# CFM International CFM56-7B27/B3 series

- Type: Engine model (FAA registry)
- Registry code: 13054
- Manufacturer (registry): CFM INTL
- Model: CFM56-7B27/B3
- Engine type: Turbo-fan
- Power: 27,300 lb thrust
- Installed in: 23 registered aircraft
- Page: https://openairdocs.org/engine/cfm-international-cfm56-7b27-b3-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 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [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 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 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 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [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 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [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 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998

Historical (superseded or no longer in force):

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

## Information bulletins (advisory) (4)

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [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 (23)

- [N162WC](https://openairdocs.org/aircraft/N162WC): [Wca Holdings III LLC](https://openairdocs.org/faa-owner/WCA%20HOLDINGS%20III%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1999, S/N 30329
- [N20TM](https://openairdocs.org/aircraft/N20TM): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2010, S/N 39109
- [N235JF](https://openairdocs.org/aircraft/N235JF): [Flye Aviation Corp](https://openairdocs.org/faa-owner/FLYE%20AVIATION%20CORP), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), S/N 32774
- [N324CH](https://openairdocs.org/aircraft/N324CH): [N324ch LLC](https://openairdocs.org/faa-owner/N324CH%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 2001, S/N 33010
- [N38424](https://openairdocs.org/aircraft/N38424): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2008, S/N 37095
- [N39416](https://openairdocs.org/aircraft/N39416): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2008, S/N 37093
- [N512AS](https://openairdocs.org/aircraft/N512AS): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2008, S/N 39043
- [N524AS](https://openairdocs.org/aircraft/N524AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), built 2009, S/N 35195
- [N525AS](https://openairdocs.org/aircraft/N525AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), built 2009, S/N 35692
- [N527AS](https://openairdocs.org/aircraft/N527AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), S/N 35694
- [N583AS](https://openairdocs.org/aircraft/N583AS): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2007, S/N 35681
- [N584AS](https://openairdocs.org/aircraft/N584AS): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2007, S/N 35682
- [N585AS](https://openairdocs.org/aircraft/N585AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), built 2007, S/N 35683
- [N586AS](https://openairdocs.org/aircraft/N586AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), built 2007, S/N 35189
- [N587AS](https://openairdocs.org/aircraft/N587AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seatac, WA](https://openairdocs.org/faa-place/WA/Seatac), built 2007, S/N 35684
- [N590AS](https://openairdocs.org/aircraft/N590AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle), built 2008, S/N 35687
- [N592AS](https://openairdocs.org/aircraft/N592AS): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2008, S/N 35190
- [N594AS](https://openairdocs.org/aircraft/N594AS): [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle), built 2008, S/N 35191
- [N78509](https://openairdocs.org/aircraft/N78509): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2008, S/N 31638
- [N8767](https://openairdocs.org/aircraft/N8767): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2002, S/N 32807
- [N950TR](https://openairdocs.org/aircraft/N950TR): [Ohio Resources LLC](https://openairdocs.org/faa-owner/OHIO%20RESOURCES%20LLC), [Camden, DE](https://openairdocs.org/faa-place/DE/Camden), built 1999, S/N 30751
- [N972BJ](https://openairdocs.org/aircraft/N972BJ): [Flye Aviation Corp](https://openairdocs.org/faa-owner/FLYE%20AVIATION%20CORP), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), built 2002, S/N 29972
- [N9PF](https://openairdocs.org/aircraft/N9PF): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2009, S/N 37583

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA26LA102](https://openairdocs.org/ntsb/DCA26LA102), Jan 15, 2026: Boeing 737 (N583AS), Kodiak, AK, substantial damage. Probable cause: The reduced surface friction of the contaminated ramp which led to a loss of directional control during taxi.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20091028025649I](https://openairdocs.org/incident/20091028025649I), Oct 28, 2009: Boeing 737-890 (N525AS), Anchorage, AK, Substantial damage. Asaa flt#131 departed ord for anc. There was no suspected tire damage on takeoff. When the gear was lowered on final at anc, the crew noted an unsafe…

