# Boeing 757-27B

- Type: Aircraft model (FAA registry)
- Registry code: 1384921
- Manufacturer (registry): BOEING
- Model: 757-27B
- 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: 1
- Page: https://openairdocs.org/model/boeing-757-27b

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)

- [N916FD](https://openairdocs.org/aircraft/N916FD): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 24137

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (242, newest 50)

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

- [SDR FDEA202606190782](https://openairdocs.org/sdr/FDEA202606190782), Jun 19, 2026: WEDGE. GOUGED. LEFT WING OTBD L/E SLAT # 4 I/B LOWER SURFACE REAR EDGE HAS (2) GOUGES APPLIED PERMANENT REPAIR AT L/WING O/B L/E SLAT # 4 I/B LOWER SKIN IAW SRM 57-43-02- 2R, 
- [SDR FDEA202604250497](https://openairdocs.org/sdr/FDEA202604250497), Apr 25, 2026: LAMP. INOPERATIVE. R1 DOOR EXTERIOR SLIDE LIGHT INOP. RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2 OPS CHKD SERVICEABLE.
- [SDR FDEA202502100210](https://openairdocs.org/sdr/FDEA202502100210), Feb 10, 2025: GIRT BAR. DIRTY. ENTRY DOOR IS NOT GIVING PROPER INDICATIONS UPON CLOSING. SLIDE LIGHT IS NOT COMING ON AND THE DOOR ARMING LEVER HAS RESISTANCE WHEN MOVING. WHEN TRYING TO DISA
- [SDR FDEA202405110658](https://openairdocs.org/sdr/FDEA202405110658), May 11, 2024: SMOKE HOOD. DAMAGED. DURING SERVICE CHECK, FOUND COURIER PBE VACUUM BAG SEAL BROKEN. RELEASED FOR SERVICE PER MEL : 35-20-01 CATEGORY : D EXPIRATION : 08SEP24 "MEL 35-20-01: COURIER
- [SDR FDEA2023012650164](https://openairdocs.org/sdr/FDEA2023012650164), Jan 25, 2023: LAMP. FAILED. LIGHTS INOP IN GALLEY FASTEN SEAT BELT SIGN. IAWAMM 33-24-00-2 REPLACE THE LAMPS IN THE FASTEN SEAT BELT SIGN IAW AMM 33-24-00-2, OPS OK.
- [SDR FDEA202211302857](https://openairdocs.org/sdr/FDEA202211302857), Nov 30, 2022: LIGHT. MALFUNCTIONED. RIGHT FORWARD ENTRY DOOR SLIDE LIGHT STAYS ILLUMINATED AFTER DOOR IS DISARMED. ACCOMPLISHED FIM 52-11-00, OPS TEST ON GND PERFORMED ON SLIDE ARM/DISARM INDICATI
- [SDR FDEA202211122761](https://openairdocs.org/sdr/FDEA202211122761), Nov 12, 2022: UNKNOWN. UNKNOWN. RIGHT SIDE SERVICE DOOR FAILED TO DISARM. DOOR 1R - CHECKED GIRT BAR FOR SMOOTH ENGAGE/DISENGAGE ACTION X 20 TIMES AND OPERATION OF DOOR WARNING LIGHT IAW AMM 5
- [SDR FDEA202209152333](https://openairdocs.org/sdr/FDEA202209152333), Sep 15, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #18 HAS REJECTABLE INDICATIONS DUE TO CORROSION. ACCOMPLISHED REPAIR ON #2 ENGINE DRAG FITTING HOLE #18 IAW EA F-5730-T03702
- [SDR FDEA202209152332](https://openairdocs.org/sdr/FDEA202209152332), Sep 15, 2022: DRAG FITTING. CRACKED. RH WING #2 ENGINE DRAG FITTING HOLE #2 HAS CRACK AND CORROSION INDICATIONS NOTED. ACCOMPLISHED #2 ENGINE DRAG FITTING HOLE #2 REPAIR IAW EA F-5730-T0370276 P1, 
- [SDR FDEA202209152331](https://openairdocs.org/sdr/FDEA202209152331), Sep 15, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #12 HAS REJECTABLE INDICATIONS DUE TO CORROSION. ACCOMPLISHED REPAIR ON #2 ENGINE DRAG FITTING HOLE #12 IAW EA F-5730-T03702
- [SDR FDEA202209152330](https://openairdocs.org/sdr/FDEA202209152330), Sep 15, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #9 HAS CRACK AND CORROSION INDICATIONS NOTED. ACCOMPLISHED REPAIR ON RH WING #2 ENGINE DRAG FITTING HOLE #9 IAW EA F-5730-T0
- [SDR FDEA202209152329](https://openairdocs.org/sdr/FDEA202209152329), Sep 15, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #17 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED REPAIR ON RH WING #2 ENGINE DRAG FITTING HOLE #17 IAW EA F-5730
- [SDR FDEA202209142322](https://openairdocs.org/sdr/FDEA202209142322), Sep 14, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #4 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED #2 ENGINE DRAG FITTING HOLE #4 IAW EA F-5730-T0370276 P1, WINGS-
- [SDR FDEA202209142319](https://openairdocs.org/sdr/FDEA202209142319), Sep 14, 2022: DRAG FITTING. CORRODED. RH WING #2 ENGINE DRAG FITTING HOLE #8 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED #2 ENGINE DRAG FITTING HOLE #8 REPAIR IAW E.A. F-5730-T0370276 P
