# CFM International CFM56-5A series

- Type: Engine model (FAA registry)
- Registry code: 13170
- Manufacturer (registry): CFM INTL
- Model: CFM56-5A
- Engine type: Turbo-fan
- Power: 25,000 lb thrust
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/cfm-international-cfm56-5a-series

The registry names only the engine series, so ADs for every model in the series are matched.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 2002
- [AD 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-18-16](https://openairdocs.org/ad/96-18-16): Low Pressure Turbine Rotor (LPTR) Stub Shaft And Conical Support · CFM International CFM56-2, CFM56-2A, CFM56-2B and 9 more. Effective Dec 9, 1996

## Information bulletins (advisory) (7)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (109, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR DALA2015032502377](https://openairdocs.org/sdr/DALA2015032502377), Mar 24, 2015: PROFILE. CRACKED. DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES 843 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 5
- [SDR CA140627005](https://openairdocs.org/sdr/CA140627005), Jun 20, 2014: MECHANISM. MISMANUFACTURED. (CAN) GIRT BAR TRIGGER POSITION REF F, TRIGGER DEVIATIONS FROM DWG REF G, SB A320-53-1289, REF H, GIRT BAR ATTACHMENT FITTING CONFIGURATION REF I, GIRT BAR EXPL
- [SDR CA140611004](https://openairdocs.org/sdr/CA140611004), Jun 11, 2014: SMOKE DETECTOR. FAILED. (CAN) FLIGHT REPORTED AN "AVIONICS SMOKE ECAM" MESSAGE WITH SMOKE NOT VISUALLY CONFIRMED AND COULD NOT DETERMINE IF WARNING WAS VALID. CREW ELECTED TO DO A PREC
- [SDR SOKF20140114001](https://openairdocs.org/sdr/SOKF20140114001), Jan 13, 2014: INTERFACE UNIT. FAULTY. DURING TAKEOFF AT MROC THE LG DID NOT RETRACT & LG DOORS DID NOT CLOSE CORRECTLY. LG LGCIU 1 FAULT & LG SYS DISAGREE APPEARED ON ECAM. R & R LGCIU IAW AMM 32-41
- [SDR CA111019014](https://openairdocs.org/sdr/CA111019014), Oct 14, 2011: B-NUT. FAILED. (CAN) CREW ADVISED FLIGHT DISPATCH THAT THEY HAD A "YELLOW HYDRAULIC" FAILURE AND REQUIRED A PATCH TO MOC. PATCH WAS COMPLETED, FLIGHT CONTINUED, ATC WAS ADVISE
- [SDR CA110926002](https://openairdocs.org/sdr/CA110926002), Sep 24, 2011: COMPUTER. FAILED. (CAN) AFTER TAKEOFF CREW RECEIVED SMOKE INIDICATION IN AVIONICS BAY. FLIGHT DECLARED EMERGENCY RETURNED AND LANDED OVERWEIGHT. NO SMOKE OR ODOR FOUND DURING INV
- [SDR CA110725001](https://openairdocs.org/sdr/CA110725001), Jul 22, 2011: ADIRU. FAILED. ACFT WAS DISPATCHED WITH NR 3 ADR INOPERATIVE. AFTER DEPARTURE IN THE CLIMB, THE FLIGHT EXPERIENCED A FAILURE OF THE NR1 ADR AND ELECTED TO RETURN. NO EMERGENCY
- [SDR DALA1100083131](https://openairdocs.org/sdr/DALA1100083131), Jan 1, 2011: WIRE. SHORTED. DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 2A INOPERATIVE. MX RECONNECTED SHORTED WIRE AT SEAT AND PERFORMED FUNCTIONAL CHECK. CHECK WAS
