# Boeing 757-2T7

- Type: Aircraft model (FAA registry)
- Registry code: 138491A
- Manufacturer (registry): BOEING
- Model: 757-2T7
- 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: 3
- Page: https://openairdocs.org/model/boeing-757-2t7

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 (3)

- [N935FD](https://openairdocs.org/aircraft/N935FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 22780
- [N936FD](https://openairdocs.org/aircraft/N936FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1985, S/N 23293
- [N937FD](https://openairdocs.org/aircraft/N937FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1987, S/N 23895

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (666, newest 50)

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

- [SDR FDEA202610131587](https://openairdocs.org/sdr/FDEA202610131587), Oct 13, 2026: INDICATION SYS. MALFUNCTIONED. DURING CLIMB OUT, GOT RT HYD SYS PRESSURE EICAS & ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE & NORMAL QUANTITY. EMERGENCY DECL
- [SDR FDEA202610131564](https://openairdocs.org/sdr/FDEA202610131564), Oct 13, 2026: WIRE. SHORTED. DURING CLIMB OUT GOT R HYD SYS PRESS EICAS AND ASSOCIATED LIGHT ON OVERHEAD. LOWER EICAS STATUS PAGE SHOWED NORMAL PRESSURE AND NORMAL QUANTITY. EMERGENCY DECLA
- [SDR FDEA202609181374](https://openairdocs.org/sdr/FDEA202609181374), Sep 18, 2026: EEC. FAILED. L EEC EICAS DURING TAKEOFF ROLL AND 4X IN FLIGHT ALL WITH ASSOCIATED AUTOTHROTTLES EICAS. NOTABLE YAW IN FLIGHT WHEN IT WOULD OCCUR. COMPLIED WITH QRH. FIM: 73-
- [SDR FDEA202609141333](https://openairdocs.org/sdr/FDEA202609141333), Sep 14, 2026: GUST LOCK. FAILED. WHILE CLOSING THE L-1 DOOR, RAMP WAS UNABLE TO RELEASE THE GUST LOCK. FOUND HOLD OPEN DOOR COLLAR DAMAGED AND WILL REQUIRE REPLACEMENT. PART NIS AT FLL. AMM 52-
- [SDR FDEA202607231013](https://openairdocs.org/sdr/FDEA202607231013), Jul 23, 2026: BEAM. CORRODED. NOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER A
- [SDR FDEA202607200955](https://openairdocs.org/sdr/FDEA202607200955), Jul 20, 2026: STRAP. CORRODED. APU INLET DUCT ATTACHMENTS AT THE AFT FRAME WITH CORROSION CORRSION OUT OF LIMITS AT APU INLET DUCT ATTACHMENTS ON THE AFT FRAME (MIDDLE STRAP) IAW B-757 SRM 53
- [SDR FDEA202607200954](https://openairdocs.org/sdr/FDEA202607200954), Jul 20, 2026: CREASE BEAM. CORRODED. MCC CREASE BEAM SIDE LH BSTA 1620 TO BSTA 1370 IT HAS CORROSION SPOTS MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1430 TO 1530 LBL 64.40 I
- [SDR FDEA202607200953](https://openairdocs.org/sdr/FDEA202607200953), Jul 20, 2026: CREASE BEAM. CORRODED. MCC SIDE LH BETWEEN BS 1080 TO BS 1100 CREASE BEAM WITH CORROSION MCC L/H CREASE BEAM SECTION WITH CORROSION OUT OF LIMITS FROM STA 1040 TO STA 1100 IAW B-757 S
- [SDR FDEA202607150928](https://openairdocs.org/sdr/FDEA202607150928), Jul 15, 2026: FLOORBEAM. CORRODED. MCC BL 0 TO LBL 24.75 BS 1200 FLOOR BEAM WITH CORROSION AREA WITH CORROSION OUT OF LIMITS AT FLOOR BEAM BS 1200 LBL 8 TO LBL 14 WAS REPAIRED IAW B757 SRM 53-00-
- [SDR FDEA202607150927](https://openairdocs.org/sdr/FDEA202607150927), Jul 15, 2026: COLLAR. BROKEN. L1 DOOR GUST LOCK FOUND BROKEN DURING POST FLIGHT CHECK UPON FLIGHT ARRIVAL. REINSTALLED NEW AND SERVICEABLE GUST LOCK AS REQUIRED, OPS CHECK GOOD IAW AMM 52-11
