# Boeing 757-2G5

- Type: Aircraft model (FAA registry)
- Registry code: 1384912
- Manufacturer (registry): BOEING
- Model: 757-2G5
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 239
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 5
- Page: https://openairdocs.org/model/boeing-757-2g5

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 (5)

- [N111AS](https://openairdocs.org/aircraft/N111AS): [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables), S/N 29488
- [N489BR](https://openairdocs.org/aircraft/N489BR): [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Doral, FL](https://openairdocs.org/faa-place/FL/Doral), S/N 29489
- [N943FD](https://openairdocs.org/aircraft/N943FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1987, S/N 23929
- [N944FD](https://openairdocs.org/aircraft/N944FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1989, S/N 24497
- [N962FD](https://openairdocs.org/aircraft/N962FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1988, S/N 24176

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (556, newest 50)

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

- [SDR FDEA202610121559](https://openairdocs.org/sdr/FDEA202610121559), Oct 12, 2026: SKIN. CORRODED. LEFT WING INBD FLAP UPPER SURFACE O/B SIDE EXTERNAL SKIN SOME AREA WITH CORROSION. LT WING I/B FLAP UPPER SURFACE O/B SIDE WAS REPAIRED IAW B757 SRM 57-53-01-2R
- [SDR FDEA202610091536](https://openairdocs.org/sdr/FDEA202610091536), Oct 9, 2026: FLOORBEAM. CORRODED. MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 24LBL TO 0BL SOME AREAS WITH CORROSION. AREA OUT OF LIMITS WAS REPAIRED AT MAIN CARGO COMPARTMENT FLOORBEAM BS 
- [SDR FDEA202610051478](https://openairdocs.org/sdr/FDEA202610051478), Oct 5, 2026: SKIN. DELAMINATED. TWO INDICATIONS OF DISBOND WERE FOUND OVER TWO DENTS ON THE UPPER SKIN OF THE LEFT ELEVATOR: ONE AT ELEV STA 107.360, 1.800 INCHES IN DIAMETER AND 13.5 INCHES F
- [SDR FDEA202607220987](https://openairdocs.org/sdr/FDEA202607220987), Jul 22, 2026: FITTING. CRACKED. CRACK FOUND ON #2 ENGINE LOWER OUTBD MIDSPAR BULKHEAD FITTING. REPAIRED OUTBD MIDSPAR BULKHEAD FITTNG IAW EA F-5450-T0387823 PT1, NACELLS / PYLON - WING PYLON /
- [SDR FDEA202607030828](https://openairdocs.org/sdr/FDEA202607030828), Jul 3, 2026: DOOR. UNSECURE. COULD NOT GET R1 DOOR SLIDE LIGHT TO ILLUMINATE WHEN CLOSING DOOR. WHILE APPROACHING AIRCRAFT NOTED R1 DOOR NOT COMPLETELY CLOSED. CYCLED DOOR AND ARMED SLIDE, 
- [SDR IXXA20260501001](https://openairdocs.org/sdr/IXXA20260501001), May 6, 2026: SKIN. CORRODED. CORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKIN
- [SDR IXXA20260424001](https://openairdocs.org/sdr/IXXA20260424001), Apr 21, 2026: BRACKET. CORRODED. LEFT WHEEL WELL ON THE H BEAM IS A HYDRAULIC LINE B NUT THATS SITTING RIGHT IN FRONT OF THE CUSHION CLAMP AND BRACKET, AND THE BRACKET IS CORRODED.