- [SDR CA110104001](https://openairdocs.org/sdr/CA110104001), Jan 1, 2011: IDG. FAILED. DURING CRUISE ELECTRICAL TRANSIENT OCCURRED CAUSING LOSS OF FAC NR 1, ALL DISPLAYS EXCEPT F/O PFD WAS LOST FOR ABOUT 5 SECONDS. TSM 24-20-00-810-806/814 CARRIED
- [SDR DALAFAR145SDR104](https://openairdocs.org/sdr/DALAFAR145SDR104), Nov 19, 2010: NUT. MISSING. UPON DISASSEMBLY OF THE ROTOR STACK, SHOP NOTICED 48 NUTS OUT OF 60 MISSING FROM THE STACK WHICH HOLDS THE LLPS TOGETHER. THE LLPS AND HARDWARE INVOLVED ARE AS 
- [SDR F3LA2010110800535](https://openairdocs.org/sdr/F3LA2010110800535), Nov 3, 2010: THERMOSTAT. DEFECTIVE. LOST BLEED NR1 AT 36,000 CAUSING CABIN PRESSURE EXCESS CABIN ALTITUDE. EMERGENCY WAS DECLARE AND DECENTED TO 10,000. FOUND THERMOSTAT DEFECTIVE, R & R THE THERM
- [SDR DALA1026593120](https://openairdocs.org/sdr/DALA1026593120), Oct 13, 2010: LIGHT. INOPERATIVE. DURING A NON-ROUTINE CHECK, FOUND 1B EMERGENCY LIGHT INOPERATIVE. MAINT REPLACED 2 EMERGENCY LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVIC
- [SDR DALA1025953124](https://openairdocs.org/sdr/DALA1025953124), Oct 7, 2010: SOLENOID. FAILED. DURING A NON ROUTINE CHECK, THE OXYGEN CONTAINER FAILED A DROP TEST AT ROW 4 LT. MX REPLACED SOLENOID IN OXYGEN CONTAINER AND FUNCTIONAL TEST WAS NORMAL.
- [SDR CA101004008](https://openairdocs.org/sdr/CA101004008), Oct 4, 2010: SEAL. DAMAGED. ON DEPARTURE CREW RECOGNIZED A HIGH RATE OF CLIMB IN CABIN PRESSURIZATION. CREW STOPPED THE CLIMB AND DESCENDED TO FL150 FOR DURATION OF FLIGHT. CABIN PRESSURE 
- [SDR CA101004004](https://openairdocs.org/sdr/CA101004004), Oct 2, 2010: VALVE. FAILED. AFTER TAKEOFF POWER WAS APPLIED THE CREW REJECTED TAKEOFF DUE TO A LOSS OF THE YELLOW HYD SYS PRESSURE. THE ACFT RETURNED TO THE GATE. EMERG BRAKE DUAL DISTRIBU
- [SDR DALA1024923129](https://openairdocs.org/sdr/DALA1024923129), Sep 30, 2010: FLOOR PANEL. DAMAGED. DURING L-CHECK FOUND DAMAGE TO AFT CARGO FLOOR PANEL 151 ZG. REPLACED FLOOR PANEL IAW DWG 3025-40532 & AMM 53-42-14, PAGE 401.
- [SDR CA101001002](https://openairdocs.org/sdr/CA101001002), Sep 30, 2010: COMPRESSOR. FAILED. LAVATORY-E WAS REPORTED TO HAVE WATER CONTINUOUSLY RUNNING FROM THE SINK FAUCET. THE WATER COMPRESSOR C/B WAS PULLED FROM THE AFT GALLEY CEILING PANEL 2001VU. A
- [SDR CA100929003](https://openairdocs.org/sdr/CA100929003), Sep 28, 2010: CHECK VALVE. FAILED. SHORTLY AFTER TAKEOFF, THE CREW REPORTED A YELLOW HYD SYS OVERHEAT AND AFTER DISCUSSION WITH MX AND SOC IT WAS DECIDED TO RETURN THE ACFT TO AIRPORT OF DEPARTUR
- [SDR DALA1022693101](https://openairdocs.org/sdr/DALA1022693101), Sep 14, 2010: SKIN. DAMAGED. DURING M-CHECK FOUND R2 DOOR LOWER CUT OUT EXTERNAL SKIN HAD 8 EA ELONGATED HOLES. REPAIRED IAW SRM 51-90-00, SRM 51-10-01, SRM 51-10-08 & ERA 484908-14.