- [SDR FDEA202607100893](https://openairdocs.org/sdr/FDEA202607100893), Jul 10, 2026: SKIN PANEL. DENTED. UPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I
- [SDR FDEA202607100892](https://openairdocs.org/sdr/FDEA202607100892), Jul 10, 2026: ACCESS PANEL. CRACKED. LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-75
- [SDR FDEA202607100890](https://openairdocs.org/sdr/FDEA202607100890), Jul 10, 2026: ACCESS PANEL. CRACKED. LH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 
- [SDR FDEA202605280640](https://openairdocs.org/sdr/FDEA202605280640), May 28, 2026: GUST LOCK. DAMAGED. L1 DOOR HOLD OPEN LOCK IS BROKEN. TROUBLESHOOTING REQUIRED PRIOR TO INSTALLING IPC EFFECTIVITY VERIFICATION IS ALSO REQUIRED. REMOVED AND REPLACED L1 DOOR HOLD 
- [SDR FDEA202601060008](https://openairdocs.org/sdr/FDEA202601060008), Jan 6, 2026: SKIN. CORRODED. ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN AREA IS WITH CORROSION AREA WITH CORROSION AT ENG. #2 NACELLE STRUT AFT ACCESS PANEL 443LL INSIDE SKIN 
- [SDR FDEA202601060007](https://openairdocs.org/sdr/FDEA202601060007), Jan 6, 2026: CREASE BEAM. CRACKED. RH LOBE INTERIOR BETWEEN BS 1720 AND STR 17 HAS CREASE BEAM WITH CRACK 2 INCH APROX. ACCOMPLISHED REPAIR ON ADDITIONAL DAMAGE FOUND: CRACK IN THE HOLE AT AFT PR
- [SDR FDEA202512302297](https://openairdocs.org/sdr/FDEA202512302297), Dec 30, 2025: SKIN. CORRODED. NR 1 ENGINE NACELLE STRUT PP STA 174.30 R/H FWD BULKHEAD INTERNAL SIDE SKIN WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A.#: F - 5430 - T0385806 P1 W
- [SDR FDEA202512302296](https://openairdocs.org/sdr/FDEA202512302296), Dec 30, 2025: SKIN. CORRODED. NR 1 ENGINE NACELLE STRUT ACCESS PANEL 433JR CUTOUT WITH CORROSION THIS JOB WAS ACCOMPLISHED UNDER FEDEX E.A F- 5430 - T0385806 P1
- [SDR FDEA202512292295](https://openairdocs.org/sdr/FDEA202512292295), Dec 29, 2025: STRINGER. CORRODED. MEC BETWEEN BS 418 - 440, S24R CORRODED. PERMANENTLY REPAIRED STRINGER 24R IAW SRM 53-00-03-2R, REP 2, FIG 201.
- [SDR FDEA202512272292](https://openairdocs.org/sdr/FDEA202512272292), Dec 27, 2025: SKIN. CORRODED. NO 1 ENGINE NACELLE BETWEEN ACCESS PANEL 433 HR AND 433 JR INTERNAL SKIN WITH CORROSION. JOBS FOR NR W/O 91519, N00437 AND N00438 WAS INCLUDED AND ACCOMPLISHED 
- [SDR FDEA202512222284](https://openairdocs.org/sdr/FDEA202512222284), Dec 22, 2025: CREASE BEAM. CORRODED. MAIN CABIN. CREASE BEAM. (RH) STA 1200 CORRODED. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT CREASE BEAM INBOARD CHORD AT STA 1200 RBL 64 WAS REPAIRED IAW
- [SDR FDEA202512222283](https://openairdocs.org/sdr/FDEA202512222283), Dec 22, 2025: CREASE BEAM. CORRODED. MCC FLOOR BTWN STA 440 - 460 (RH CREASE BEAM) RBL 64.5 APROX WAS FOUND ON LOCATION WITH CORROSION. CORROSION OUT OF LIMITS AT MAIN CARGO COMPARTMENT, CREASE BEA
- [SDR FDEA202512222282](https://openairdocs.org/sdr/FDEA202512222282), Dec 22, 2025: CREASE BEAM. CORRODED. MAIN CARGO BAY, FLOOR INBOARD CHORD HAS SURFACE CORROSION AROUND NUTS PLATE BETWEEN BS 860 AND 879 CORROSION OUT OF LIMITS AT MAIN CARGO BAY CREASE BEAM INBOARD
- [SDR FDEA202512192264](https://openairdocs.org/sdr/FDEA202512192264), Dec 19, 2025: SKIN. CORRODED. ENG NR 2 NACELLE STRUT FWD ACCESS PANEL 443AR INSIDE SKIN IS WITH CORROSION. (INNER AREA.) ENG. NR 2 NACELLE STRUT OTBD SIDE FWD ACCESS PANEL 443AR SKIN OUT OF 