## Service difficulty reports (363, newest 50)

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

- [SDR CALA2026012113129](https://openairdocs.org/sdr/CALA2026012113129), Jan 18, 2026: ANTI-ICE VALVE. FAULTED. RTO AT 20KTS FOR COWL ANTI-ICE CAUTION NR 1 ENGINE. R & R THE NR 1 ENGINE COWL ANT-ICE VALVE IAW AMM 30-21-11-400-801. OPS & LEAK CHECKED GOOD IAW AMM 30-21-11-
- [SDR ASAA2023012391589](https://openairdocs.org/sdr/ASAA2023012391589), Jan 19, 2023: PACKING. LEAKING. ENGINE NUMBER 1 HAS OIL BY THE IDG DOOR. LOOKS EXCESSIVE. GROUNDED - YES. FOUND EVIDENCE OF SEALOL SEAL LEAKING. REPLACED SELOL SEAL IAW B737-800 AMM 72-60-00.
- [SDR CALA2023010900064](https://openairdocs.org/sdr/CALA2023010900064), Jan 9, 2023: HMU. INOPERATIVE. LEFT ENGINE UNABLE TO PRODUCE MORE THAN 90.1 WITH A REQUEST FOR MAX RIGHT ENG 100.3 CLOSE TO 80 DEGREES AT IDLE. REMOVED MAIN FUEL PUMP. INSTALLED NR 1 HMU IAW 
- [SDR ASAA2023010241358](https://openairdocs.org/sdr/ASAA2023010241358), Jan 2, 2023: SPACER. DEBONDED. WHILE ACCOMPLISHING FAN LUBE CARD #1 ENG FOUND SPACERS DISBONDING ON 2, 3, 4, 5, 7, 11, 13, 14, 15, 17, 18, 19, & 20. GROUNDED - YES. REMOVED AND REPLACED #1 EN
- [SDR ASAA2022112940967](https://openairdocs.org/sdr/ASAA2022112940967), Nov 29, 2022: BLEED VALVE. FAULTY. P6-4 BLEED AIR VALVES LEFT CIRCUIT BREAKER FOUND OPEN DURING PRE-FLIGHT. GROUNDED - YES. P6-4,A7 C796 C/B POPPED OPEN AFTER RESET REF SSM 36-11-11-102 REMOVED C
- [SDR ASAA2022101040233](https://openairdocs.org/sdr/ASAA2022101040233), Oct 10, 2022: SPACER. UNBONDED. WHILE ACCOMPLISHING FAN LUBE ASA T/C 78472010, #1 ENGINE, FOUND #10 SPACER ELASTOMER STRIP UNBONDED. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE, #10 SPACER 
- [SDR ASAA2022101040234](https://openairdocs.org/sdr/ASAA2022101040234), Oct 10, 2022: SHIM. WORN. WHILE ACCOMPLISHING FAN LUBE ASA T/C 78472010, #1 ENGINE FOUND ALL SHIMS TO BE WORN. GROUNDED - YES. REMOVED AND REPLACED ALL #1 ENGINE SHIMS PER ASA T/C 784720
- [SDR ASAA2022100740215](https://openairdocs.org/sdr/ASAA2022100740215), Oct 7, 2022: ENGINE. LEAKING. # 2 ENGINE DRIPPING FUEL. GROUNDED - YES. ON DEFERRAL.
- [SDR ASAA2022100340154](https://openairdocs.org/sdr/ASAA2022100340154), Oct 3, 2022: SPACER. DEBONDED. PER ASA TC 78472010 #2 ENF FAN LUBE SPACERS #1,2,3,4,5,8,10,11,13,14,16,20,21,22,23 AND 24 ARE DISBONDED. GROUNDED - YES. REMOVED & REPLACED #2 ENG FAN LUBE SPA
- [SDR ASAA2022092740136](https://openairdocs.org/sdr/ASAA2022092740136), Sep 27, 2022: VALVE. LEAKING. #2 ENGINE FUEL DRIPPING FROM DRAIN MAST WITH ENGINE OFF. GROUNDED - YES. FUEL LEAKING FROM #2 ENGINE TBV @ 70 DROPS /MIN STATIC. RAN ENGINE FOR 5 MINUTES REF B7
