# Boeing 757-29J - Type: Aircraft model (FAA registry) - Registry code: 1384942 - Manufacturer (registry): BOEING - Model: 757-29J - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 221 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-757-29j Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N757QM](https://openairdocs.org/aircraft/N757QM): [Aero Micronesia Inc DBA](https://openairdocs.org/faa-owner/AERO%20MICRONESIA%20INC%20DBA), [Barrigada, GU](https://openairdocs.org/faa-place/GU/Barrigada), built 1994, S/N 27203 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (245, newest 50) As reported by operators and repair stations, by the model named in the report. - [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 245: https://openairdocs.org/model/boeing-757-29j/reports.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.