- [SDR FDEA202512172260](https://openairdocs.org/sdr/FDEA202512172260), Dec 17, 2025: DECK PLATE. CORRODED. POINTS NR 2 AND 3 WITH CORROSION OUT OF LIMITS AT DECK PLATE AREA, BS 1681, BTW RBL 13 - 23, OUT OF LIMITS AT CABIN DECK PLATE. REPAIRED IAW SRM 53-60-51-2R, RE
- [SDR FDEA202512172259](https://openairdocs.org/sdr/FDEA202512172259), Dec 17, 2025: SKIN. CORRODED. NR 2 NACELLE STRUT FWD ACCESS PANEL 443GL INSIDE SKIN AREA IS WITH CORROSION. NR 2 NACELLE STRUT INBD SIDE FWD ACCESS PANEL 443GL SKIN OUT OF LIMITS WAS REPLACE
- [SDR FDEA202512122247](https://openairdocs.org/sdr/FDEA202512122247), Dec 12, 2025: SHEAR WEB. CORRODED. CABIN FLOOR SHEAR WEB HAD MULTIPLES SPOTS OF CORROSION, BS 1680 - 1720, AREA OUT OF LIMITS. BS 1697, LBL 08 IAW SRM 53-60-51-1A. REPAIRED IAW SRM 53-60-51-2R, R
- [SDR FDEA202512122246](https://openairdocs.org/sdr/FDEA202512122246), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CARGO BAY SEAT TRACK 45.50 RBL BETWEEN BS 1100 -1140 HAS MULTIPLE AREAS WITH CORROSION. REMOVED SEAT TRACK BS 1076 TO 1180, RBL 45.50 IAW SRM 51-40-02-0G; 
- [SDR FDEA202512122245](https://openairdocs.org/sdr/FDEA202512122245), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CARGO BAY, SEAT TRACK 45.50 LBL BETWEEN BS 1180 - 1200 WITH CORROSION IN MULTIPLES AREAS. REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 118
- [SDR FDEA202512122244](https://openairdocs.org/sdr/FDEA202512122244), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CARGO BAY FLOOR SEAT TRACK HAS SURFACE CORROSION BETWEEN BS 680 & 720, RBL 58.22. REMOVED SEAT TRACK SECTION OUT LIMITS AT MAIN CARGO BS BS 640 - 880, RBL 
- [SDR FDEA202512122243](https://openairdocs.org/sdr/FDEA202512122243), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CABIN. SEAT TRACK, RBL 58.22 BTW BS 1180 TO 1200 CORRODED REMOVED SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT BS 1180 TO 1420 RBL 58.22 IAW 
- [SDR FDEA202512122242](https://openairdocs.org/sdr/FDEA202512122242), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CARGO BAY SEAT TRACK LBL 58.22, BS 1180 - 1420 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION IAW SRM 51-40-02-0G. TRIMMED, LOCATED, DRIL
- [SDR FDEA202512122241](https://openairdocs.org/sdr/FDEA202512122241), Dec 12, 2025: SEAT TRACK. CORRODED. MAIN CARGO COMPARMENT SEAT TRACK LBL BETWEEN BS 1180 - 900 WITH CORROSION IN MULTIPLE AREAS. REMOVED THE SEAT TRACK SECTION OUT OF LIMITS AT MAIN CARGO BAY BS 9
- [SDR FDEA202512122240](https://openairdocs.org/sdr/FDEA202512122240), Dec 12, 2025: SKIN. DELAMINATED. LEFT WING OTBD MAIN FLAP T/E UPPER SURFACE HAD POSSIBLE DELAMINATION. APPLIED PERMANENT REPAIR ON AREAS WITH DELAMINATION AT LT WING OTBD MAIN FLAP T/E UPPER SU
- [SDR FDEA202512112237](https://openairdocs.org/sdr/FDEA202512112237), Dec 11, 2025: CREASE BEAM. CORRODED. MAIN CARGO BAY FLOOR CREASE BEAM HAS SURFACE CORROSION BETWEEN BS 760 AND 780. REMOVED CREASE BEAM INBD CHORD SECTION OUT OF LIMITS AT MAIN CARGO COMPARTMENT LB
- [SDR FDEA202512102230](https://openairdocs.org/sdr/FDEA202512102230), Dec 10, 2025: SKIN. DENTED. LEFT HORIZONTAL STAB UPPER SKIN HAD REPAIR DAMAGE AT LOWER INTERNAL SURFACE, HSS 104.248 & 128.248, DENT WITH DELAMINATION AT LT HORIZONTAL STAB UPPER SKIN ON L
- [SDR FDEA202512102229](https://openairdocs.org/sdr/FDEA202512102229), Dec 10, 2025: SKIN. DENTED. LEFT HORIZONTAL STAB UPPER SKIN HAD FIVE DENTS BETWEEN HSS 81.249 AND 104.248, APPLIED PERMANENT REPAIR AT LT HORIZONTAL STAB UPPER SKIN IAW SRM 55-10-01-1A, TA
