# Boeing 757-2Y0

- Type: Aircraft model (FAA registry)
- Registry code: 138492A
- Manufacturer (registry): BOEING
- Model: 757-2Y0
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 178
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 4
- Page: https://openairdocs.org/model/boeing-757-2y0

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 (4)

- [N753CX](https://openairdocs.org/aircraft/N753CX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1992, S/N 26152
- [N961FD](https://openairdocs.org/aircraft/N961FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1991, S/N 25268
- [N973FD](https://openairdocs.org/aircraft/N973FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1992, S/N 26151
- [N974FD](https://openairdocs.org/aircraft/N974FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1993, S/N 26158

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (830, newest 50)

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

- [SDR FDEA202608121114](https://openairdocs.org/sdr/FDEA202608121114), Aug 12, 2026: LAMP. INOPERATIVE. L1 EXTERIOR SLIDE LIGHT INOP. AMM: 33-51-06-2-1 RELAMPED L1 SLIDE LIGHT I/A/W AMM REFERENCED ABOVE, GOOD FOR SERVICE.
- [SDR FDEA202606270817](https://openairdocs.org/sdr/FDEA202606270817), Jun 27, 2026: BATTERY PACK. FAILED. R1 EMERGENCY LIGHT DOESN'T STAY ON FOR THE COMPLETE LIGHT TEST. L1 LIGHT NORMAL. AMM 33-51-07-2 REMOVED POWER SUPPLY BATTERY PACK, HAS POWER AT POWER SUPPLY, RE
- [SDR FDEA202605200624](https://openairdocs.org/sdr/FDEA202605200624), May 20, 2026: BATTERY PACK. INOPERATIVE. DURING MX PRE-FLIGHT FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT, R1 DOOR EXIT SIGN, AND CENTER OVERHEAD SIGN INOP. AMM: 33-51-07-2-2 ALLOWED EMERGENCY LIGHT BATTERY
- [SDR IXXA20260329026](https://openairdocs.org/sdr/IXXA20260329026), Mar 29, 2026: BOTTLE. RUPTURED. L4 DOOR SLIDE DEPLOYED BY CREW. SLIDE DID NOT INFLATE. REMOVED AND REPLACED PAX DOOR RESERVOIR DIAPHRAGM AND SERVICED RESERVOIR IAW B757 AMM 12-15-10. REINSTALL
- [SDR FDEA202603240369](https://openairdocs.org/sdr/FDEA202603240369), Mar 24, 2026: BATTERY PACK. FAILED. DURING MX PRE-FLIGHT, FOUND THE R1 OVERHEAD EMERGENCY LIGHT, EMERGENCY LOCATOR SIGN, AND R1 OUTDOOR EMERGENCY LIGHT WAS OUT. FOUND EMERGENCY LIGHT BATTERY PACK,
- [SDR FDEA202603150352](https://openairdocs.org/sdr/FDEA202603150352), Mar 15, 2026: BATTERY. NO TEST. DURING SERVICE CHECK FOUND R1 DOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED BATTERY AT M730.
- [SDR FDEA202602270287](https://openairdocs.org/sdr/FDEA202602270287), Feb 27, 2026: GIRT BAR. DAMAGED. WHEN OPENING THE MAIN CABIN DOOR, A METAL PIECE ON THE BOTTOM OF THE DOOR FELL OFF. LOOKS LIKE A PIECE OF THE GIRT BAR. REINSTALLED GIR BAR END, NO RII AT BHM P
- [SDR FDEA202602140201](https://openairdocs.org/sdr/FDEA202602140201), Feb 14, 2026: CREASE BEAM. CORRODED. MCC STA 880 SIDE LH CREASE BEAM WITH CORROSION CUT AND REMOVED DAMAGE AREA M.C.C STA 852 TO STA 900 CREASE BEAM IAW B757 SRM 53-00- 13-2R REP 1 FABRICATED TRIMM
- [SDR FDEA202602140200](https://openairdocs.org/sdr/FDEA202602140200), Feb 14, 2026: FLOORBEAM. CORRODED. MAIN DECK FLOOR BEAM STA 1200 BTW BL 0 RBL 58 CORRODED REMOVED DAMAGE T CAP SECTION INSTALLED T CAP SECTION AND REPAIR SPLICE PARTS MAIN DECK FLOOR BEAM STA 120
