# N757QM: 1994 Boeing 757-29J

- Status: Valid registration
- Airframe: [Boeing 757-29J](https://openairdocs.org/model/boeing-757-29j) (registry code 1384942, 221 seats)
- Engine: [Pratt & Whitney PW2040](https://openairdocs.org/engine/pratt-whitney-pw2040) (registry code 52121)
- Data sheets: [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 27203
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 2015
- Certificate issued: December 19, 2014
- Expires: December 31, 2027
- Mode S code: AA3574
- Registered owners: [Aero Micronesia Inc DBA](https://openairdocs.org/faa-owner/AERO%20MICRONESIA%20INC%20DBA), [Asia Pacific Airlines](https://openairdocs.org/faa-owner/ASIA%20PACIFIC%20AIRLINES)
- Location: Barrigada, GU, Guam
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=757QM
- Page: https://openairdocs.org/aircraft/N757QM

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 15 in force

### Matched by airframe (Boeing 757-29J)

None in force.

### Matched by engine (Pratt & Whitney PW2040)

- [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

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N757QM.

## FAA accident and incident reports

None matched to N757QM.

## Service difficulty reports (244, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [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 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 I5PA2026062975708](https://openairdocs.org/sdr/I5PA2026062975708), Jun 29, 2026: EEC. FAULTED. LEFT ENGINE HIGH EGT. R & R LT ENGINE EEC IAW AMM.
- [SDR I5PA2026062675707](https://openairdocs.org/sdr/I5PA2026062675707), Jun 26, 2026: FMC. FAULTED. RIGHT FMC INOPERATIVE. R & R RT FMC IAW AMM. OPS CHKD NORMAL.
- [SDR I5PA2026062275706](https://openairdocs.org/sdr/I5PA2026062275706), Jun 23, 2026: PRESSURE SWITCH. FAULTED. FLIGHT MGE301, APU INFLIGHT START FAILED. FOUND APU DIFF PRESSURE SWITCH FAULTY. R & R DIFFERENTIAL PRESSURE SWITCH IAW AMM. OPS CHECK NORMAL, APU VERIFICATION 
- [SDR I5PA2026062275705](https://openairdocs.org/sdr/I5PA2026062275705), Jun 22, 2026: GCU. INOPERATIVE. RIGHT BUSS TIE LIGHT ILLUMINATED. R & R RT GCU IAW AMM OPS CHECK NORMAL.
- [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 I5PA2026061375703](https://openairdocs.org/sdr/I5PA2026061375703), Jun 13, 2026: GCU. INOPERATIVE. RIGHT BUSS TIE TRIPS WHEN POWER TRANSFERED. R & R RT GCU IAW AMM, OPS CHECKED NORMAL.
- [SDR I5PA2026061275702](https://openairdocs.org/sdr/I5PA2026061275702), Jun 12, 2026: FMC. INOPERATIVE. RIGHT FMC INOPERATIVE. R & R THE LT FMC IAW AMM. OPS CHECKED NORMAL.
- [SDR I5PA2026061275701](https://openairdocs.org/sdr/I5PA2026061275701), Jun 12, 2026: FMC. INOPERATIVE. LEFT FMC INOPERATIVE. R & R LT FMC IAW AMM. OPS CHECKED NORMAL.