- [SDR ASAA2022091239946](https://openairdocs.org/sdr/ASAA2022091239946), Sep 12, 2022: ENGINE. MULTIPLE IND. #2 ENGINE S/N 894549 REF ASA T/C SBC FM 56-7B-72-1074-1, THIRD STAGE VSV SEGMENT AT 4 O'CLOCK SEAL SEGMENT GAP IS GREATER THEN .500, J HOOK MISSING AND STATOR S
- [SDR ASAA2022082539678](https://openairdocs.org/sdr/ASAA2022082539678), Aug 25, 2022: IGNITER. FAULTY. WHILE STARTING ENGINE #1 NO FUEL FLOW WITHIN 30 SEC. ON 2ND START ATTEMPT FUEL FLOW CAME UP NORMALLY AND DROPPED TO0 IN A FEW SECONDS. ON 3RD ATTEMPT USING IGN 
- [SDR ASAA2022081039459](https://openairdocs.org/sdr/ASAA2022081039459), Aug 10, 2022: SENSOR. BENT. DURING REPLACEMENT OF J9 AND J10 HARNESSES ON ENG 1, REF ASA LOGPAGE 60482836, FOUND T3 SENSOR RECEPTACLE BENT. GROUNDED - YES. REMOVED AND REPLACED T3 SENSOR I
- [SDR ASAA2022072239309](https://openairdocs.org/sdr/ASAA2022072239309), Jul 22, 2022: SEAL. LEAKING. #2 ENGINE CONTINUES TO SHOW GREATER THAN EXPECTED OIL CONSUMPTION. GROUNDED - YES. REMOVED AND REPLACED SEALOL SEAL IAW B737-800 AMM 72-60-00.
- [SDR ASAA2022063038882](https://openairdocs.org/sdr/ASAA2022063038882), Jun 30, 2022: CONNECTOR. BROKEN. #2 ENGINE TAI VALVE CONNECTOR BACK SHELL IS BROKEN OFF. GROUNDED - YES. REMOVED AND REPLACED MW0313 ON #2 ENGINE ALL TESTS CK GOOD REF B737-800 AMM 71-51-03-000
- [SDR ASAA2022062438800](https://openairdocs.org/sdr/ASAA2022062438800), Jun 24, 2022: TRANSMITTER. LEAKING. WHILE PERFORMING LEAK CHECK ON THE # 1 MOTOR NOTED THE FUEL FLOW TRANSMITTER LEAKING. GROUNDED - YES. REMOVED AND REPLACED # 1 ENG FUEL FLOW TRANSMITTER AND PER
- [SDR ASAA2022062338773](https://openairdocs.org/sdr/ASAA2022062338773), Jun 23, 2022: PLATFORM. WORN. WHILE ACCOMPLISHING TC 78472010 FOUND 8 PLATFORMS WITH RUBBER MISSING. (6, 11, 12, 17, 19, 20, 22, AND 24). GROUNDED - YES. REPLACED 8 PLATFORMS (6, 11, 12, 17,
- [SDR ASAA2022062338774](https://openairdocs.org/sdr/ASAA2022062338774), Jun 23, 2022: ELASTOMER. LOOSE. WHILE ACCOMPLISHIG TC 78472010 FOUND 11 SPACERS WITH LOOSE ELASTOMER (1, 2, 4, 5, 10, 12, 13, 16, 21, 23, AND 24). GROUNDED - YES. REPLACED 11 SPACERS (1, 2, 4,
- [SDR ASAA2022061738699](https://openairdocs.org/sdr/ASAA2022061738699), Jun 17, 2022: DRAIN LINE. LEAKING. #1 ENG MAIN FUEL/OIL HEAT EXCHANGER PAD DRAIN LINE DRIPPING FUEL OUT OF LIMITS. GROUNDED - YES. REMOVED #1 MAIN FUEL/OIL HEAT EXCHANGER PER B737-800 AMM 79-21-0
- [SDR ASAA2022061738936](https://openairdocs.org/sdr/ASAA2022061738936), Jun 17, 2022: O-RING. LEAKING. #2 ENGINE OIL TREND DATA SHOWS OIL CONSUMPTION TO GREATER THAN EXPECTED. ENGINE POWER RUN REQUIRED RECOMMEND SEA ONLY. GROUNDED - YES. ACCOMPLISHED STEPS 1 THRO