- [SDR FDEA202602140199](https://openairdocs.org/sdr/FDEA202602140199), Feb 14, 2026: SKIN PANEL. CORRODED. NR 2 ENGINE ACCESS PANEL # 443GL FRAME SKIN CUT OUT CORRODED (EXFOLIATED) REMOVED AND REPLACED # 2 ENGINE FWD NACELLE STRUT NEW SKIN PANEL IAW DWG 311N5002 REV 
- [SDR FDEA202602120191](https://openairdocs.org/sdr/FDEA202602120191), Feb 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 1620 - 1420, LBL 58.22 MULTIPLE SPOTS OF CORROSION. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G, TRIMMED, LOCATED, & DRILLED A N
- [SDR FDEA202602100162](https://openairdocs.org/sdr/FDEA202602100162), Feb 10, 2026: CREASE BEAM. CORRODED. MAIN CARGO COMPARTMENT BS 660 R/H CREASE BEAM INB CHORD WITH CORROSION
- [SDR FDEA202602100161](https://openairdocs.org/sdr/FDEA202602100161), Feb 10, 2026: CREASE BEAM. CORRODED. MAIN CABIN CREASE BEAM RBL 64.50 FROM STA 1490 TO STA 1640 MULTIPLES SPOTS WITH CORROSION CUT OUT DAMAGE SECTION (TRIMMED) MAIN CABIN CREASE BEAM RBL 64.5 FROM 
- [SDR FDEA202602100159](https://openairdocs.org/sdr/FDEA202602100159), Feb 10, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK FLANGE WITH CORROSION BETWEEN B.S 1280-1300 RBL 24.75 REMOVED SEAT TRACK SECTION MAIN CABIN BETWEEN STA 1200 TO 1320 LBL 24.75 IAW B757 SR
- [SDR FDEA202602030118](https://openairdocs.org/sdr/FDEA202602030118), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 1540 AND 1640 RBL 45.50 SEAT TRACK WITH CORROSION (TWO LOCATIONS). REMOVED SEAT TRACK SECTION MAIN CARGO COMP BETWEEN STA 1540
- [SDR FDEA202602030117](https://openairdocs.org/sdr/FDEA202602030117), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BS 1320 RBL 45.50 SEAT TRACK WITH CORROSION.
- [SDR FDEA202602030116](https://openairdocs.org/sdr/FDEA202602030116), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO SEAT TRACK BS 1320 TO 1540 LBL 45.50 WITH MULTIPLE CORROSION. REMOVED SEAT TRACK SECTION MAIN CABIN STA 1320 TO 1540 LBL 45.50 TRIMMED, LOCATED AND D
- [SDR FDEA202601300108](https://openairdocs.org/sdr/FDEA202601300108), Jan 30, 2026: SEAT TRACK. CORRODED. MCC STA 1280 LBL 58.22 SEAT TRACK WITH CORROSION. REMOVED AND REPLACED THE SEAT TRACK SRA 1180-1420 LBL 58.22 IAW SRM 51-40-02-0G, & DWG 657N3332, REV A.
- [SDR FDEA202601300107](https://openairdocs.org/sdr/FDEA202601300107), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BS 1620 RBL 58.22 SEAT TRACK WITH CORROSION. REMOVED SEAT TRACK SECTION MAIN CARGO STA 1180-1420 RBL 58.22 IAW B757 SRM 51-40-02-0G TRIMM
- [SDR FDEA202601300104](https://openairdocs.org/sdr/FDEA202601300104), Jan 30, 2026: SKIN. DELAMINATED. LEFT WING MAIN INBOARD FLAP LOWER SURFACE HAS SKIN CRACKED. UPON FURTHER EVALUATION ON L/WING MAIN FLAP INBD LOWER SURFACE FOUND DELAMINATION DIM L = 10.5" W=1.
- [SDR FDEA202601300103](https://openairdocs.org/sdr/FDEA202601300103), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK LBL 58.00 FROM 1180 TO STA 900 MULTIPLES SPOTS CORRODED
- [SDR FDEA202601300102](https://openairdocs.org/sdr/FDEA202601300102), Jan 30, 2026: SEAT TRACK. CORRODED. MCC STA 880 TO 840 LBL 58.22 SEAT TRACK FOUND CORRODED. REMOVED SEAT TRACK SECTION STA 660 TO STA 885 RBL 58.22 M.C.C IAW SRM 51-40-02-0G. TRIMMED, LOCATED AND 
