicable> > RA32071-164/SB* Rev.01 INTRODUCTION OF AN IMPROVED AFT ENGINE MOUNT RETAINER ASSEMBLY Open


06.Oct.2020Perform initially within (effective fromEffective Date 06.Oct.2016) (F) 48/MT

Exp Date Togo06.Oct.2020 172d, 15h






17.Apr.2020Page 28/35

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29.Dec.2017COMP AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Open

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2017-04-10FAA AD 2018-16-02

ADAD

0000



Complete document sign-up hierarchy2017-0251/AD Rev.00 AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Open





> > > RA32071-165/SB* Rev.00 NACELLE - ENGINE MOUNT - INSPECTION OF AFT ENGINE MOUNT INNER RETAINER Not Applicable> > RA32071-164/SB* Rev.01 INTRODUCTION OF AN IMPROVED AFT ENGINE MOUNT RETAINER ASSEMBLY Open


06.Oct.2020Perform initially within (effective fromEffective Date 06.Oct.2016) (F) 48/MT

Exp Date Togo06.Oct.2020 172d, 15h






17.Apr.2020Page 29/35

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16.Aug.2017COMP AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Not Applicable


Complete document sign-up hierarchy2017-04-10/AD Rev.00 AFT ENGINE MOUNTS RETAINERS – INSPECTION / REPLACEMENT Not Applicable> > > RA32071-165/SB* Rev.00 NACELLE - ENGINE MOUNT - INSPECTION OF AFT ENGINE MOUNT INNER RETAINER Not Applicable

2017-05-09 AD 00 Mandatory13.Apr.2017

COMP REMOVAL OF THE RADIAL DRIVE SHAFT (RDS) ASSEMBLY AND THE RDS OUTERHOUSING

Not Applicable


Complete document sign-up hierarchy2017-05-09/AD Rev.00 REMOVAL OF THE RADIAL DRIVE SHAFT (RDS) ASSEMBLY AND THE RDS OUTER

HOUSINGNot Applicable

> CFM56-5B-72-0934/SB*Rev.01

TGB ASSY - REPLACEMENT OF SUSPECTED BATCH OF RDS ASSY AND ASSOCIATEDRADIAL DRIVE SHAFT OUTER HOUSING

Not Applicable by Serial Number





17.Apr.2020Page 30/35

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28.Jun.2019COMP CFM56 - REPLACEMENT OF THE AFFECTED ROTATING AIR HPT FRONT SEAL WITH A

PART ELIGIBLE FOR INSTALLATION.Superseded (Not Applicable)

Reference(s) (Document No/Doc-Type/Revision)2019-12-05 AD 00Replacement InformationThis Document has been SUPERSEDED BY 2019-0150/AD Rev.00

Complete document sign-up hierarchy2019-0146/AD Rev.00 CFM56 - REPLACEMENT OF THE AFFECTED ROTATING AIR HPT FRONT SEAL WITH A

PART ELIGIBLE FOR INSTALLATION.Not Applicable


> CFM56-5B-72-1074/SB*Rev.02

REPLACEMENT OF ROTATING AIR HPT FRONT SEAL P/N 1795M36P02 Not Applicable

Document-Number Installed in affected Rotable Status> > EODCFM56-7B-72-1042/EOD(Rev.: 0 Issued by: SDMEDRE)






17.Apr.2020Page 31/35

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05.Jul.2019COMP CFM56 - REPLACEMENT OF THE AFFECTED ROTATING AIR HPT FRONT SEAL WITH A

PART ELIGIBLE FOR INSTALLATION.Superseded (Not Applicable)

Reference(s) (Document No/Doc-Type/Revision)2019-12-05 AD 00Replacement InformationThis Document SUPERSEDES 2019-0146/AD Rev.00This Document has been SUPERSEDED BY 2020-0007/AD Rev.00Original Document RequirementPerform within an unlimited threshold.




> CFM56-5B-72-1074/SB*Rev.02








17.Apr.2020Page 32/35

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29.Jan.2020COMP CFM56 - REPLACEMENT OF THE AFFECTED ROTATING AIR HPT FRONT SEAL WITH A






> CFM56-5B-72-1074/SB*Rev.02




2020-0044 AD 00 Mandatory17.Mar.2020

COMP CFM56 - HIGH-PRESSURE TURBINE INNER STATIONARY SEAL – INSPECTION Not Applicable

Original Document RequirementPerform within an unlimited interval.