- [SDR DALA1022703102](https://openairdocs.org/sdr/DALA1022703102), Sep 14, 2010: SKIN. DENTED. DURING M-CHECK FOUND DENT ON FUSELAGE SKIN BETWEEN FRAMES 24-25 STRINGER 42R TO STRINGER 41R. REPAIRED IAW SRM 53-21-11, SRM 51-75-15 & SRM 51-42-11. REPAIR MUS
- [SDR DALA1022493131](https://openairdocs.org/sdr/DALA1022493131), Sep 12, 2010: WIRE. DAMAGED. DURING A NON ROUTINE CHECK, FOUND EMERGENCY SEAT LIGHT AT ROW 12L AND 20L INOPERATIVE. MX REPAIRED WIRING AT SEAT ROW 12L AND 20L. FUNCTIONAL CHECK WAS NORMAL. 
- [SDR DALA1022503135](https://openairdocs.org/sdr/DALA1022503135), Sep 12, 2010: CONNECTOR. INOPERATIVE. DURING A NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 7C INOPERATIVE. MX INSTALLED NEW CONNECTOR AT SEAT HARNESS. FUNCTIONAL CHECK WAS NORMAL. AC
- [SDR DALA1022103102](https://openairdocs.org/sdr/DALA1022103102), Sep 11, 2010: DOOR FRAME. CORRODED. DURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED
- [SDR DALA1022093101](https://openairdocs.org/sdr/DALA1022093101), Sep 10, 2010: DOOR FRAME. CORRODED. DURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED
- [SDR DALA1022123102](https://openairdocs.org/sdr/DALA1022123102), Sep 10, 2010: FLOORBEAM. CORRODED. DURING M-CHECK FOUND CORROSION ON CABIN FLOORBEAM AT +Y1292 FR68. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.
- [SDR DALA1021953102](https://openairdocs.org/sdr/DALA1021953102), Sep 9, 2010: FLOOR PANEL. DELAMINATED. DURING M-CHECK FOUND CARGO FLOOR PANEL 131AF IS DELAMINATED. REPLACED FLOOR PANEL 161PF IAW DWG 3D25-40532.
- [SDR DALA1021963101](https://openairdocs.org/sdr/DALA1021963101), Sep 9, 2010: MOUNT. GOUGED. DURING M-CHECK FOUND GOUGE IN NR 1 PYLON AFT ENGINE MOUNT INBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTI
- [SDR DALA1021973101](https://openairdocs.org/sdr/DALA1021973101), Sep 9, 2010: MOUNT. GOUGED. DURING M-CHECK FOUND GOUGES IN NR 1 PYLON ENGINE MOUNT OTBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTION 
- [SDR DALA1021743101](https://openairdocs.org/sdr/DALA1021743101), Sep 8, 2010: FLOOR SUPPORT. CORRODED. DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FR 67 & FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.
- [SDR DALA1021753101](https://openairdocs.org/sdr/DALA1021753101), Sep 8, 2010: FLOOR SUPPORT. CORRODED. DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y1292 BETWEEN FR 66- FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.
- [SDR DALA1021723101](https://openairdocs.org/sdr/DALA1021723101), Sep 8, 2010: SILL. CORRODED. DURING M-CHECK FOUND CORROSION ON AFT RT AFT DOOR SILL. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.
- [SDR DALA1021763121](https://openairdocs.org/sdr/DALA1021763121), Sep 8, 2010: SEAT TRACK. DAMAGED. DURING LINE CHECK FOUND SEAT TRACK DAMAGE AT BS Y1292. REPAIRED IAW SRM 53-00-15 FIG 201.
- [SDR CA100913009](https://openairdocs.org/sdr/CA100913009), Sep 7, 2010: WINDSHIELD. CRACKED. LT WINDSHIELD CRACKED IN CRUISE - STARTED IN LOWER LT CORNER. ACFT DIVERTED, WINDSHIELD REPLACED. REFER ETQ SAFETY REPORT NR 12134. STRIP REPORT REQUESTED.
- [SDR DALA1021033210](https://openairdocs.org/sdr/DALA1021033210), Sep 2, 2010: FLOORBOARD. DAMAGED. FOUND FWD CARGO FLOORBOARDS DAMAGED BEYOND SRM LIMITS. R & R CARGO FLOORBOARDS 131AE AND 131EG IAW AMM 53-22-14.