- [SDR FDEA202601300101](https://openairdocs.org/sdr/FDEA202601300101), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 740 AND 860 RBL 58.22 SEAT TRACK WITH CORROSION (03 LOCATION). REMOVED SEAT TRACK SECTION MAIN CABIN BETWEEN STA 660 TO 885 RB
- [SDR FDEA202601300100](https://openairdocs.org/sdr/FDEA202601300100), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 58.00 BTW BS 900 - 1180, MULTIPLES SPOTS WITH CORROSION. REMOVED SEAT TRACK SECTION BETWEEN STA 900 TO 1180 RBL 58.0 M.C.C IAW B757 SRM
- [SDR FDEA202601300099](https://openairdocs.org/sdr/FDEA202601300099), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK STA 1205, RBL 58 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G.
- [SDR FDEA202601280094](https://openairdocs.org/sdr/FDEA202601280094), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK LBL 58.00 FROM BS 1180 TO 900 MULTIPLES SPOTS CORRODED. REMOVED SEAT TRACK SECTION MAIN DECK STA 900 TO 1180 LBL 58.00 IAW B757 SRM 51-40-0
- [SDR FDEA202601280093](https://openairdocs.org/sdr/FDEA202601280093), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 1280 AND 1320 RBL 45.50 SEAT TRACK WITH CORROSION. REMOVED AND REPLACED SEAT TRACK MAIN CARGO COMPARTMENT BETWEEN BS 1280-1320
- [SDR FDEA202601280092](https://openairdocs.org/sdr/FDEA202601280092), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 45 BTW BS 1180 TO 1200 CORRODED. REMOVED SEAT TRACK MAIN DECK RBL 45 BETWEEN STA 1180 TO 1280 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED
- [SDR FDEA202601280091](https://openairdocs.org/sdr/FDEA202601280091), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 58.00 BTW STA 900 TO STA 1180 MULTIPLES SPOTS WITH CORROSION.
- [SDR FDEA202601090016](https://openairdocs.org/sdr/FDEA202601090016), Jan 9, 2026: HOUSING. DAMAGED. COURIER AREA CENTER EMERGENCY LIGHT WITH R1 DOOR OVERHEAD EMERGENCY LIGHT AND EXTERIOR SLIDE LIGHT INOP. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-07-2, R
- [SDR IXXA20251219086](https://openairdocs.org/sdr/IXXA20251219086), Dec 19, 2025: HOUSING. DIRTY. L1 ENTRY DOOR SLIDE LIGHT INOPERATIVE. PLACED ON DEFERRAL 69103 MNIMUM EQUIPMENT LIST ATI-25-66-05-01 CATEGORY C. DUE 30 DECEMBER 2025. REMOVED, CLEANED AND REI
- [SDR IXXA202512109085](https://openairdocs.org/sdr/IXXA202512109085), Dec 9, 2025: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK FOUND EMERGENCY LIGHTS IN FORWARD GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FORWARD GALLEY AFT OF ENTRANCE LIGHT PANEL IN AC
- [SDR IXXA20251105002](https://openairdocs.org/sdr/IXXA20251105002), Nov 5, 2025: SKIN. CORRODED. RIGHT WING LOWER SURFACE SKIN PANEL NO 1, WSTA 95.0-177.5 CORROSION GRID NR 2.
- [SDR IXXA20251105001](https://openairdocs.org/sdr/IXXA20251105001), Nov 5, 2025: SKIN. CORRODED. RIGHT WING LOWER INBD SURFACE, AFT OUTBD OF FUSELAGE HAS AREA OF CORROSION WSTA, 95.0-177.5
- [SDR IXXA20251030004](https://openairdocs.org/sdr/IXXA20251030004), Oct 30, 2025: SKIN. CORRODED. RIGHT WING I/B LOWER LEADING EDGE WING SKIN IS CORRORED AT RIGHT WING I.B SLAT STA 284