Complete document sign-up hierarchy2020-0044/AD Rev.00 CFM56 - HIGH-PRESSURE TURBINE INNER STATIONARY SEAL – INSPECTION Not Applicable> CFM56-5B-72-0952/SB*Rev.00

REPAIR OF HPT INNER STATIONARY SEAL HONEYCOMB Not Applicable

Document-Number Installed in affected Rotable Status> >EODCFM56-7B-72-1054/EOD (Rev.: 0 Issued by:SDM EDRE)






17.Apr.2020Page 33/35

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Document-Number Type Rev Compl/Eff Date A|C Subject StatusF-2003-001 AD 02 Mandatory

18.Jan.2003COMP ENGINE INDICATING - EGT HARNESSES AND COUPLINGS Not Applicable

Reference(s) (Document No/Doc-Type/Revision)FAA AD 2007-03-15 AD 00 (Same header)Original Document RequirementPerform WITHIN 500/H (effective from Effective Date 18.Jan.2003)

Complete document sign-up hierarchyF-2003-001/AD Rev.02 ENGINE INDICATING - EGT HARNESSES AND COUPLINGS Not Applicable



> CFM56-5B-77-0008/SB* Rev.4 INSPECTION OR REPLACEMENT OF SUSPECT WIRING EGT HARNESS Not Applicable

F-2003-403 AD 1 Mandatory06.Dec.2003

COMP REWORK OF THE AIR TURBINE STARTER Superseded (Superseded)

Replacement InformationThis Document has been SUPERSEDED BY F-2003-422/AD Rev.0

F-2003-403 AD 0 Mandatory08.Nov.2003

COMP REWORK OF THE AIR TURBINE STARTER Cancelled (Cancelled)

Replacement InformationThis Document has been CANCELLED BY F-2003-403/AD Rev.1

F-2003-422 AD 1 Mandatory24.Dec.2003

COMP REWORK OF AIR TURBINE STARTER Superseded (Superseded)

Replacement InformationThis Document has been SUPERSEDED BY F-2003-456/AD Rev.02





17.Apr.2020Page 34/35

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Document-Number Type Rev Compl/Eff Date A|C Subject StatusF-2003-422 AD 0 Mandatory

06.Dec.2003COMP REWORK OF THE AIR TURBINE STARTER Cancelled (Cancelled)

Replacement InformationThis Document has been CANCELLED BY F-2003-422/AD Rev.1

F-2003-456 AD 02 Mandatory09.Oct.2004

COMP REWORK OF THE AIR TURBINE STARTER Not Applicable


Complete document sign-up hierarchyF-2003-456/AD Rev.02 REWORK OF THE AIR TURBINE STARTER Not Applicable



> CFM56-5B-80-0011/SB*Rev.01

REWORK OF THE AIR TURBINE STARTER Not Applicable





17.Apr.2020Page 35/35

01.05.2020Anton VlasovPowerplant Engineer"Rossiya Airlines" JSC

06.07.2020 40525 FH ENG CSN: 20557 FC

SECTIONTASK

NUMBERDESCRIPTION

TASK CODE

AIRBUSTHRESHOLD

AIRBUSINTERVAL

REFERENCE Last Done DateEngine TSN @

Last DoneEngine CSN @

Last DoneAPPLICABILITY

2-20 200435-01-1 FAN COMPARTMENT

DETAILED INSPECTION OF EWIS IN THE FAN AND ACCESSORY GEAR BOX (EWIS)

DET 24 MO 249200-220-003 01 MAR 2019 35968 18571 CEO

2-20 200453-01-1 CORE COMPARTMENT

DETAILED INSPECTION OF EWIS INSTALLED IN THE HOT SECTION (EWIS)

DET 24 MO 249200-220-004 01 MAR 2019 35968 18571 CEO

2-24 242000-21-1 AC GENERATION

- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER ELEMENTS,- DRAIN AND REPLENISH OIL SYSTEM

NOTE:INTERVAL:- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY INTO SERVICE. THEREAFTER REFER TO INTERVAL.

DIS 6 MOOR800 FHNOTE

242100-920-040 N/A CFM56-5POST 30352

2-24 242100-01-1 INTEGRATED DRIVE GENERATOR

CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION BOLT

FNC 24 MOOR2400 FH

242100-210-043 18 APR 2020 40525 20557 CFM56-5


CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE INDICATOR

NOTE:DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.