- [SDR DALA1021053102](https://openairdocs.org/sdr/DALA1021053102), Sep 1, 2010: SEAT TRACK. CORRODED. CABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. LOG PAGE NR 0264321. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68)
- [SDR DALA1020983102](https://openairdocs.org/sdr/DALA1020983102), Sep 1, 2010: FLOOR SUPPORT. CORRODED. CABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68).
- [SDR DALA1020923101](https://openairdocs.org/sdr/DALA1020923101), Aug 30, 2010: FLOOR SUPPORT. CORRODED. AFT CABIN UTILITY AREA BETWEEN FR66 & FR68 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=2.100" W=1.100" D=0.055" ORIG MA
- [SDR DALA1020933101](https://openairdocs.org/sdr/DALA1020933101), Aug 30, 2010: FLOOR SUPPORT. CORRODED. AFT CABIN UTILITY AREA BETWEEN FR68 & FR69 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.500" W=1.300" D=0.075" ORIG MA
- [SDR DALA1020943101](https://openairdocs.org/sdr/DALA1020943101), Aug 30, 2010: SEAT TRACK. CORRODED. AFT CABIN UTILITY AREA FR66 SEAT TRACK Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.740" W=1.360" D=0.070" ORIG MAT THICKNESS 0.157 
- [SDR DALA1020913101](https://openairdocs.org/sdr/DALA1020913101), Aug 29, 2010: SEAT TRACK. CORRODED. FWD CABIN, FR16 TO FR20, SEAT TRACK -Y254 CORRODED AT 2 AREAS. BLENDED OUT CORROSION AREA IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REMOVED D
- [SDR DALA1020883101](https://openairdocs.org/sdr/DALA1020883101), Aug 28, 2010: SEAT TRACK. CORRODED. FWD CABIN, FR20 DUMMY RAIL AT -Y189 CORRODED THRU T-CHORD OF SEAT TRACK. REMOVED DUMMY RAIL AT FR20 Y-189 IAW SRM 51-42-11 REMOVED CORROSION IAW SRM 51-74-00 BL
- [SDR DALA1020893101](https://openairdocs.org/sdr/DALA1020893101), Aug 28, 2010: FLOOR SUPPORT. CORRODED. AFT CABIN UTILITY AREA BETWEEN FR 66 & FR 70 FLOOR SUPPORT Y-765 HAS CORROSION. BLENDED OUT CORRODED AREA IAW SRM 51-74-00 DIMENSION L=1.900" W=1.020" D=.065" M
- [SDR DALA1020903102](https://openairdocs.org/sdr/DALA1020903102), Aug 28, 2010: FLOOR SUPPORT. CORRODED. CABIN FLOOR LONGITUDINAL BEAM AT FR 66, Y512 HAS CORROSION. REMOVED DAMAGED FLOORBEAM AT FR 66, Y512 DAMAGED AREA DIM ARE W=0.50" D=0.24" L=1.5" FOUND TO BE OUT
- [SDR DALA1020453101](https://openairdocs.org/sdr/DALA1020453101), Aug 25, 2010: FLOOR SUPPORT. CORRODED. DURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS +Y765 BETWEEN FR 66 & FR 69. REPAIRED IAW SRM 51-42-11, 51-44-11.
- [SDR DALA1019253114](https://openairdocs.org/sdr/DALA1019253114), Aug 11, 2010: WIRE. DAMAGED. DURING A NON-ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 11 INOP. REPAIRED WIRE AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL AND ACFT RETURNED TO S
- [SDR CA100819011](https://openairdocs.org/sdr/CA100819011), Aug 10, 2010: SAFETY VALVE. SHORTED. A SHORT IN THE LANDING GEAR HYD SAFETY VALVE CAUSED THE TRIPPING OR CIRCUIT BREAKERS LGCIU SYS 1 AND LGCIU SYS 1 GRD SUP. THE FAILURE CONDITION OF THE LANDING G
- [SDR CA100804025](https://openairdocs.org/sdr/CA100804025), Jul 23, 2010: WINDOW. FAILED. IN CRUISE, CAPT`S REAR FIXED WINDOW SHATTERED. THE CREW FOLLOWED THE QRH AND DESCENDED TO FL230 JUST PRIOR TO TOD. ATC WAS ADVISED, NO EMERGENCY WAS DECLARED.
