# Pratt & Whitney PW2037(M)

- Type: Engine model (FAA registry)
- Registry code: 51511
- Manufacturer (registry): P & W
- Model: PW2037(M)
- Engine type: Turbo-fan
- Power: 37,530 lb thrust
- Data sheet: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (OpenAirDocs)
- Holder: Pratt & Whitney
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-pw2037-m

Model codes come from the FAA registry's reference file.

## 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 2026-07-06](https://openairdocs.org/ad/2026-07-06): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 3 more. Effective May 29, 2026
- [AD 2024-12-04](https://openairdocs.org/ad/2024-12-04): Turbine Section · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Aug 13, 2024
- [AD 2021-14-13](https://openairdocs.org/ad/2021-14-13): Turbine Section · Pratt & Whitney F117-PW-100, PW2037, PW2037M and 1 more. Effective Sep 1, 2021
- [AD 2019-05-01](https://openairdocs.org/ad/2019-05-01): Turbine/Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Apr 16, 2019
- [AD 2018-22-06](https://openairdocs.org/ad/2018-22-06): Fuel Control/Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Dec 3, 2018
- [AD 2018-14-10](https://openairdocs.org/ad/2018-14-10): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Sep 28, 2018
- [AD 2012-02-01](https://openairdocs.org/ad/2012-02-01): Fan blades · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Apr 24, 2012
- [AD 2009-14-05](https://openairdocs.org/ad/2009-14-05): High-pressure compressor (HPC) · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jul 23, 2009
- [AD 2009-10-08](https://openairdocs.org/ad/2009-10-08): High-pressure turbine 2nd stage hubs that have previously been exposed to Pratt & Whitney cleaning procedure SPOP 10 or SPOP 9 or equivalent procedure. · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Jun 17, 2009
- [AD 2007-02-06](https://openairdocs.org/ad/2007-02-06): High pressure compressor (HPC) drum rotor disk assemblies · Pratt & Whitney Division PW2037, PW2037M and PW2040. Effective Feb 28, 2007
- [AD 2005-18-03](https://openairdocs.org/ad/2005-18-03): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division PW2037, PW2037D, PW2037M and 5 more. Effective Feb 28, 2006
- [AD 99-20-03](https://openairdocs.org/ad/99-20-03): High Pressure Turbine Disks · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 23, 1999
- [AD 96-18-08 R1](https://openairdocs.org/ad/96-18-08-R1): (HPT) High Pressure or (LPT) Low Pressure Turbine · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 2 more. Effective Nov 10, 1998
- [AD 97-11-51 R1](https://openairdocs.org/ad/97-11-51-R1): First Stage High Pressure Turbine (HPT) Disk Assembly · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Aug 7, 1997
- [AD 88-03-52](https://openairdocs.org/ad/88-03-52): Fuel Quantity Indication System · Pratt & Whitney Division PW2037 and PW2040. Effective Jul 13, 1988

Historical (superseded or no longer in force):

- [AD 2017-12-03](https://openairdocs.org/ad/2017-12-03) (historical): Fuel Control Turbine Engines · Pratt & Whitney PW2037, PW2037M and PW2040. Effective Jul 20, 2017
- [AD 2017-11-06](https://openairdocs.org/ad/2017-11-06) (historical): Turbine/ Turboprop Engine · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 6 more. Effective Jul 18, 2017
- [AD 2014-05-32](https://openairdocs.org/ad/2014-05-32) (historical): Diffuser-to-high-pressure turbine (HPT) case flange · Pratt & Whitney F117-PW-100, PW2037, PW2037D and 8 more. Effective May 5, 2014
- [AD 2002-12-06](https://openairdocs.org/ad/2002-12-06) (historical): Time Limits Section (TLS) · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jul 17, 2002
- [AD 2000-21-09](https://openairdocs.org/ad/2000-21-09) (historical): Critical Life-limited Parts · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective Jan 22, 2001
- [AD 99-08-14](https://openairdocs.org/ad/99-08-14) (historical): Maintenance Program, Mandatory Inspections · Pratt & Whitney Division PW2037, PW2037M, PW2040 and 5 more. Effective May 13, 1999

## Registered aircraft (1)

- [N752CS](https://openairdocs.org/aircraft/N752CS): [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 2002, S/N 30046

## NTSB investigations

None matched to aircraft with this engine model.