SVC 2 MOOR300 FHNOTE

242100-210-046 20 MAR 2020 300 FH to go CFM56-5


- REMOVE AND DISCARD SCAVENGE FILTER ELEMENT- DRAIN AND REPLENISH OIL SYSTEM

NOTE:INTERVAL:- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT DELIVERY. THEREAFTER REFER TO INTERVAL.

DIS 6 MOOR800 FHNOTE

242100-920-040 13 FEB 2020 547 FH to go CFM56-5PRE 30352


OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG) DISCONNECT AND RECONNECT FUNCTION.

NOTE:TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.

OPC NOTE 242100-710-040 18 APR 2020 40525 20557 CFM56-5


REMOVE IDG COOLER FOR IN-SHOP CLEANING

NOTE:INTERVAL:- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE SHOP VISIT.

RST 252 MOOR36000 FHNOTE

731160-100-040 22 FEB 2016 28067 14125 CFM56-5

2-26 261200-01-1 ENGINE FIRE AND OVERHEAT DETECTION

OPERATIONAL CHECK OF LOOP/SQUIB

OPC 12 MOOR1000 FH

261200-710-001 10 FEB 2020 39913 20289 ALL

ESN575355 CFM56 ENGINE MPD TASK LIST

As of DATE: ENG TSN:

Printed 06.07.2020 CFM56-5B - Engine MPD Tasks Page 1 of 5

SECTIONTASK

NUMBERDESCRIPTION

TASK CODE

AIRBUSTHRESHOLD

AIRBUSINTERVAL




2-29 290000-01-1 HYDRAULIC POWER

CHECK CLOGGING INDICATORS OF THE FOLLOWING FILTERS (POP OUT NOT PROTRUDING)- HIGH PRESSURE DELIVERY- GROUND SERVICING (RESERVOIR FILLING)- RETURN (LOW PRESSURE)- HIGH PRESSURE BLEED AIR- LOW PRESSURE BLEED AIR- CASE DRAIN

VCK 12 MOOR1000 FH

291000-200-004 N/Adue to SDM fleet is post 25365 mod

A320PRE 25365 (29-1076)ORA321PRE 25365 (29-1076)


DETAILED INSPECTION OF HYDRAULIC PRESSURE SWITCH LINE (P/N 642-5658-501/505) FOR CLAMP CHAFING DAMAGE AND PRELOAD CONDITION

DET 600 FH 2400 FH 291000-200-009VSB RA320 029-9

N/A due to ESN575355 is post-VSB RA32029-13

CFM56-5BPRE 24387 P6969PRE SB 71-1023


CHECK CLOGGING INDICATORS OF THE FOLLOWING FILTERS (POP OUT NOT PROTRUDING)- HIGH PRESSURE DELIVERY- GROUND SERVICING (RESERVOIR FILLING)- RETURN (LOW PRESSURE)- HIGH PRESSURE BLEED AIR- LOW PRESSURE BLEED AIR- WATER SEPARATOR- CASE DRAIN

VCK 24 MOOR2000 FH

291000-210-002 18 MAR 2020 40357 20481 A318ORA319ORA320POST 25365 (29-1076)ORA321POST 25365 (29-1076)

2-30 302149-C1-1 ENGINE AIR INTAKE ICE PROTECTION

DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY DUCTS AND ASSOCIATED HARDWARE IN THE CORE AND FAN COMPARTMENTS.

DET 108 MOOR12000 FH

302149-200-001 22 FEB 2016 28067 14125 CFM56-5

2-36 361100-01-1 ENGINE BLEED AIR SUPPLY SYSTEM

FUNCTIONAL CHECK OF OVERPRESSURE VALVE

FNC 60 MOOR22000 FH

361153-720-001 21 FEB 2017 as per Air Cote D'Ivoire MPD task status

as per Air Cote D'Ivoire MPD task status

CEO

2-36 361141-03-1 IP BLEED CHECK VALVE

CHECK OF IP BLEED CHECK VALVE FOR CONDITION

DET 72 MOOR7500 FH

361141-200-001 10 FEB 2020 39913 20289 CFM56-5

2-36 361143-01-1 THERMOSTAT - FAN AIR VALVE CONTROL

REMOVE THE THERMOSTAT-FILTER OF THE FAN AIR VALVE-CONTROL FOR CLEANING.

NOTE:DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.