- [SDR I5P2026F00000](https://openairdocs.org/sdr/I5P2026F00000), May 12, 2026: APU. INOPERATIVE. APU INOP. REPLACED APU PER TASK CARD.
- [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 I5PA2026042175702](https://openairdocs.org/sdr/I5PA2026042175702), Apr 21, 2026: SOLENOID. FAILED. PERFORMED APU BITE PER FIM. FOUND LOW OIL PRESS APU DE-OIL SOLENOID FAULTY. REPLACED SAME PER AMM. OPS AND LEAK CHECK OK. SUCCESSFUL APU INFLIGHT START PERFORME
- [SDR I5PA2026041875703](https://openairdocs.org/sdr/I5PA2026041875703), Apr 18, 2026: FLEX LINE. LEAKING. FLIGHT MGE601, AIR RETURN DUE LOW LEFT HYD QTY. FOUND HYD. FLEX LINE LEAK AT R MLG TILT ACTUATOR. R/R FLEX LINE AND SERVICED HYD. SYSTEM PER AMM. NO LEAKS DETEC
- [SDR I5PA2026041775702](https://openairdocs.org/sdr/I5PA2026041775702), Apr 17, 2026: APU. FAULTED. FLIGHT MGE301, APU INFLIGHT START FAILED. OPEN
- [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 I5PA2026033075711](https://openairdocs.org/sdr/I5PA2026033075711), Mar 30, 2026: DRIVE UNIT. FAILED. FLIGHT MGE301, WXR FAILED. REPLACED WXR DRIVE UNIT 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 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 I5PA2026031975708](https://openairdocs.org/sdr/I5PA2026031975708), Mar 19, 2026: STARTER. FAULTED. RIGHT ENGINE SLOW TO START. REPLACED RT ENGINE STARTER IAW AMM.
- [SDR I5PA2026031875707](https://openairdocs.org/sdr/I5PA2026031875707), Mar 18, 2026: WARNING MESSAGE. FALSE ACTIVATION. FLIGHT MGE400 - AIR RETURN. LT & RT EICAS COMPUTER STATUS MESSAGE. PERFORMED EICAS BITE, FOUND NUISANCE FAULTS. CLEARED FAULTS PER FIM. SWAPPED LT & RT COMPUTER
- [SDR I5PA2026031675706](https://openairdocs.org/sdr/I5PA2026031675706), Mar 15, 2026: TRANSCEIVER. FAULTY. FLIGHT MGE600, WXR FAIL. FOUND AND REPLACED FAULTY WXR TRANSCEIVER 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 I5PA2026031375704](https://openairdocs.org/sdr/I5PA2026031375704), Mar 12, 2026: FMC. INOPERATIVE. FLT MGE502, RT FMC INOP. REPLACED RH FMC PER AMM.
- [SDR I5PA2026031275703](https://openairdocs.org/sdr/I5PA2026031275703), Mar 12, 2026: CONTROLLER. INOPERATIVE. RIGHT PACK TEMP EICAS MESSAGE. REPLACED PACK TEMP CONTROLLER PER AMM. NO DEFECTS NOTED.
- [SDR I5PA2026031275702](https://openairdocs.org/sdr/I5PA2026031275702), Mar 12, 2026: DRIVE UNIT. INOPERATIVE. FLT. MGE502, WXR FAILED. PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM. FOUND DRIVE UNIT FAILED. REPLACED DRIVE UNIT PER AMM. NO DEFECTS NOTED.
- [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 I5PA2025101375702](https://openairdocs.org/sdr/I5PA2025101375702), Oct 13, 2025: ECU. FAULTY. APU PNEUMATICS INOPERATIVE. R & R APU ECU PER AMM. OPS CHECKED NORMAL.
- [SDR I5PA2025101375701](https://openairdocs.org/sdr/I5PA2025101375701), Oct 13, 2025: SHUTOFF VALVE. FAULTY. FLT: MGE831, APU FUEL VAL EICAS. R & R APU FUEL SHUTOFF VALVE IAW AMM, OPS CHECK NORMAL.