## 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 19990510017349I](https://openairdocs.org/incident/19990510017349I), May 10, 1999: Boeing 757222 (N587UA), Syracuse, NY. On may 10, 1999 at 1000 EST, a Boeing 757-222, s/n 26713, N587UA, registered to united airlines, inc., twenty minutes after takeoff in stabilized climb passing…

## Service difficulty reports (12,807, newest 50)

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

- [SDR I5PA2026101488801](https://openairdocs.org/sdr/I5PA2026101488801), Oct 14, 2026: CHIP DETECTOR. DAMAGED. ETOPS SIGNIFICANT REPORT, FOUND CHIP DETECTOR ON THE OIL SCAVENGE LINE FROM THE ANGLE GEARBOX ON THE LT ENGINE DAMAGED. REPLACED THE CHIP DETECTOR IAW AMM.
- [SDR DALA2026100605523](https://openairdocs.org/sdr/DALA2026100605523), Oct 4, 2026: ENGINE. MAKING METAL. IFSD/DIV- AIRCRAFT DIVERTED TO BZE DUE TO LEFT ENGINE OIL FILTER MESSAGE. FLIGHT CREW FOLLOWED QRH AND SHUTDOWN ENGINE. METAL FOUND ON MCDS AND OIL FILTER, REPL
- [SDR DALA2026092805377](https://openairdocs.org/sdr/DALA2026092805377), Sep 23, 2026: OIL SYSTEM. LEAKING. ATB- DUE ODOR IN THE FLIGHT DECK DURING CLIMB. REPLACED LEFT ENGINE. REMOVED OIL CONTAMINATION FROM PACK AND PNEUM SYSTEM. REPLACE BOTH RECIRC FILTER. OPS NORMA
- [SDR I5PA2026092288807](https://openairdocs.org/sdr/I5PA2026092288807), Sep 22, 2026: PROBE. DAMAGED. ETOPS SIGNIFICANT REPORT, RT ENGINE EGT WENT BLANK. REPLACED RH EGT PROBE IAW AMM DUE TO FINDING ONE LOOSE STUD DURING INSPECTION.
- [SDR I5PA2026092168812](https://openairdocs.org/sdr/I5PA2026092168812), Sep 21, 2026: VALVE. FAULTY. ETOPS SIGNIFICANT REPORT, LT ENGINE PNEUMATIC HEALTH CHECK REQUIRED - PERFORMED PNEUMATIC HEALTH CHECK PER AMM, FOUND HPSOV FAULTY. REPLACED HPSOV PER AMM
- [SDR I5PA2026091688806](https://openairdocs.org/sdr/I5PA2026091688806), Sep 16, 2026: SENSOR. INOPERATIVE. ETOPS SIGNIFICANT REPORT - RH PRI/SEC T2 OR ADC/EEC EPCS STATUS MESSAGE DISPLAYED - REPLACED RIGHT ENGINE PTS SENSOR PER AMM
- [SDR I5PA2026091688805](https://openairdocs.org/sdr/I5PA2026091688805), Sep 15, 2026: BLADE. DAMAGED. ETOPS - RH ENGINE FAN BLADE NUMBER 16 FOUND WITH A TEAR ON THE LEADING EDGE - REPLACED FAN BLADE 16 AND 34 PER AMM AS A MATCHED MOMENT WEIGHT
- [SDR DALA2026091605170](https://openairdocs.org/sdr/DALA2026091605170), Sep 11, 2026: SHUTOFF VALVE. FAULTED. ATB- DUE TO CABIN ALT WARNING CAUSED FROM LEFT BLEED TRIP CAUSING LEFT PACK OFF WITH RIGHT PACK ON MEL. O2 MASKS DEPLOYED. REPLACED HPSOV. REPLACED FAN AIR TEMP