- [SDR ASAA2022053038504](https://openairdocs.org/sdr/ASAA2022053038504), May 30, 2022: SEAL. LEAKING. #2 ENGINE OIL CONSUMPTION IS HIGHER THAN DESIRED. CURRENT OIL CONSUMPTION .4. GROUNDED - YES. COMPLETED STEPS 1 AND 2 OF TSR AND BAGGED OIL DRAINS FOR STEP 3. F
- [SDR ASAA2022052738500](https://openairdocs.org/sdr/ASAA2022052738500), May 27, 2022: IGNITER. DAMAGED. WHILE WORKING A T-101 FOR TRANSIT BLEED VALVE HARNESS CHANGE: FOUND LT & RT IGNITER LEAD COOLING TUBE (ORANGE) DISCONNECTED ON THE LT AND TORN ON THE RT. GROUND
- [SDR ASAA2022052538448](https://openairdocs.org/sdr/ASAA2022052538448), May 25, 2022: HARNESS. FAULTY. #1 ENGINE EGT TREND DATA SHOWS RECENT GREATER THAN NORMAL SCATTER AND INCREASE IN DELTA EGT/DECREASE IN EGTHDM. GROUNDED - YES. REF ASA L/P 60458740. INPUT MONI
- [SDR ASAA2022052538454](https://openairdocs.org/sdr/ASAA2022052538454), May 25, 2022: SENSOR. DAMAGED. DURING TROUBLESHOOTING #1 ENG EGT REF ASA LOG 60458740 AND ASA TSR TSR7122012, FOUND T3A CONNECTOR INSULATOR DAMAGE AND T3 SENSOR PIN DAMAGE. SENSOR KEYWAY FOUN
- [SDR ASAA2022052538455](https://openairdocs.org/sdr/ASAA2022052538455), May 25, 2022: HARNESS. FAULTY. RED BOX AROUND #1 EGT APPEARS AFTER LANDING. GROUNDED - YES. ENGINE 1 BITE CHECK SHOWS FAULT 77-20861, ENGINE EXCEEDANCE PAGE SHOWS EGT EXCEEDANCE 961 2 SECONDS
- [SDR ASAA2022052438503](https://openairdocs.org/sdr/ASAA2022052438503), May 24, 2022: BLEED VALVE. FAILED. WHILE PERFORMING ASA TC 78273000 FOUND FC 75-30602 THE TBV POSITION SIGNALS DISAGREE. ON LEGS 1 AND 5. ON #2 ENGINE. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 2
- [SDR ASAA2022051438303](https://openairdocs.org/sdr/ASAA2022051438303), May 14, 2022: SHIM. OUT OF LIMITS. WHILE ACCOMPLISHING #2 FAN BLADE LUBE FOUND 24 SHIMS TO BE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED 24 EA FAN BLADE SHIMS ON #2 ENGINE PER TASK CARD 
- [SDR ASAA2022051438317](https://openairdocs.org/sdr/ASAA2022051438317), May 14, 2022: PLATFORM. WORN. WHILE ACCOMPLISHING #2 FAN BLADE LUBE FOUND 6 PLATFORMS WORN OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED 6 EA PLATFORMS ON #2 ENGINE PER TASK CARD 78472
- [SDR ASAA2022051438318](https://openairdocs.org/sdr/ASAA2022051438318), May 14, 2022: SPINNER. DAMAGED. WHILE ACCOMPLISHING #2 FAN BLADE LUBE FOUND FRONT SPINNER DAMAGED. GROUNDED - YES. REMOVED AND REPLACED SPINNER ON #2 ENGINE PER TASK CARD 78472010.
- [SDR ASAA2022051438326](https://openairdocs.org/sdr/ASAA2022051438326), May 14, 2022: BLEED VALVE. FAULTY. #2 ENG SHORT TIME(MSG NBR: 75-30602)THE TBV POSITION SIGNALS DISAGREE. DEFERRED PER T/C 78273000. GROUNDED - YES. REMOVED AND REPLACED TRANSIENT BLEED VALVE PER