RST 72 MOOR6000 FHNOTE

361143-100-001 08 OCT 2019 38504 19700 CEO

3-71 712111-01-1 FORWARD ENGINE MOUNT

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION

DET 2200 FCOR4500 FH

2200 FCOR4500 FH

712111-210-040 01 AUG 2019 37796 19418 A318-PAXCFM56-5ORA319-PAXCFM56-5ORA320CFM56-5


DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION

DET 800 FCOR1600 FH

800 FCOR1600 FH

712111-210-040 N/A due to A/C type applicability (ESN575355 was used for operation on A319 only)

A321CFM56-5


DETAILED INSPECTION OF DISASSEMBLED FORWARD ENGINE MOUNT INSTALLATION INCLUDING MATING SURFACES.

NOTE:ACCOMPLISHMENT OF THIS INSPECTION TO BE PERFORMED WITH A MAXIMUM INTERVAL OF 12 YEARS BETWEEN MOUNT DISASSEMBLY

DET 12 YE 12 YENOTE

712111-210-042 22 FEB 2016 28067 14125 CFM56-5


SECTIONTASK

NUMBERDESCRIPTION

TASK CODE

AIRBUSTHRESHOLD

AIRBUSINTERVAL





SPECIAL DETAILED INSPECTION (TC) OF FORWARD ENGINE MOUNT PYLON BOLTS

SDI 7500 FCOR15000 FH

7500 FCOR15000 FH

712111-210-803 22 NOV 2018 34977 18130 A318-PAXCFM56-5ORA319-PAXCFM56-5ORA320CFM56-5ORA321CFM56-5


SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FORWARD ENGINE MOUNT LINK LUGS


7500 FCOR15000 FH

712112-200-803 22 FEB 2016 28067 14125 A318-PAXCFM56-5ORA319-PAXCFM56-5ORA320CFM56-5ORA321CFM56-5

3-71 712211-01-1 AFT ENGINE MOUNT

DETAILED INSPECTION OF DISASSEMBLED AFT ENGINE MOUNT INSTALLATION INCLUDING MATING SURFACES.

NOTE:ACCOMPLISHMENT OF THIS INSPECTION TO BE PERFORMED WITH A MAXIMUM INTERVAL OF 12 YEARS BETWEEN MOUNT DISASSEMBLY

DET 12 YE 12 YENOTE

712211-210-040 22 FEB 2016 28067 14125 CFM56-5


DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION

DET 7500 FCOR15000 FH

7500 FCOR15000 FH



SPECIAL DETAILED INSPECTION (TC) OF AFT ENGINE MOUNT PYLON BOLTS


7500 FCOR15000 FH

712211-210-803 22 NOV 2018 34977 18130 A318-PAXCFM56-5ORA319-PAXCFM56-5ORA320CFM56-5ORA321CFM56-5


SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT LINK LUGS


7500 FCOR15000 FH



SECTIONTASK

NUMBERDESCRIPTION

TASK CODE

AIRBUSTHRESHOLD

AIRBUSINTERVAL





SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF AFT ENGINE MOUNT PINS


7500 FCOR15000 FH


2-72 722000-C1-1 FAN SECTION

DETAILED INSPECTION OF SPINER, ENGINE INLET, FAN BLADES, FAN OUTLET AND ABRADABLE MATERIAL.

NOTE:INTERVAL:- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL INTERVAL MAY BE USED.

DET 24 MOOR2000 FCNOTE

722300-210-003 01 AUG 2019 37796 19418 CFM56-5

2-72 722000-C3-1 FAN SECTION

DETAILED INSPECTION AND RELUBRICATION OF FAN BLADE DOVETAILS, MIDSPAN SHROUDS, SPACERS, PLATFORMS AND FAN DISK DOVETAIL SLOTS.

DET 3000 FC 722100-210-804 16 DEC 2019 39224 20003 CFM56-5B

2-72 724000-C1-1 COMBUSTION SECTION

BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINERS, DOME AREAS, HPT NOZZLE VANES AND SHROUDS (AS FAR AS VISIBLE THROUGH TWO OPPOSITE PORTS)

SDI 36 MOOR1600 FC

724100-290-001 25 JUN 2020 40525 20557 CFM56-5

2-72 725000-C1-3 TURBINE SECTION

BORESCOPE INSPECTION OF HPT BLADES (FROM THE FRONT AND THE REAR)

SDI 24 MOOR1600 FC

725200-290-001 25 JUN 2020 40525 20557 CFM56-5B

2-72 725000-C6-1 TURBINE SECTION

SURVEILLANCE INSPECTION OF TURBINE FRAME AFT ENGINE MOUNT LUGS

NOTE:INTERVAL:- TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE SHOP VISIT.