- [SDR DALA2026091605171](https://openairdocs.org/sdr/DALA2026091605171), Sep 11, 2026: PUMP. FAULTED. DECLARED AN EMERGENCY AND DIVERTED TO LAS DUE TO LEFT ENGINE OIL TEMP IN THE AMBER BAND DURING CLIMB. REPLACED LEFT OIL PUMP, AIR OIL COOLER, FUEL OIL HEAT EXCH
- [SDR I5PA2026090968805](https://openairdocs.org/sdr/I5PA2026090968805), Sep 9, 2026: CHIP DETECTOR. MISSING. ETOPS SIGNIFICANT REPORT. RT ENGINE CHIP DETECTOR MISSING DURING INSPECTION. REPLACED RT CHIP DETECTOR IAW APPLICABLE AMM
- [SDR I5PA2026090888802](https://openairdocs.org/sdr/I5PA2026090888802), Sep 8, 2026: IDG. INOPERATIVE. TOPS SIGNIFICANT REPORT. LEFT IDG INOPERATIVE, ON MEL. REPLACED LH IDG PER APPLICABLE AMM
- [SDR I5PA2026083068807](https://openairdocs.org/sdr/I5PA2026083068807), Aug 30, 2026: IGNITER. WORN. ETOPS SIGNIFICANT REPORT, RT ENGINE UPPER IGNITER PLUG WORN. REPLACED IGNITER PLUG IAW AMM.
- [SDR I5PA2026083068808](https://openairdocs.org/sdr/I5PA2026083068808), Aug 30, 2026: CIRCUIT CARD. INOPERATIVE. ETOPS SIGNIFICANT REPORT, LT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED AFOLTS NR 1 CARD IAW AMM.
- [SDR DALA2026080404481](https://openairdocs.org/sdr/DALA2026080404481), Aug 1, 2026: TUBE. LEAKING. DECLARED EMERGENCY FOR RIGHT ENGINE ENCOUNTERED A LOSS OF OIL QUANTITY IN FLIGHT. THE LOW PRESSURE LIGHT ILLUMINATED, OIL PRESSURE MAINTAINED WITHIN THE YELLOW 
- [SDR DALA2026080404482](https://openairdocs.org/sdr/DALA2026080404482), Jul 30, 2026: ENGINE. FIRE. FLIGHT CREW PERFORMING AIR TURN BACK DUE TO LEFT ENGINE FIRE INDICATION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO COMBUSTOR CASE (APPROXIMATELY 12 O'CLOCK POSI
- [SDR DALA2026073104430](https://openairdocs.org/sdr/DALA2026073104430), Jul 24, 2026: COMBUSTION CASE. DAMAGED. ATB, IFSD - FLIGHT CREW PERFORMING AIR TURN BACK DUE TO LEFT ENGINE FIRE INDICATION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO COMBUSTOR CASE (APPROXIMATELY 12 
- [SDR DALA2026071704229](https://openairdocs.org/sdr/DALA2026071704229), Jul 16, 2026: ENGINE. HUNG START. HUNG START ON #1 ENGINE N2 38% GROUND CREW REPORTED SMOKE AND FIRE, QRH RAN FOR POSSIBLE TAIL PIPE FIRE AND ABORTED ENGINE START. REPLACED STARTER IAW AMM 80-11
- [SDR I5PA2026071575701](https://openairdocs.org/sdr/I5PA2026071575701), Jul 15, 2026: PILOT VALVE. INOPERATIVE. FLIGHT 305, RT ENG BLEED ISSUES. R & R RT ENG HS PILOT IAW AMM, OPS CHKD NORMAL.