- [SDR ASAA2022050838266](https://openairdocs.org/sdr/ASAA2022050838266), May 8, 2022: EEC. FAULTY. SHORT TERM FAULT 75-30602 (TBV POSITION SIGNALS DISAGREE) FOUND WHILE ACCOMPLISHING ASA T/C 78283000 FOR ENG #2. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE 
- [SDR ASAA2021081335705](https://openairdocs.org/sdr/ASAA2021081335705), Aug 13, 2021: EEC. FAULTED. DURING "AFTER ENGINE CHANGE" TESTING - MULTIPLE FAULTS LOGGED DURING EEC BITE TEST AND ACUATOR TESTS. GROUNDED - YES. REMOVED AND REPLACED EEC ON #1 ENG REF AMM
- [SDR ASAA2021081035685](https://openairdocs.org/sdr/ASAA2021081035685), Aug 10, 2021: TURBINE WHEEL. DISTRESSED. PER MAINTENANCE CONTROL, SEA ACCOMPLISHED THE FOLLOWING DEFECT: WHILE ACCOMPLISHING TASK CARD #78472022 "SDI BOROSCOPE ENGINE HPT BLADES" #2 ENGINE S/N 895170 F
- [SDR ASAA2021080735723](https://openairdocs.org/sdr/ASAA2021080735723), Aug 7, 2021: ENGINE. FAULTY. AFTER SHUTDOWN EGT DIGITAL READOUT BOX TURNED RED ON #2 ENGINE NO ABNORMAL INDICATIONS NOTED PRIOR TO THE RED BOX. GROUNDED - YES. #2 ENG. REPLACED, TRANSFERRED
- [SDR ASAA2021061535131](https://openairdocs.org/sdr/ASAA2021061535131), Jun 15, 2021: ACTUATOR. FAULTED. WHILE PERFORMING T/C 78273000 FOUND LONG TIME MESSAGE ON #2 ENG # 75-10392 VSV POSTION SIGNAL IS OUT OF RANGE, DEFERRED PER T/C 78273000. GROUNDED - YES. ACCOMP
- [SDR ASAA2021052934983](https://openairdocs.org/sdr/ASAA2021052934983), May 29, 2021: PRESSURE SWITCH. FAULTY. WHILE ACCOMPLISHING T/C 78273000 #2 ENG CODE 73-31072 LONG TIME FAULT THE FUEL FILTER SIGNALS DISAGREE. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FUEL FILTER 
- [SDR ASAA2021052634982](https://openairdocs.org/sdr/ASAA2021052634982), May 26, 2021: BLADE. CRACKED. WHILE ACCOMP #1 ENG S/N 897424 HPT BLADE INSPECTION TC 78472022. FOUND ONE LPT 1ST STG NGV @ APPROX 3CLOCK POSN AFT LOOKING FWD. HAD ONE FULL CRACK WITH INTERSE
- [SDR ASAA2021052034877](https://openairdocs.org/sdr/ASAA2021052034877), May 20, 2021: GUIDE VANE. CRACKED. WHILE ACCOMPLISHING #2 ENG HPT BORO T/C 78472022 FOUND 4 EA LPT NGV CRACKED. EACH CRACKED NGV IS IN IT'S OWN SEGMENT. ONE IS CRACKED 1/2 TO 3/4 CHORD. 2 EA ARE 
- [SDR ASAA2021041734592](https://openairdocs.org/sdr/ASAA2021041734592), Apr 17, 2021: SWITCH. FAILED. #2 ENG VALVE CLOSED LIGHT ILLUMINATED BRIGHT DOES NOT DIM. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE HMU HPSOV SWITCH REF B737-800 AMM 73-21-09-000/400-801
- [SDR ASAA2021041434575](https://openairdocs.org/sdr/ASAA2021041434575), Apr 14, 2021: SPACER. DEBONDED. PER T/C 78472010 #2 ENG FAN BLADE LUBE INSP SPACERS #4 AND 16 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REPLACED #2 ENG BLADE SPACERS #4 AND #16 PER T/C 7847201