- [SDR DALA1012253123](https://openairdocs.org/sdr/DALA1012253123), Jun 5, 2010: BATTERY PACK. INOPERATIVE. DURING A NON ROUTINE CHECK, EMERGENCY LIGHT ON FAP MESSAGE EPSU LOAD FAIL AT FWD LT. REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORMAL. ACFT RETURNED TO SERV
- [SDR DALA1010293102](https://openairdocs.org/sdr/DALA1010293102), May 17, 2010: WIRE HARNESS. INOPERATIVE. DURING A NON ROUTINE CHECK, MX FOUND SEAT 5C EMERGENCY LIGHT INOPERATIVE. FOUND WIRE PULLED FROM INBD CONNECTOR OF HARNESS. REPLACED HARNESS AND FUNCTIONAL CHEC
- [SDR DALA109573152](https://openairdocs.org/sdr/DALA109573152), May 8, 2010: WIRE. DAMAGED. DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 5C INOPERATIVE. MX REPAIRED WIRE AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

All 109: https://openairdocs.org/engine/cfm-international-cfm56-5a-series/reports.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [3051-1051KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121122166320260805155543.0001): Seal, Trapezoidal. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 3051-1051 · Jul 21, 2026
- [3051-1051KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121122166320260805155543.0001): Seal, Trapezoidal. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 3051-1051 · Jul 21, 2026
- [AAP-3504163-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180945408320260406133714.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3504163-1 · Apr 1, 2026
- [AAP-3504163-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180945408320260406133714.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3504163-1 · Apr 1, 2026
- [336-031-701-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144123523920260324201242.0001): Weight-Balance 2.9G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-701-0 · Feb 25, 2026
- [336-031-701-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144123523920260324201242.0001): Weight-Balance 2.9G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-701-0 · Feb 25, 2026
- [336-031-710-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129285223420260324201243.0001): Weight-Balance 6.5G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-710-0 · Feb 25, 2026
- [336-031-710-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129285223420260324201243.0001): Weight-Balance 6.5G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-710-0 · Feb 25, 2026
- [336-031-708-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112259513820260324201242.0001): Weight-Balance 5.7G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-708-0 · Feb 25, 2026
- [336-031-708-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112259513820260324201242.0001): Weight-Balance 5.7G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-708-0 · Feb 25, 2026
- [E140375-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181608826420251229153151.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-3 · Dec 17, 2025
- [E140375-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181608826420251229153151.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-3 · Dec 17, 2025
- [E140375-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149149609920251229153152.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-4 · Dec 17, 2025
- [E140375-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149149609920251229153152.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-4 · Dec 17, 2025
- [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199148521820251125143636.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025
- [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199148521820251125143636.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025
- [WF335301](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167080527920250602133024.0001): Filter Element, Lube. Donaldson Company Inc · PMA PQ2432CE · Replaces QA06422, Alternate: 7593194-101… · May 23, 2025
- [WF335301](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167080527920250602133024.0001): Filter Element, Lube. Donaldson Company Inc · PMA PQ2432CE · Replaces QA06422, Alternate: 7593194-101… · May 23, 2025
- [1211313-010](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102870449220250402211756.0001): Actuator, Variable Stator. Arkwin Industires Inc · PMA PQ0365NE · Replaces 1324M12P10Software version: N/A · Mar 24, 2025
- [1211313-010](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102870449220250402211756.0001): Actuator, Variable Stator. Arkwin Industires Inc · PMA PQ0365NE · Replaces 1324M12P10Software version: N/A · Mar 24, 2025
- [305-050-003-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147610688520250311191844.0001): Nipple Assy Restrictor. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 305-050-003-0 · Feb 28, 2025
- [305-050-003-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147610688520250311191844.0001): Nipple Assy Restrictor. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 305-050-003-0 · Feb 28, 2025
- [9528M76P01KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118980261520250303215300.0001): Sleeve. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9528M76P01 · Feb 27, 2025