- [SDR FDEA202506060850](https://openairdocs.org/sdr/FDEA202506060850), Jun 6, 2025: GUST LOCK. INOPERATIVE. L1 DOOR GUST LOCK FOUND DAMAGED/BROKEN ON WALKAROUND. AMM: 52-11-08-8 INSTALLED NEW SPLIT COLLAR IRW AMM 52-11-08-8.
- [SDR FDEA202408301193](https://openairdocs.org/sdr/FDEA202408301193), Aug 30, 2024: TRANSMISSION. DIRTY. TE FLAP DISAGREE ON APPROACH. FLAPS STUCK BETWEEN 20-25 DEGREES. EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER FIM. FOUND FAULT CODE 305 (FLAP DISAGREE) ON 
- [SDR FDEA202408171144](https://openairdocs.org/sdr/FDEA202408171144), Aug 17, 2024: STRINGER. CORRODED. FORWARD CARGO LSTR 19-22 STA 760 FRAME HAS AREAS OF CORROSION AT SKIN ATTACHMENT POINTS AND STR EVALUATED CORROSION AT SKIN ATTACHMENT POINTS S-19L, 21L, AND 22
- [SDR FDEA202406280877](https://openairdocs.org/sdr/FDEA202406280877), Jun 28, 2024: BATTERY. NO TEST. LEFT SIDE EMERGENCY LIGHTS DO NOT TEST. R & R LT EMERGENCY LIGHTS POWER SUPPLY REF 757 AMM 33-51-07-2. OPS CHECK GOOD, OK FOR SERVICE.
- [SDR FDEA202406120794](https://openairdocs.org/sdr/FDEA202406120794), Jun 12, 2024: BATTERY. NO TEST. DURING EMERGENCY EXIT LIGHT TEST R/H EXIT LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. R/H EXIT LIGHT OPS CHK 
- [SDR FDEA202403300423](https://openairdocs.org/sdr/FDEA202403300423), Mar 30, 2024: BATTERY PACK. INOPERATIVE. THROUGHOUT MAINTANENCE DAILY CHECK FOUND L1 EMER EXIT SIGN DOOR 1 LT, FLT DECK DOME EMER LT MODULE, SLIDE LT DR 1 EMER INOP. SHGN 30MAR24 05:49 BNA WDM: CH 33-5
- [SDR FDEA202403160300](https://openairdocs.org/sdr/FDEA202403160300), Mar 16, 2024: GIRT BAR. OUT OF ALIGNMENT. L1 DOOR ESCAPE SLIDE BEGAN TO FALL OUT WHEN DOOR WAS OPENED FOR CREW STAIR MATING. DURING TROUBLESHOOTING FOUND LH DOOR AFT FLOOR FITTING MISALIGNED. RE-ALIGNED
- [SDR FDEA202402210206](https://openairdocs.org/sdr/FDEA202402210206), Feb 21, 2024: FITTING. DAMAGED. DURING ACCOMPLISHED W/C EF-5730-E0340076 P11 STEP #3 PAGE 5 OF 13. FOUND #8 HOLE 2ND OVERSIZED. REMOVED & REINSTALLED #1 ENG IB & OB FAN COWLS, #1 PYLON BULLNOS
- [SDR FDEA202401240105](https://openairdocs.org/sdr/FDEA202401240105), Jan 24, 2024: SKIN. DENTED. DENT FOUND AT FUSELAGE SKIN BTW STA 480-500, STR 22-R TO 23R. EVALUATED DENT ON FUSELAGE SKIN BETWEEN STA 480-500, STR 22R TO 23R FOUND TO BE OUT OF LIMITS IAW 
- [SDR FDEA202401230102](https://openairdocs.org/sdr/FDEA202401230102), Jan 23, 2024: SKIN. GOUGED. MAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 497 1 1/8" BELOW S-10 IAW B757-200
- [SDR FDEA202401230101](https://openairdocs.org/sdr/FDEA202401230101), Jan 23, 2024: SKIN. GOUGED. MAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 490 0.787" BELOW S-10 IAW B757-200
- [SDR FDEA202401190091](https://openairdocs.org/sdr/FDEA202401190091), Jan 19, 2024: FLOOR PANEL. DENTED. MAIN CABIN FOUND DENTS ON FLOORBOARD PANEL #232 MJF BETWEEN STA 560 TO STA 680 RBL 58.22 TO RBL 63.5.
- [SDR FDEA202208071908](https://openairdocs.org/sdr/FDEA202208071908), Aug 7, 2022: FRAME. DELAMINATED. LEFT ELEVATOR O/B UPPER SURFACE CONDUCTIVE FRAME IS DELAMINATED. REMOVED & REPLACED -7 ADAPTER PLATE IAW DWG 183N2003 REV G, -5 SPLICE PLATE & CONDUCTIVE FRAME 

All 666: https://openairdocs.org/model/boeing-757-2t7/reports.md

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