- [SDR ASAA2021041434576](https://openairdocs.org/sdr/ASAA2021041434576), Apr 14, 2021: PLATFORM. WRONG PART. PER T/C 78472010 #2 ENG FAN BLADE LUBE INSP, PLATFORM #11 HAS A WRONG PART #. GROUNDED - YES. REPLACED #11 PLATFORM ON #2 ENGINE PER T/C 78472010.
- [SDR ASAA2021032834453](https://openairdocs.org/sdr/ASAA2021032834453), Mar 28, 2021: GEARBOX. LEAKING. REPEAT OIL LEAKING #1 ENG ONTO FMU PUDDLING. GROUNDED - YES. REMOVED TGB REF B737-800 AMM 72-62-00-000-801-F00, INSTALLED SERVICEABLE TGB REF AMM 72-62-00-400-8
- [SDR ASAA2021031734312](https://openairdocs.org/sdr/ASAA2021031734312), Mar 17, 2021: SPACER. DEBONDED. PER T/C 78472010 #2 ENG. FAN BLADE LUBE, SPACER #20 ELASTOMER IS DIDBONDED. GROUNDED - YES. REMOVED AND REPLACED #20 SPACER ON #2 ENG. REF T/C 78472010.
- [SDR ASAA2021031734313](https://openairdocs.org/sdr/ASAA2021031734313), Mar 17, 2021: BLADE. WORN. PER T/C 78472010 #2 ENG. FAN BLADE LUBE, #17 FAN BLADE MISSING CU-NI-IN COATING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED BLADE #17 AND ITS PAIR #5 ON
- [SDR ASAA2021030934261](https://openairdocs.org/sdr/ASAA2021030934261), Mar 9, 2021: SPACER. DEBONDED. PER T/C 78472010 #1 ENG. FAN BLADE LUBE, SPACERS #1, 11, 18, AND 22 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REPLACED #1 ENG. FAN BLADE SPACERS #1, 11, 18, AND
- [SDR ASAA2021030934270](https://openairdocs.org/sdr/ASAA2021030934270), Mar 9, 2021: FUEL SYS. LEAKING. FUEL LEAK NOTED AT #2 ENGINE. GROUNDED - YES. ON DEFERRAL.
- [SDR ASAA2020122533766](https://openairdocs.org/sdr/ASAA2020122533766), Dec 25, 2020: BRACKET. LOOSE. DURING J9 HARNESS CHANGE, FOUND BRACKET THAT HOLDS J9 TO 3 O'CLOCK STRUT LOOSE UNDER RIVETS. GROUNDED-YES. REMOVED AND REPLACED BRACKET AND FASTENERS, BRACKET I
- [SDR ASAA2020121933730](https://openairdocs.org/sdr/ASAA2020121933730), Dec 19, 2020: START VALVE. STUCK. NR 1 ENGINE START VALVE FAILED TO OPEN DURING ENGINE START. GROUNDED-YES. NR 1 ENGINE START VALVE FROZEN. THAWED VALVE AND ENGINE NR 1 START, OPERATIONS NORMAL.
- [SDR ASAA2020121233687](https://openairdocs.org/sdr/ASAA2020121233687), Dec 12, 2020: HEAT EXCHANGER. DAMAGED. WHILE REPLACING NR 1 ENGINE FUEL PUMP PACKAGE FUEL/OIL HEAT EXCHANGER FAILED BOLT TORQUE LOCKING CHECK. GROUNDED-YES. REMOVED AND REPLACED MAIN OIL/FUEL HEAT EX
- [SDR ASAA2020121133686](https://openairdocs.org/sdr/ASAA2020121133686), Dec 11, 2020: SPINNER. DAMAGED. NR 2 ENGINE FRONT SPINNER COATING OUT OF LIMITS. GROUNDED-YES. REMOVED AND REPLACED NR 2 ENGINE FWD SPINNER, REF T/C 78472010.