- [SDR I5PA2026071575702](https://openairdocs.org/sdr/I5PA2026071575702), Jul 15, 2026: SHUTOFF VALVE. INOPERATIVE. FLIGHT 305, RT ENG BLEED ISSUES. R & R RT ENG HPSOV PER AMM OPS CHECK NORMAL.
- [SDR I5PA2026071088801](https://openairdocs.org/sdr/I5PA2026071088801), Jul 10, 2026: LDVT. FAULTY. DEFERRED LT THRUST REVERSER DUE TO LT ENG REVERSER, LT ENG SEC CONT STATUS MSG. R & R LT ENG LDVT IAW AMM, OPS CHKD NORMAL.
- [SDR DALA2026070703948](https://openairdocs.org/sdr/DALA2026070703948), Jul 3, 2026: PUMP. FAULTED. ATO- DISCONTINUED TAKEOFF AT 40 KNOTS DUE TO NO ACCELERATION RIGHT ENGINE. INSPECTED 2.5 BLEED SYSTEM WITH NTF. REPLACED FUEL PUMP, FUEL CONTROL, EEC, AND 14TH 
- [SDR I5PA2026062975708](https://openairdocs.org/sdr/I5PA2026062975708), Jun 29, 2026: EEC. FAULTED. LEFT ENGINE HIGH EGT. R & R LT ENGINE EEC IAW AMM.
- [SDR I5PA2026062275704](https://openairdocs.org/sdr/I5PA2026062275704), Jun 22, 2026: IDG. INOPERATIVE. RIGHT ENG IDG INOPERATIVE. (DEFERRED PER MEL 24-00-01). R & R RT ENG IDG IAW AMM, OPS CHKD NORMAL.
- [SDR DALA2026061603614](https://openairdocs.org/sdr/DALA2026061603614), Jun 14, 2026: IGNITER. FAULTY. ABORTED ENGINE START RIGHT ENGINE, STRONG FUEL SMELL IN CABIN. MAINT ADVISED START AGAIN ON BOTH IGNITORS, WITH NORMAL START INDICATIONS, AGIN STRONG FUEL SMELL
- [SDR DALA2026060603411](https://openairdocs.org/sdr/DALA2026060603411), Jun 6, 2026: ENGINE. POWER LOSS. ATO- DISCONTINUED TAKEOFF AT 15 KNOTS DUE TO NO ACCEL ON THE RIGHT ENGINE. REPLACED RIGHT ENGINE. (LP 6457816, 1630475 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060503403](https://openairdocs.org/sdr/DALA2026060503403), Jun 4, 2026: OIL COOLER. ODOR. CREW REPORTED EXHAUST ODOR IN AFT CABIN ON TAKEOFF AND TOP OF DESCENT. EMERGENCY DECLARED DURING APPROACH. ROAD TRIP. REPLACED AIR/OIL COOLER. (LP 8075720, 1628
- [SDR DALA2026050602879](https://openairdocs.org/sdr/DALA2026050602879), May 5, 2026: SENSOR. LEAKING. AIRCRAFT DIVERTED TO MCO DUE TO LEFT ENGINE IFSD DUE TO ZERO OIL PRESSURE AND OIL QUANTITY. FOUND OIL TEMP SENSOR LEAKING AND PACKING DETERIORATED. COMPLETED WI
- [SDR I5PA2026042175704](https://openairdocs.org/sdr/I5PA2026042175704), Apr 21, 2026: EEC. FAULTY. FLIGHT MGE601. LT ENG LOW OIL PRESS AFTER LANDING. FOUND FAULTY EEC. R/R LH ENG EEC PER AMM, OPS CHECK NORMAL.
- [SDR I5PA2026040875701](https://openairdocs.org/sdr/I5PA2026040875701), Apr 8, 2026: SHAFT. SHEARED. LEFT ENG HYDRAULIC PUMP. LEFT ENG EDP SHAFT FOUND SHEARED. R/R LEFT ENG EDP PER AMM. OPS CHECK, LEAK CHECK OK.