- [9528M76P01KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118980261520250303215300.0001): Sleeve. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9528M76P01 · Feb 27, 2025
- [9115M40P03JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131954054120250311191919.0001): Spacer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 9115M40P03 · Feb 17, 2025
- [9115M40P03JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131954054120250311191919.0001): Spacer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 9115M40P03 · Feb 17, 2025
- [663700-124WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112350436520250226225453.0001): Packing. Wencor, LLC · PMA PQ1370NM · Replaces 663700-124 · Jan 30, 2025
- [663700-124WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112350436520250226225453.0001): Packing. Wencor, LLC · PMA PQ1370NM · Replaces 663700-124 · Jan 30, 2025
- [219818-2MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139406088920241211141040.0001): Bolt-D Head. Mitchell PMA, LLC · PMA PQ04379CE · Replaces 219818-2 · Dec 6, 2024
- [219818-2MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139406088920241211141040.0001): Bolt-D Head. Mitchell PMA, LLC · PMA PQ04379CE · Replaces 219818-2 · Dec 6, 2024
- [1523M39P07KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134003115120241022134047.0001): Hook Bolt, Self-Wrenching. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 1523M39P07 · Sep 23, 2024
- [1523M39P07KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134003115120241022134047.0001): Hook Bolt, Self-Wrenching. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 1523M39P07 · Sep 23, 2024
- [TA0330014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198478108420240715162425.0001): Clamp. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces TA0330014 · Jul 12, 2024
- [TA0330014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198478108420240715162425.0001): Clamp. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces TA0330014 · Jul 12, 2024
- [P00018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196766919420240620131645.0001): Seal Element. Aviation Component Solutions · PMA PQ2685CE · Replaces 569246 · May 14, 2024
- [P00018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196766919420240620131645.0001): Seal Element. Aviation Component Solutions · PMA PQ2685CE · Replaces 569246 · May 14, 2024
- [P00328](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194618868620240620131652.0001): Shaft Seal Bushing. Aviation Component Solutions · PMA PQ2685CE · Replaces 353850 · May 14, 2024
- [P00328](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194618868620240620131652.0001): Shaft Seal Bushing. Aviation Component Solutions · PMA PQ2685CE · Replaces 353850 · May 14, 2024
- [P00512](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193343169320240620131654.0001): Wave Spring. Aviation Component Solutions · PMA PQ2685CE · Replaces 330894 · May 14, 2024
- [P00512](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193343169320240620131654.0001): Wave Spring. Aviation Component Solutions · PMA PQ2685CE · Replaces 330894 · May 14, 2024
- [P00647](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191418655420240620131656.0001): Sealing Element. Aviation Component Solutions · PMA PQ2685CE · Replaces 972576 · May 14, 2024
- [P00647](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191418655420240620131656.0001): Sealing Element. Aviation Component Solutions · PMA PQ2685CE · Replaces 972576 · May 14, 2024
- [P00267](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191074779720240620131648.0001): Compensator Bushing & Valves S/A. Aviation Component Solutions · PMA PQ2685CE · Replaces 569546 · May 14, 2024
- [P00267](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191074779720240620131648.0001): Compensator Bushing & Valves S/A. Aviation Component Solutions · PMA PQ2685CE · Replaces 569546 · May 14, 2024
- [P00937](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187019017720240620131703.0001): Spring Guide. Aviation Component Solutions · PMA PQ2685CE · Replaces 624124 · May 14, 2024
- [P00937](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187019017720240620131703.0001): Spring Guide. Aviation Component Solutions · PMA PQ2685CE · Replaces 624124 · May 14, 2024
- [P00323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184721597820240620131649.0001): Seal Grommet. Aviation Component Solutions · PMA PQ2685CE · Replaces 329282 · May 14, 2024
- [P00323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184721597820240620131649.0001): Seal Grommet. Aviation Component Solutions · PMA PQ2685CE · Replaces 329282 · May 14, 2024
- [P00023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183044716520240620131646.0001): Spring Seat. Aviation Component Solutions · PMA PQ2685CE · Replaces 569362 · May 14, 2024
- [P00023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183044716520240620131646.0001): Spring Seat. Aviation Component Solutions · PMA PQ2685CE · Replaces 569362 · May 14, 2024

All of them: https://openairdocs.org/engine/cfm-international-cfm56-5a-series/pma.md

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