DET 36000 FHNOTE

712212-210-001 22 FEB 2016 28067 14125 CFM56-5

2-73 730000-C3-1 ENGINE FUEL & CONTROL-GENERAL

READ ENGINE SCHEDULED MAINTENANCE REPORT (SMR) FOR UNLIMITED (ASTERISKED) FAULTS.

OPC 1200 FH 732160-740-029 N/A due to Engine FADEC STD 5B.T.F1

CFM56-5B(DAC)FADEC STD 5DD TO 5DLORCFM56-5B(SAC)FADEC STD 5BE TO 5BHORCFM56-5AFADEC STD 5AD 5AD, 5AE TO 5AH

2-73 730000-C4-1 ENGINE FUEL AND CONTROL

REMOVE, INSPECT AND REPLACE FUEL FILTER ELEMENT

DIS 36 MOOR4000 FH

731110-920-001 10 FEB 2020 39913 20289 CFM56-5

2-78 781112-C1-1 CENTERBODY

DETAILED INSPECTION OF THE EXHAUST CENTERBODY

NOTE:PLANNING:- CENTERBODY WITH P/N 238-0451-511, 238-0451-513 AND 238-0451-523 DO NOT REQUIRE INSPECTION.

DET 3000 FH 781112-210-041VSB RA32078-65

N/A due to P/N installed (238-0451-513)

CFM56-5WITH EITHER OF CENTERBODY P/N 238-0451-7R, 238-0451-9R, 238-0451-517 NOTE


SECTIONTASK

NUMBERDESCRIPTION

TASK CODE

AIRBUSTHRESHOLD

AIRBUSINTERVAL




2-78 781112-C1-2 CENTERBODY

DETAILED INSPECTION OF THE EXHAUST CENTERBODY

NOTE:INTERVAL:- CENTERBODY WITH P/N 238-0451-505, 238-0451-515, 238-0451-519 AND 238-0451-521 CAN BE INSPECTED EVERY 3000 FH IF A REINFORCEMENT DOUBLER HAS BEEN INSTALLED (POST VSB RA32078-65).

DET 400 FHNOTE

781112-210-041VSB RA32078-65

N/A due to P/N installed (238-0451-513)

CFM56-5WITH EITHER OF CENTERBODY P/N 238-0451-505, 238-0451-507, 238-0451-509, 238-0451-515, 238-0451-519, 238-0451-521, NOTE

2-79 792000-C4-2 DISTRIBUTION

REMOVE AND DISCARD SUPPLY FILTER

DIS 36 MOOR4000 FH

792110-920-002 10 FEB 2020 39913 20289 CFM56-5B


CHECK OF FWD SUMP, AFT SUMP, AGB, AND TGB SCAVENGE SCREENS

DET 36 MOOR4000 FH

790000-281-003 01 AUG 2019 37796 19418 CFM56-5B


CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES

DET 12 MOOR1000 FH

790000-281-002 27 FEB 2020 40103 20371 CFM56-5B


OPERATIONAL CHECK OF THE MASTER CHIP DETECTOR REMOTE INDICATION

OPC 36 MOOR3000 FH

790000-200-001 01 AUG 2019 37796 19418 CFM56-5B

2-80 801110-C1-1 STARTER

CHECK CHIP DETECTOR

DET 12 MOOR1000 FH

801110-210-001 27 FEB 2020 40103 20371 CFM56-5

2-80 801110-C2-1 STARTER

REPLENISH OIL SYSTEM

SVC 6 MOOR600 FH

121380-610-002 27 FEB 2020 40103 20371 CFM56-5

2-80 801110-C3-1 STARTER

DRAIN AND REPLENISH OIL SYSTEM

SVC 12 MOOR1200 FH

121380-610-001 11 MAR 2020 40280 20447 CFM56-5

4-ZL-400 ZL-435-01-1 FAN AND ACCESSORY GEAR BOX

GENERAL VISUAL INSPECTION OF FAN AND ACCESSORY GEAR BOX (EWIS)

GVI 12 MO 052430-200-002 07 OCT 2019 38504 19700 CFM56-5

4-ZL-400 ZL-453-01-1 HOT SECTION

GENERAL VISUAL INSPECTION OF HOT SECTION (EWIS)

GVI 24 MO 052450-200-002 01 MAR 2019 35968 18571 CFM56-5

Anton VlasovPowerplant Engineer


Documents

ENGINE MINI PACK - AJW Group