- [SDR I5PA2026033075709](https://openairdocs.org/sdr/I5PA2026033075709), Mar 30, 2026: FUEL CONTROL. FAULTED. FLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND FCU/EEC EPCS MESSAGE, REPLACED FCU PER AMM.
- [SDR I5PA2026033075710](https://openairdocs.org/sdr/I5PA2026033075710), Mar 30, 2026: IGNITER. WORN. FLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND UPPER IGNITER PLUG WORN TO LIMITS. REPLACED IGNITER PLUG PER AMM.
- [SDR I5PA2026031975708](https://openairdocs.org/sdr/I5PA2026031975708), Mar 19, 2026: STARTER. FAULTED. RIGHT ENGINE SLOW TO START. REPLACED RT ENGINE STARTER IAW AMM.
- [SDR DALA2026031801876](https://openairdocs.org/sdr/DALA2026031801876), Mar 17, 2026: EEC. FAILED. ATO- DISCONTINUED TAKEOFF AROUND 40 KNOTS DUE TO LEFT ENGINE FAILURE. FOUND EPCS P EEC AND P 275-16, INSP AND CLEANED EEC PB SENSE SYS AND R & R EEC.
- [SDR DALA2026031801878](https://openairdocs.org/sdr/DALA2026031801878), Mar 17, 2026: PUMP. ODOR. STRANGE ODOR IN THE COCKPIT WHEN DESCENDING THROUGH 10,000 FT ON TWO CONSECUTIVE LEGS. R&R NR 1 ENG LUBE & SCAVENGE PUMP IAW B757 AMM 79 -21-04. PERFORMED TEST 
- [SDR I5PA2026031588802](https://openairdocs.org/sdr/I5PA2026031588802), Mar 15, 2026: START VALVE. INOPERATIVE. RIGHT ENGINE START VALVE FAILED TO OPEN. REPLACED RIGHT ENGINE START VALVE PER AMM.
- [SDR I5PA2026031588803](https://openairdocs.org/sdr/I5PA2026031588803), Mar 15, 2026: STARTER. INOPERATIVE. RIGHT ENGINE SLOW TO START. REPLACED RIGHT ENGINE STARTER PER AMM.
- [SDR I5PA2026031575705](https://openairdocs.org/sdr/I5PA2026031575705), Mar 15, 2026: CONVERTER. LEAKING. FLIGHT MGE600 - ESI / (AIR RETURN) RIGHT ENGINE BLEED OFF MESSAGE ON T/O. NO DUCT PRESSURE ON RIGHT SIDE. PERFORMED FIM, FOUND RFCC LEAKING. REPLACED RFCC IAW A
- [SDR I5PA2026031075701](https://openairdocs.org/sdr/I5PA2026031075701), Mar 10, 2026: TRANSMITTER. INTERMITTENT. RIGHT ENGINE FUEL FLOW INDICATION INTERMITTENT. REPLACED FUEL FLOW TRANSMITTER IAW AMM.
- [SDR I5PA2026013068803](https://openairdocs.org/sdr/I5PA2026013068803), Jan 30, 2026: PILOT VALVE. FAULTED. DEFERRED RT ENG HPSOV IAW MEL 36-11-02. R & R RT ENG HIGH STAGE PILOT PER AMM 36-11-08.
- [SDR DALA2026013000727](https://openairdocs.org/sdr/DALA2026013000727), Jan 29, 2026: FUEL CONTROL. FAULTED. DURING LEFT ENGINE START, LEFT ENGINE EXPERIENCED A TAIL PIPE FIRE. FLIGHT CREW FOLLOWED QRH. ARFF RESPONDED AND SPRAYED WATER ON THE ENGINE. FOUND P/S PDIU/EEC