- [SDR I5PA2025070575701](https://openairdocs.org/sdr/I5PA2025070575701), Jul 5, 2025: SKIN. CORRODED. MAJOR REPAIR: LEVEL 2 CORROSION FOUND AT BSTA 680-700 BETWEEN STRINGERS 26R/28R. REPAIRED CORROSION PER EO APA-0043-001 REV 1 DTD 28JUN2025 AND PER SRM 53-00-01
- [SDR I5PA2025061675701](https://openairdocs.org/sdr/I5PA2025061675701), Jun 16, 2025: SMOKE DETECTOR. FAULTED. AIR RETURN DUE TO MAIN CARGO FIRE WARNING DURING CLIMBOUTFOLLOWED BY POPPED CB. QRH CONSULTED, ACFT RETURNED TO HNL. MX T/S PER PRECISION AMM AND FOUND FAULTY S
- [SDR I5PA2025053075702](https://openairdocs.org/sdr/I5PA2025053075702), May 30, 2025: BLADE. WORN. FLT: N/A (MX INSP.) ESI: RH ENG LPC 1ST STAGE BLADE #17 FOUND OUT OF LIMITS R/R #17 AND #35 FAN BLADES PER AMM NO DEFECTS NOTED.
- [SDR I5PA2025050675701](https://openairdocs.org/sdr/I5PA2025050675701), May 6, 2025: CONTROLLER. FAULTY. FLIGHT DECK TEMP HOT. R & R STBY PACK TEMP CONTROLLER PER AMM.
- [SDR I5PA2025042875701](https://openairdocs.org/sdr/I5PA2025042875701), Apr 28, 2025: EXCITER. FAULTED. FLT: MGE301. LH ENG DID NOT START ON IGNITOR 1 STARTED NORMAL ON BOTH. R/R LH ENG EXCITER 1 PER AMM.
- [SDR I5PA2025031575702](https://openairdocs.org/sdr/I5PA2025031575702), Mar 15, 2025: PILOT VALVE. FAULTY. FLT NO: N/A (MX INSP). ESI - PERFORMED RH ENG PNEUMATIC HEALTH CHECK. FOUND HS PILOT FAULTY. R/R RH ENG HS PILOT PER AMM 36-11-08. OPS CHECK NORMAL.
- [SDR I5PA2025031275701](https://openairdocs.org/sdr/I5PA2025031275701), Mar 12, 2025: PRESSURE SENSOR. FAULTED. FLT NO: MGE 401. ESI - APU SHUTDOWN 2X WHILE ENG STARTING. PERFORMED ECU BITE CHECK FOUND REVERSE FLOW MSG. R/R PRESSURE SENSOR PER AMM 49-61-04. OPS CHECK GOOD
- [SDR I5PA2025012575705](https://openairdocs.org/sdr/I5PA2025012575705), Jan 25, 2025: DISPLAY. INOPERATIVE. FLT NO: N/A (MX INSP) ESI - FO MCDU INOP. REMOVED AND REPLACED FO MCDU PER AMM.
- [SDR I5PA2025011775704](https://openairdocs.org/sdr/I5PA2025011775704), Jan 17, 2025: AUTOTHROTTLE SYS. MALFUNCTIONED. MGE 300, EVENT - AIR RETURN DUE TO NO LNAV/VNAV AND AUTO THROTTLE. DEFERRED LNAV / VNAV AND AUTO THROTTLE.
- [SDR I5PA2025012175703](https://openairdocs.org/sdr/I5PA2025012175703), Jan 17, 2025: FMC. INOPERATIVE. FLT NO: N/A, MX INSP, ESI - DISCREPANCY: LEFT FMC FAULT. SWAPPED LT AND RT FMC, FAULT FOLLOWED. PLACED RT FMC ON MEL. REMOVE AND REPLACED RT FMC PER AMM 34-61-0
- [SDR I5PA2025011275702](https://openairdocs.org/sdr/I5PA2025011275702), Jan 6, 2025: AUTOTHROTTLE SYS. INOPERATIVE. MGE 300 (EVENT) - AIR RETURN DUE TO: NO LNAV/VNAV, NO AUTO THROTTLE NO TMC INFO.
- [SDR I5PA2025010475701](https://openairdocs.org/sdr/I5PA2025010475701), Jan 4, 2025: FMC. FAULTED. FLT NO. MGE 300 (EVENT). AIR RETURN DUE TO: NO INFO ON PROGRESS PAGE BURN, TIME WIND UNABLE TO MAINTAIN COURSE. TEMP SELECT FOR THROTTLES INOP. NO LNAV / VNAV. 