- [SDR IXXA202604080002](https://openairdocs.org/sdr/IXXA202604080002), Apr 8, 2026: SUPPORT FITTING. CORRODED. CORROSION AROUND SUPPORT FITTING FASTENER AT STA 1180 RBL 28
- [SDR IXXA2026040600001](https://openairdocs.org/sdr/IXXA2026040600001), Apr 6, 2026: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE IN LWW FOR STRUT DOOR CUTOUT
- [SDR IXXA20260403002](https://openairdocs.org/sdr/IXXA20260403002), Apr 3, 2026: PAD. GOUGED. WHILE SERVICING MAIN LANDING GEAR STRUTS, THE AIRCRAFT TILTED TO THE LEFT CAUSING LEFT MAIN GEAR JACK TO COME INTO CONTACT LOWER WING AT JACKING PAD.
- [SDR IXXA20260403001](https://openairdocs.org/sdr/IXXA20260403001), Apr 3, 2026: PAD. GOUGED. WHILE DRILLING OUT FASTENER IN THE LEFT-WING JACK PAD DOUBLER, THE DRILL CONTACTED THE OUTER PERIMETER OF HOLE IN THE WING SKIN
- [SDR IXXA20260329002](https://openairdocs.org/sdr/IXXA20260329002), Mar 29, 2026: KEELBEAM. CORRODED. CORROSION AT THE HYD TUBING PASS THRU AT THE KEEL WALL IN THE LWW BS 1171-1180.
- [SDR IXXA20260329001](https://openairdocs.org/sdr/IXXA20260329001), Mar 29, 2026: SUPPORT BEAM. CORRODED. LEFT WING UPPER FIXED WING SKIN PANEL SUPPORT BEAM CORRODED IN SEVERAL PLACES
- [SDR IXXA20260316001](https://openairdocs.org/sdr/IXXA20260316001), Mar 16, 2026: BRACKET. CORRODED. LEFT WING T/E INBD. OF DEFUEL VALVE HAS CABLE GUIDE BRACKET CORRODED
- [SDR IXXA20260315002](https://openairdocs.org/sdr/IXXA20260315002), Mar 15, 2026: RETAINER. BROKEN. SEAL RETAINER SUPPORT STRUCTURE BROKEN IN RWW MLG DOOR CUTOUT
- [SDR IXXA20260315001](https://openairdocs.org/sdr/IXXA20260315001), Mar 15, 2026: SKIN. CORRODED. FOUND SKIN CORROSION COMMON TO RT FILLET PANEL @ STA 793, 805, 825 ALL ON SKIN PANEL 143N3561-4
- [SDR IXXA04062026CC01](https://openairdocs.org/sdr/IXXA04062026CC01), Mar 13, 2026: BRACKET. CRACKED. NR 1 ENGINE COMPRESSOR BOOST FRAME FLANGE BRACKET BENT AND CRACKED AT THE ENGINE 11 O'CLOCK POSITION.
- [SDR IXXA2026031301](https://openairdocs.org/sdr/IXXA2026031301), Mar 13, 2026: SKIN PANEL. DAMAGED. REPAIRED CORRODED LEFT WING REAR SPAR UPPER PANEL SUPPORT LIP AND SKIN.
- [SDR IXXA20260311001](https://openairdocs.org/sdr/IXXA20260311001), Mar 11, 2026: SKIN. CORRODED. FUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2
- [SDR IXXA20260310001](https://openairdocs.org/sdr/IXXA20260310001), Mar 10, 2026: SKIN. CORRODED. FUSEELAGE LEFT SIDE STA 785-855 LEVEL 2 CORROSION2 BODY TO WING PANELS
- [SDR IXXA20260304001](https://openairdocs.org/sdr/IXXA20260304001), Mar 4, 2026: SKIN PANEL. CORRODED. RIGHT FUSELAGE CLOSEOUT FAIRING PANEL AFT OF MAIN CARGO DOOR FOUND CORROSION AT UPPER AND LOWER DOOR CORNERS NO PART NUMBERS FOUND ON REMOVE PANEL. FABRICATED N