- [SDR I5PA2026020188801](https://openairdocs.org/sdr/I5PA2026020188801), Jan 29, 2026: PUMP. LEAKING. MX FOUND HYD LEAK AT THE RT ENG. R & R THE RT ENGINE EDP IAW AMM 29-11-05.
- [SDR DALA2026012700634](https://openairdocs.org/sdr/DALA2026012700634), Jan 26, 2026: STARTER. FAILED. FLAMES & SPARKS COMING FROM THE RT ENGINE DURING TAKEOFF. ACCOMPANIED BY FUMES IN REAR CABIN, CONFIRMED BY FA'S. INSPECTED NR 2 ENGINE FOR DAMAGE, NO TROUBLE FO
- [SDR I5PA2026011988801](https://openairdocs.org/sdr/I5PA2026011988801), Jan 18, 2026: ANTI-ICE VALVE. STICKING. LEFT ENG ANTI-ICE VALVE STICKING. R & R LT ENG ANTI-ICE VALVE IAW AMM 30-21-03. OP CHECKED NORMAL.
- [SDR DALA2026012000420](https://openairdocs.org/sdr/DALA2026012000420), Jan 17, 2026: BUSHING. MISSING. NUMBER 2 ENGINE PYLON BULKHEAD, AFT ENGINE MOUNT FORWARD SHEAR PIN BUSHING NOT INSTALLED. PERFORMED FPI ON AFT ENGINE MOUNT FORWARD SHEAR PIN BORE REF. SOPM 20-
- [SDR DALA2025123009523](https://openairdocs.org/sdr/DALA2025123009523), Dec 29, 2025: FUEL CONTROL. FAULTED. ATB/DE, LEFT ENGINE COMPRESSOR STALL DURING CLIMB. PULLED THROTTLES BACK AND ENGINE WAS STABLE. BORESCOPE COMPLETED WITH NO FINDINGS, REPLACED FCU.
- [SDR DALA2025122909481](https://openairdocs.org/sdr/DALA2025122909481), Dec 25, 2025: OIL SYSTEM. LOW PRESSURE. ATB/IFSD/DE - AIRCRAFT RETURNED TO DTW DUE TO RIGHT ENGINE IFSD DUE TO ZERO OIL PRESSURE AND OIL QUANTITY. RIGHT ENGINE OPERATED ABOVE IDLE POWER WITH ZERO OIL 
- [SDR DALA2025121609174](https://openairdocs.org/sdr/DALA2025121609174), Dec 13, 2025: FUEL CONTROL. FAULTED. MISC/DE INTO ATL DUE TO RIGHT ENGINE INDICATION FLUX. REPLACED FUEL CONTROL UNIT AND 14TH STAGE BLEED CONVERTER VALVE.
- [SDR I5PA2025111688801](https://openairdocs.org/sdr/I5PA2025111688801), Nov 16, 2025: OIL SYSTEM. LOW PRESSURE. MGE305 (N888LT) DECLARED AN EMERGENCY DUE TO LOSS OF OIL QUANTITY AND PRESSURE ON THE LEFT ENGINE JUST PRIOR TO TOP OF DESCENT. ACFT LANDED SAFELY WITHOUT FURTH
- [SDR DALA2025102207745](https://openairdocs.org/sdr/DALA2025102207745), Oct 22, 2025: ENGINE. MAKING METAL. IFSD/DIV/DE- DIVERTED TO SAL DUE TO LEFT ENGINE FAILURE. MAINTENANCE FOUND METAL ON CHIP DETECTORS, REMOVED AND REPLACED ENGINE.
- [SDR I5PA2025091768801](https://openairdocs.org/sdr/I5PA2025091768801), Sep 17, 2025: IGNITION LEAD. DAMAGED. RIGHT ENGINE IGNITION SYSTEM 1 INOP. PERFORMED FIM, FOUND SYSTEM 1 IGNITION LEAD DAMAGED. REPLACED IGNITION LEAD PER APPLICABLE AMM.