All 363: https://openairdocs.org/engine/cfm-international-cfm56-7b27-b3-series/reports.md

## STCs that may be installed (OpenAirDocs) (2)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## 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.

- [AAP-3179410-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161769751220261022213314.0001): SETSCREW. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3179410-1 · Oct 14, 2026
- [AAP-3179410-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161769751220261022213314.0001): SETSCREW. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3179410-1 · Oct 14, 2026
- [KT9974M10P207](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156771068620261019153205.0001): Ring, Piston. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9974M10P207 · Oct 7, 2026
- [KT9974M10P207](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156771068620261019153205.0001): Ring, Piston. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9974M10P207 · Oct 7, 2026
- [337-141-601-0KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157822411420261008134816.0001): Bolt. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 337-141-601-0 · Sep 29, 2026
- [337-141-601-0KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157822411420261008134816.0001): Bolt. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 337-141-601-0 · Sep 29, 2026
- [649-788-399-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103937182820260909145920.0001): Packing-Preformed O-Ring. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 649-788-399-0 · Aug 24, 2026
- [649-788-399-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103937182820260909145920.0001): Packing-Preformed O-Ring. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 649-788-399-0 · Aug 24, 2026
- [AAP-3181263-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134991105620260923165754.0001): SPRING. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3181263-1 · Aug 5, 2026
- [AAP-3181263-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134991105620260923165754.0001): SPRING. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3181263-1 · Aug 5, 2026
- [2002M87P02JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199317637820260806140031.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P02 · Jul 30, 2026
- [2002M87P02JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199317637820260806140031.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P02 · Jul 30, 2026
- [2002M87P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133871277820260806140030.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P01 · Jul 30, 2026
- [2002M87P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133871277820260806140030.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P01 · Jul 30, 2026
- [3177421JP-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144029116620260805181453.0001): Setscrew. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 3177421-1 · Jul 16, 2026
- [3177421JP-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144029116620260805181453.0001): Setscrew. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 3177421-1 · Jul 16, 2026
- [301-547-905-0JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163539788920260806140647.0001): Nut. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 301-547-905-0 · Jul 14, 2026
- [301-547-905-0JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163539788920260806140647.0001): Nut. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 301-547-905-0 · Jul 14, 2026
- [AAP-3181264-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110152260220260804212133.0001): LINK ASSEMBLY. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3181264-1 · Jun 29, 2026
- [AAP-3181264-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110152260220260804212133.0001): LINK ASSEMBLY. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3181264-1 · Jun 29, 2026
- [1211342-240-014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101824618120260706131723.0001): Packing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1211342-240-014 · Jun 25, 2026
- [1211342-240-014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101824618120260706131723.0001): Packing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1211342-240-014 · Jun 25, 2026
- [9523M35G03JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191057781220260806140516.0001): Arm Assembly. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 9523M35G03 · Jun 8, 2026
- [9523M35G03JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191057781220260806140516.0001): Arm Assembly. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 9523M35G03 · Jun 8, 2026
- [1385M33G03JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141058667820260806140515.0001): Arm Assembly. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 1385M33G03 · Jun 8, 2026
- [1385M33G03JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141058667820260806140515.0001): Arm Assembly. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 1385M33G03 · Jun 8, 2026
- [1476M79P05JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107210147820260616140659.0001): Damper - Forward Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1476M79P05 · May 29, 2026
- [1476M79P05JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107210147820260616140659.0001): Damper - Forward Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1476M79P05 · May 29, 2026
- [AAP-3177487-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169754361520260623134833.0001): Setscrew. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3177487-1 · May 26, 2026
- [AAP-3177487-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169754361520260623134833.0001): Setscrew. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3177487-1 · May 26, 2026
- [340-084-104-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177357668320260506211035.0001): Bracket. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 340-084-104-0 · May 4, 2026
- [340-084-104-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177357668320260506211035.0001): Bracket. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 340-084-104-0 · May 4, 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
- [2949M03P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165472228620260225205426.0001): Blade Lock-Compressor Stg 8,9. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2949M03P01 · Feb 4, 2026
- [2949M03P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165472228620260225205426.0001): Blade Lock-Compressor Stg 8,9. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2949M03P01 · Feb 4, 2026
- [2684985JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180898542020260123155357.0001): Seal, Spring Loaded. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2684985 · Jan 22, 2026
- [2684985JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180898542020260123155357.0001): Seal, Spring Loaded. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2684985 · Jan 22, 2026
- [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
- [2502M08G01MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116108932520251216184607.0001): Bracket-Harness J10. Mitchell PMA, LLC · PMA PQ00057EB · Replaces 2502M08G01, 1894M80G01, 1896M53G01 · Nov 13, 2025
- [2502M08G01MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116108932520251216184607.0001): Bracket-Harness J10. Mitchell PMA, LLC · PMA PQ00057EB · Replaces 2502M08G01, 1894M80G01, 1896M53G01 · Nov 13, 2025
- [BLC2100M96P05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121701476220251205160851.0001): High Pressure Turbine, Blade, Stage 1. BELAC LLC (subsidiary of Chromalloy Gas Turbine LLC) · PMA PQ1667CE · Replaces 2100M96P05 · Oct 17, 2025
- [BLC2100M96P05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121701476220251205160851.0001): High Pressure Turbine, Blade, Stage 1. BELAC LLC (subsidiary of Chromalloy Gas Turbine LLC) · PMA PQ1667CE · Replaces 2100M96P05 · Oct 17, 2025
- [340-140-903-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196417412120250918135555.0001): Bracket Assy. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 340-140-903-0 · Sep 12, 2025
- [340-140-903-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196417412120250918135555.0001): Bracket Assy. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 340-140-903-0 · Sep 12, 2025

All of them: https://openairdocs.org/engine/cfm-international-cfm56-7b27-b3-series/pma.md

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