- [SDR IXXA20251030003](https://openairdocs.org/sdr/IXXA20251030003), Oct 30, 2025: SKIN. CORRODED. RIGHT WING LOWER SKIN APPROX 18 INCHES FWD OF FUEL PANEL 631BB CORRODED AT SKIN BUTT SPLICE
- [SDR IXXA20251030002](https://openairdocs.org/sdr/IXXA20251030002), Oct 30, 2025: SKIN. CORRODED. RW LOWER SKIN 37" AFT OF SKIN SPLICE 5"- 46" OUTBD OF FUSELAGE HAS AREA OF CORROSION PN112N4101-34, AND 112N4102-42
- [SDR IXXA20251030001](https://openairdocs.org/sdr/IXXA20251030001), Oct 30, 2025: SKIN. CORRODED. RW LOWER SKIN 37" AFT OF SKIN SPLICE, 5"- 46 "OUTBD OF FUSELAGE HAS AREA OF CORROSION PN 112N4101-34 AND 112N4102-42
- [SDR IXXA20280925055](https://openairdocs.org/sdr/IXXA20280925055), Sep 25, 2025: BULB. INOPERATIVE. FORWARD FLIGHT ATTENDANT'S EMERGENCY CALL LIGHT IS INOPERATIVE. PLACED ON DEFERRAL 66475 MINIMUM EQUIPMENT LIST 23-41-01-04 CATEGORY B. DUE 28 SEPTEMBER 2025. R
- [SDR IXXA20250809040](https://openairdocs.org/sdr/IXXA20250809040), Aug 9, 2025: GOVERNOR. INOPERATIVE. LEFT ENGINE TAKING APPROXIMATELY 30 SECONDS TO SHUTDOWN AFTER FUEL CONTROL SHUTOFF. IN ACCORDANCE WITH B767 FIM 73-21 FAULT TREE 807 REMOVED AND REPLACED FUEL F
- [SDR IXXA20250722032](https://openairdocs.org/sdr/IXXA20250722032), Jul 22, 2025: SLIDE. LOW PRESSURE. MAINTENANCE FOUND R3 EMERGENCY SLIDE PRESSURE GAUGE BELOW SERVICABLE LIMITS. REMOVED AND REPLACED R3 EMERGENCY SLIDE IN ACCORDANCE WITH BOEING 757 MAINTENANCE M
- [SDR IXXA20250709028](https://openairdocs.org/sdr/IXXA20250709028), Jul 9, 2025: LIGHT. NO TEST. CREW PRE-FLIGHT, SLIDE LIGHT AT R4 DOOR DOES NOT ILLUMINATE. CLEANED GIRT BAR SLIDER STOP. OPERATIONAL CHECK IAW B767 AMM 52-11-25 NOTED NO FAULTS.
- [SDR IXXA20250707027](https://openairdocs.org/sdr/IXXA20250707027), Jul 7, 2025: ACCESS PANEL. DAMAGED. CREW REPORTED, CATERING DAMAGED ACCESS DOOR TO SLIDE ON R4 DOOR. REINSTALLED R4 DOOR SLIDE IAW B757 AMM 25-66-03. OPERATIONAL CHECK OF SLIDE HOOK UP GOOD. NO OT
- [SDR IXXA202506200005](https://openairdocs.org/sdr/IXXA202506200005), Jun 20, 2025: LATCH. GOUGED. #2 ENG O/B T/R FWD LATCH CATCH RECEIVER IS GOUGED.
- [SDR IXXA20250620004](https://openairdocs.org/sdr/IXXA20250620004), Jun 20, 2025: HINGE. BENT. I/B T/R FWD AHAD DOOR HINGE ATTACH POINT BENT AND GOUGED
- [SDR IXXA20250620003](https://openairdocs.org/sdr/IXXA20250620003), Jun 20, 2025: PAN. CORRODED. DURING OKAY INSTALL OF HANDLE L-1 DOOR, FOUND EXTERIOR DOOR HANDLE PAN TO BE GOUGED AND HAS CORROSION.
- [SDR IXXA20250620002](https://openairdocs.org/sdr/IXXA20250620002), Jun 20, 2025: FASTENER. INCORRECT. L1 DOOR HANDLE PAN HAS SEVERAL INCORRECT LENGTH BLIND FASTENERS INSTALLED.
- [SDR IXXA20250620001](https://openairdocs.org/sdr/IXXA20250620001), Jun 20, 2025: RETAINER. CRACKED. UPPER I/B T/R SEAL RETAINER CRACKED/BENT AT THREE LOCATIONS
- [SDR IXXA2025061701](https://openairdocs.org/sdr/IXXA2025061701), Jun 17, 2025: STIFFENER. CORRODED. STIFFENER CORRODED STA 1071, RB-44.5 - RB-70
- [SDR IXXA20250611502](https://openairdocs.org/sdr/IXXA20250611502), Jun 15, 2025: SUPPORT ANGLE. CORRODED. LEFT LANDING GEAR HYDRAULIC STSTEM HOSE CLAMPS SUPPORT ANGLES CORRODED

All 830: https://openairdocs.org/model/boeing-757-2y0/reports.md

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