All 12,807: https://openairdocs.org/engine/pratt-whitney-pw2037-m/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.

- [1B2288-01SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190148212520260706131539.0001): Vent Plug. Seal Dynamics Inc · PMA PQ1715CE · Replaces 1B2288-01 · Jun 30, 2026
- [E1B8815-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197436224520260726233110.0001): Blade–HPC, 15Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-01 · Jun 24, 2026
- [E1B8817-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194359014220260726233112.0001): Blade–HPC, 17Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-04 · Jun 24, 2026
- [E1B8806](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192190687020260726233104.0001): Blade–HPC, 6Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8806 · Jun 24, 2026
- [E1B8815-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184051224720260726233110.0001): Blade–HPC, 15Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-04 · Jun 24, 2026
- [E1B8808](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180225802120260726233105.0001): Blade–HPC, 8Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8808 · Jun 24, 2026
- [E1B8815-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177720889720260726233110.0001): Blade–HPC, 15Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-03 · Jun 24, 2026
- [E1B8811-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177138863620260726233106.0001): Blade–HPC, 11Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8811-03 · Jun 24, 2026
- [E1B8815-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177006281920260726233110.0001): Blade–HPC, 15Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-02 · Jun 24, 2026
- [E1B8817-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175744069120260726233112.0001): Blade–HPC, 17Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-03 · Jun 24, 2026
- [E1B8812-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174627132720260726233107.0001): Blade–HPC, 12Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B88012-03 · Jun 24, 2026
- [E1B8813-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171624088120260726233108.0001): Blade–HPC, 13Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-01 · Jun 24, 2026
- [E1B8807](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157878584720260726233105.0001): Blade–HPC, 7Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8807 · Jun 24, 2026
- [E1B8812-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153040098920260726233107.0001): Blade–HPC, 12Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8812-01 · Jun 24, 2026
- [E1B8810](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152393883220260726233105.0001): Blade–HPC, 10Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8810 · Jun 24, 2026
- [E1B8809](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148836907320260726233105.0001): Blade–HPC, 9Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8809 · Jun 24, 2026
- [E1B8814-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144884370720260726233109.0001): Blade–HPC, 14Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-01 · Jun 24, 2026
- [E1B8816-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139083303120260726233111.0001): Blade–HPC, 16Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-02 · Jun 24, 2026
- [E1B8814-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133276121420260726233109.0001): Blade–HPC, 14Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-02 · Jun 24, 2026
- [E1B8816-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133057649020260726233111.0001): Blade–HPC, 16Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-03 · Jun 24, 2026
- [E1B8813-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132529092120260726233108.0001): Blade–HPC, 13Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-02 · Jun 24, 2026
- [E1B8812-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126543570220260726233107.0001): Blade–HPC, 12Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8812-04 · Jun 24, 2026
- [E1B8812-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122532033220260726233107.0001): Blade–HPC, 12Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B88012-02 · Jun 24, 2026
- [E1B8816-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120085852320260726233111.0001): Blade–HPC, 16Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-04 · Jun 24, 2026
- [E1B8814-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119159325320260726233109.0001): Blade–HPC, 14Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-03 · Jun 24, 2026
- [E1B8811-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117213964020260726233106.0001): Blade–HPC, 11Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8811-04 · Jun 24, 2026
- [E1B8817-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116299840320260726233112.0001): Blade–HPC, 17Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-03 · Jun 24, 2026
- [E1B8814-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116131008120260726233109.0001): Blade–HPC, 14Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-04 · Jun 24, 2026
- [E1B8817-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112048685420260726233112.0001): Blade–HPC, 17Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-01 · Jun 24, 2026
- [E1B8811-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111222754220260726233106.0001): Blade–HPC,11Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8811-01 · Jun 24, 2026
- [E1B8811-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110553377220260726233106.0001): Blade–HPC, 11Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8811-02 · Jun 24, 2026
- [E1B8813-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109773690820260726233108.0001): Blade–HPC, 13Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-04 · Jun 24, 2026
- [E1B8813-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108311965720260726233108.0001): Blade–HPC, 13Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-03 · Jun 24, 2026
- [E1B8816-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104959223820260726233111.0001): Blade–HPC, 16Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-01 · Jun 24, 2026
- [E1B8810](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199390619220260508164156.0001): Blade– HPC, 10 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8810 · Apr 30, 2026
- [E1B8811-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199101444020260508164156.0001): Blade– HPC, 11 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8811-01 · Apr 30, 2026
- [E1B8817-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194482782820260508164203.0001): Blade– HPC, 17 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-03 · Apr 30, 2026
- [E1B8817-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194244228720260508164203.0001): Blade– HPC, 17 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-04 · Apr 30, 2026
- [E1B8808](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193521795320260508164155.0001): Blade– HPC, 8 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8808 · Apr 30, 2026
- [E1B8817-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192953766720260508164203.0001): Blade– HPC, 17 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8817-02 · Apr 30, 2026
- [E1B8816-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191831662720260508164202.0001): Blade– HPC, 16 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-02 · Apr 30, 2026
- [E1B8814-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191700136220260508164159.0001): Blade– HPC, 14 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-01 · Apr 30, 2026
- [E1B8814-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191643355820260508164200.0001): Blade– HPC, 14 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8814-04 · Apr 30, 2026
- [E1B8813-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187553614020260508164158.0001): Blade– HPC, 13 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-01 · Apr 30, 2026
- [E1B8813-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187094824920260508164159.0001): Blade– HPC, 13 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8813-03 · Apr 30, 2026
- [E1B8816-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184823072120260508164202.0001): Blade– HPC, 16 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-03 · Apr 30, 2026
- [E1B8812-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182221643420260508164157.0001): Blade– HPC, 12 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8812-02 · Apr 30, 2026
- [E1B8815-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174996665720260508164201.0001): Blade– HPC, 15 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-03 · Apr 30, 2026
- [E1B8816-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169754645820260508164202.0001): Blade– HPC, 16 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8816-01 · Apr 30, 2026
- [E1B8815-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164428663020260508164201.0001): Blade– HPC, 15 Stage, Coated. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 1B8815-02 · Apr 30, 2026

All of them: https://openairdocs.org/engine/pratt-whitney-pw2037-m/pma.md

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