- [SDR IXXA20260302001](https://openairdocs.org/sdr/IXXA20260302001), Mar 2, 2026: SUPPORT BRACKET. BROKEN. NR 1 ENGINE REMOVED AND REPAIRED HP2 VALVE CASE BRACKET DUE TO BROKEN SUPPORT BRACKET NR 187303-0400-0178, AND AMES 47170REA622
- [SDR IXXA20260223001](https://openairdocs.org/sdr/IXXA20260223001), Feb 23, 2026: SUPPORT BRACKET. CORRODED. REAR SPAR HYD BLOCK CLAMP SUPPORT BRACKET CORRODED.PN 271N6114-22
- [SDR IXXA20260222002](https://openairdocs.org/sdr/IXXA20260222002), Feb 22, 2026: PRESSURE DECK. CORRODED. RIGHT WHEEL WELL PRESSURE DECK CORRODED STA1160 RBL3 P/N 144N8142-10
- [SDR IXXA20260222001](https://openairdocs.org/sdr/IXXA20260222001), Feb 22, 2026: SUPPORT WEB. CORRODED. LW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183
- [SDR IXXA2026021901](https://openairdocs.org/sdr/IXXA2026021901), Feb 19, 2026: BRACKET. CORRODED. LEADING EDGE JUST ABOVE PYLON HAS CORROSION AROUND NUT PLATE
- [SDR IXXA20260218001](https://openairdocs.org/sdr/IXXA20260218001), Feb 18, 2026: BRACKET. CORRODED. LEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODED
- [SDR IXXA2026020702](https://openairdocs.org/sdr/IXXA2026020702), Feb 7, 2026: DOOR. GOUGED. RIGHT MLG DOOR IS GOUGED NEAR NO STEP PLACARD.
- [SDR IXXA2026020701](https://openairdocs.org/sdr/IXXA2026020701), Feb 7, 2026: WEB. CORRODED. REAR SPAR FUEL BOOST PUMP CUTOUT TO BE CORRRODED
- [SDR IXXA2026020605](https://openairdocs.org/sdr/IXXA2026020605), Feb 6, 2026: SKIN. CORRODED. CORROSION ON THE UPPER EXTERIOR SURFACE OF THE RIGHT WING UPPER SKIN, LOCATED FWD OF THE RIGHT AILERON.
- [SDR FDEA202602060138](https://openairdocs.org/sdr/FDEA202602060138), Feb 6, 2026: BULB. FAILED. FOUND L1 OVERHEAD EMERGENCY LIGHT DIM DURING MX PRE-FLIGHT CHECK. AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOV
- [SDR IXXA2026020603](https://openairdocs.org/sdr/IXXA2026020603), Feb 6, 2026: SKIN. CORRODED. FOUND AREA OF LW LOWER SKIN CORRODED JUST O/B OF BBL 70.50, JUST FWD OF STR L-10 ON THE EXTERNAL SURFACE
- [SDR IXXA2026020602](https://openairdocs.org/sdr/IXXA2026020602), Feb 6, 2026: SUPPORT. CORRODED. CORROSION ON PANEL SUPPORT ATTACHED TO THE AFT WALL IN THE LWW, FROM LBL7 TO LBL34
- [SDR IXXA2026020601](https://openairdocs.org/sdr/IXXA2026020601), Feb 6, 2026: SKIN. DAMAGED. DURING REPAIR ON NR 187303-0100-0192 IT WAS DISCOVERED THAT THERE IS A SCRIBE JUST FWD OF THE REPAIR AREA AT STA 740 STR 19L COMMON TO THE SKIN LAP.
- [SDR IXXA20260205002](https://openairdocs.org/sdr/IXXA20260205002), Feb 5, 2026: STOP FITTING. DAMAGED. L1 FWD DOOR STOP FITTING DAMAGE WAS REMOVED BY BLEND. THIS DAMAGE EXCEEDS ALLOWABLE LIMITS.
- [SDR IXXA2026020404](https://openairdocs.org/sdr/IXXA2026020404), Feb 4, 2026: BRACKET. CORRODED. LEFT WING T/E FRONT SECTION OF LANDING GEAR SUPPORT BEAM HAS CORRODED PANEL SUPPORT BRACKET
- [SDR IXXA2026020403](https://openairdocs.org/sdr/IXXA2026020403), Feb 4, 2026: BRACKET. CORRODED. LOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEAR
- [SDR IXXA20260111002](https://openairdocs.org/sdr/IXXA20260111002), Jan 11, 2026: BRACKET. CORRODED. EDIT (NEW CONTROL NUMBER) FROM DUPLIACATE CONTROL NUMBER IXXA20260111001 - FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WH
- [SDR IXX2026F00000](https://openairdocs.org/sdr/IXX2026F00000), Jan 11, 2026: BRACKET. CORRODED. FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES.
- [SDR IXXA20260205001](https://openairdocs.org/sdr/IXXA20260205001), Jan 7, 2026: BEARING. GALLED. GALLING, LIGHT CORROSION AND GOUGE AROUND BEARING FACE
- [SDR IXXA20260112002](https://openairdocs.org/sdr/IXXA20260112002), Jan 6, 2026: SUPPORT BEAM. CORRODED. RMLG STRUT DOOR SUPPORT BEAM IS CORRODED IN MULTIPLE AREAS
- [SDR FDEA202601060010](https://openairdocs.org/sdr/FDEA202601060010), Jan 6, 2026: BULB. FAILED. DURING MX PRE-FLIGHT, FOUND R1 EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 FOUND R1 EMERGENCY EXIT SIGN HAS 9 BULBS OUT. REMOVED AND REPLACED 9 FAULTY BULBS AS PER
- [SDR FDEA202601060009](https://openairdocs.org/sdr/FDEA202601060009), Jan 6, 2026: BULB. FAILED. DURING MX PRE-FLIGHT, FOUND L1 EMERGENCY EXIT SIGN DIM. AMM 33-51-01-2 FOUND L1 EMERGENCY EXIT SIGN HAS 7 BULBS OUT. REMOVED AND REPLACED 7 FAULTY BULBS AS PER 
- [SDR IXXA20260112001](https://openairdocs.org/sdr/IXXA20260112001), Dec 30, 2025: CHANNEL. CORRODED. CORROSION ON THE INSIDE OF THE U CHANNEL THAT SUPPORTS THE HYD ISOLATION VALVE, LOCATED ON THE BACK WALL IN THE LEFT WHEEL WELL STA 1180
- [SDR IXXA20251222001](https://openairdocs.org/sdr/IXXA20251222001), Dec 22, 2025: SKIN. CORRODED. .CORROSION OF THE UPPER EXTERIOR SURFACE OFTHE RIGHT WING UPPER SKIN FWD OF THE AILERON
- [SDR IXXA04022026CC01](https://openairdocs.org/sdr/IXXA04022026CC01), Dec 18, 2025: FITTING. DEFORMED. REMOVED FOR ACCESS THE RW SIDE LINK ATTACH FITTING "MICKEY MOUSE FITTING" FOR SIDE LOAD FITTING ALIGHNMENT. DURING REMOVAL FOUND DAMAGED FREEZE PLUG/BUSHING IN 
- [SDR IXXA20260111001](https://openairdocs.org/sdr/IXXA20260111001), Dec 18, 2025: SUPPORT CHANNEL. CORRODED. RH AFT LOWER WING TO BODY FAIRING FRAME BS 1037 IS CORRODED
- [SDR IXXA121820250001](https://openairdocs.org/sdr/IXXA121820250001), Dec 18, 2025: RUB BLOCK. CRACKED. RIGHT WING INBD FLAP T/E FAIRING 671BB HAD A CRACKED RUB BLOCK AT FAIRING AFT ATTACH ARM.
- [SDR IXXA03292026CC01](https://openairdocs.org/sdr/IXXA03292026CC01), Dec 9, 2025: SUPPORT. CORRODED. LEFT WING UNDER PANEL 551 AT SEVERAL AREA AROUND NUTPLATES ARE CORRODED.
- [SDR IXXA03092026CC01](https://openairdocs.org/sdr/IXXA03092026CC01), Nov 21, 2025: BEAM. WORN. RIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT.

All 556: https://openairdocs.org/model/boeing-757-2g5/reports.md

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