- [SDR I5PA2024122375702](https://openairdocs.org/sdr/I5PA2024122375702), Dec 23, 2024: CONTROL VALVE. FAULTED. LH ENG STARTER VALVE DOESNT OPEN WHEN SWITCHED TO RUN. R/R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.
- [SDR I5PA2024121975701](https://openairdocs.org/sdr/I5PA2024121975701), Dec 19, 2024: SURGE VALVE. FAULTED. APU AUTO SHUTDOWN ON ENG START. REPLACED APU SURGE VALVE PER AMM 49-52-00
- [SDR I5PA2024112275704](https://openairdocs.org/sdr/I5PA2024112275704), Nov 22, 2024: CONTROL VALVE. FAULTED. EPCS FAULT MESSAGE HCC/EEC. R/R ACTIVE CLEARANCE CONTROL VALVE IAW AMM 72-53-90/601.
- [SDR I5PA2024112275703](https://openairdocs.org/sdr/I5PA2024112275703), Nov 22, 2024: CONTROL VALVE. FAULTY. LEFT ENG STARTER VALVE TAKES LONG TO CLOSE AFTER ENG START UP. R & R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.
- [SDR I5PA2024111375702](https://openairdocs.org/sdr/I5PA2024111375702), Nov 13, 2024: ECU. INOPERATIVE. APU ELECTRICAL LOAD FLUCTUATES. REPLACED APU ECU PER AMM. OPS CHECK GOOD.
- [SDR I5PA2024110375701](https://openairdocs.org/sdr/I5PA2024110375701), Nov 3, 2024: COMPUTER. INTERMITTENT. FLT NO: MGE305 - EVENT (ETOPS- AIR RETURN) MULTIPLE EICAS MESSAGES. PERFORMED FIM AND FOUND LEFT EICAS COMPUTER INTERMITTENT. REPLACED LEFT EICAS COMPUTER PER A
- [SDR I5PA2024102075704](https://openairdocs.org/sdr/I5PA2024102075704), Oct 20, 2024: SKIN. CORRODED. DURING C CHECK, CORROSION WAS FOUND ON THE RH WING LOWER SKIN AT WS 187-211. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.
- [SDR I5PA2024102075703](https://openairdocs.org/sdr/I5PA2024102075703), Oct 20, 2024: SKIN. CORRODED. DURING C CHECK, CORROSION WAS FOUND ON THE LH WING LOWER SKIN AT WS 187-213. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.
- [SDR I5PA2024102075702](https://openairdocs.org/sdr/I5PA2024102075702), Oct 20, 2024: STRUCTURE. CORRODED. DURING C CHECK, CORROSION WAS FOUND ON THE RH HORIZONTAL STAB BETWEEN STA 116.25-122.428, 140.25-148.48,153.61-156.17,164.53-174.10,176.299-180.10, 183.30-189.8

All 244: https://openairdocs.org/aircraft/N757QM/reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N757QM

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N757QM before.

- [Cancelled 1994-02-04](https://openairdocs.org/deregistered/N757QM-1994-02-04): Cessna R182, S/N R18201257. Exported to Canada. Owner: [B T Carolina Land Corp](https://openairdocs.org/faa-owner/B%20T%20CAROLINA%20LAND%20CORP), [Rutherfordton, NC](https://openairdocs.org/faa-place/NC/Rutherfordton)

## Related

- Other Boeing 757-29J aircraft: https://openairdocs.org/model/boeing-757-29j/aircraft.md
- The Pratt & Whitney PW2040 engine: https://openairdocs.org/engine/pratt-whitney-pw2040.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