- [SDR FDEA202209102283](https://openairdocs.org/sdr/FDEA202209102283), Sep 10, 2022: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK F/S 1370 RBL 48 SEAT TRACK INBD FLANGE BOTTOM SIDE EXFOLIATION CORROSION. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R, MAJOR REPAIR
- [SDR FDEA202209102280](https://openairdocs.org/sdr/FDEA202209102280), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #15 HAS REJECTABLE INDICATIONS DUE TO CORROSION. COMPLIED WITH EA# T F-5730-0370300 P1 WINGS-PLATES AND SKINS-L/H WING, UPPER SKINS
- [SDR FDEA202209102279](https://openairdocs.org/sdr/FDEA202209102279), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #13 HAS REJECTABLE INDICATIONS DUE TO CORROSION COMPLIED WITH EA# T F-5730-0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN 
- [SDR FDEA202209102278](https://openairdocs.org/sdr/FDEA202209102278), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #12 HAS REJECTABLE INDICATIONS DUE TO CORROSION. COMPLIED WITH EA# T F-5730-0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN
- [SDR FDEA202209102277](https://openairdocs.org/sdr/FDEA202209102277), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #10 HAS REJECTABLE INDICATIONS DUE TO CORROSION. COMPLIED WITH EA# T F-5730-0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN
- [SDR FDEA202209102276](https://openairdocs.org/sdr/FDEA202209102276), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #5 HAS REJECTABLE INDICATIONS DUE TO CORROSION COMPLIED WITH EA# T F-5730-0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN A
- [SDR FDEA202209102275](https://openairdocs.org/sdr/FDEA202209102275), Sep 10, 2022: DRAG FITTING. CORRODED. #1 ENGINE DRAG FITTING, HOLE #8 HAS REJECTABLE INDICATIONS DUE TO CORROSION COMPLIED WITH EA# T F-5730-0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN A
- [SDR FDEA202209102274](https://openairdocs.org/sdr/FDEA202209102274), Sep 10, 2022: DRAG FITTING. CRACKED. #1 ENGINE DRAG FITTING, HOLE #4 HAS A CRACK INDICATION. COMPLIED WITH EA T F-5730-T0370300 P1, WINGS-PLATES AND SKINS-L/W WING, UPPER SKIN AT PYLON DRAG FITTING
- [SDR FDEA202209102273](https://openairdocs.org/sdr/FDEA202209102273), Sep 10, 2022: DRAG FITTING. CRACKED. #1 ENGINE DRAG FITTING, HOLE #3 HAS A CRACK INDICATION COMPLIED WITH EA# T F-5730-T0370300 P1, WINGS-PLATES AND SKINS-L/H WING, UPPER SKIN AT PYLON DRAG FITTING
- [SDR FDEA202209102272](https://openairdocs.org/sdr/FDEA202209102272), Sep 10, 2022: STRAP. CORRODED. AFT CARGO CMPARTMENT MAIN CABIN FLOOR BEAM LOWER CHORD, FLOOR BEAM STRAP CORRODED BETWEEN F/S 1400-1420. REPAIRED FLOOR BEAM STRAP @ FS 1380-1440 IAW SRM 53-00-
- [SDR FDEA202209062219](https://openairdocs.org/sdr/FDEA202209062219), Sep 6, 2022: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 232MBF IS DAMAGED FABRICATED ZONE 230 FLOOR BOARD 232MBF ON VTMAE TRAVELER # T22/1632965 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR: OR
- [SDR FDEA202209062218](https://openairdocs.org/sdr/FDEA202209062218), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 231MQF HAS IMPACT DAMAGED AS MARKED FABRICATED ZONE 230 FLOOR BOARD 231MQF ON VTMAE TRAVELER # T22/1632472 IAW DWG SRZ-25-005 REVISION R, MAJOR REPA
- [SDR FDEA202209062216](https://openairdocs.org/sdr/FDEA202209062216), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 232MJF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FLOOR BOARD 232MJF ON VTMAE TRAVELER # T22/1632426 IAW DWG SRZ- 25-005 REVISION
- [SDR FDEA202209062215](https://openairdocs.org/sdr/FDEA202209062215), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 231MJF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FOOR BOARD 231MJF ON VTMAE TRAVELER # T22/1632471 IAW DWG SRZ- 25-005 REVISION 
- [SDR FDEA202209062214](https://openairdocs.org/sdr/FDEA202209062214), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 231MEF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FLOOR BOARD 231MEF ON VTMAE TRAVELER # T22/1632449 IAW DWG SRZ- 25-005 REVISION
- [SDR FDEA202209062213](https://openairdocs.org/sdr/FDEA202209062213), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 231MBF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FLOOR BOARD 231MBF ON VTMAE TRAVELER # T22/1632443 IAW DWG SRZ- 25-005 REVISION
- [SDR FDEA202209062212](https://openairdocs.org/sdr/FDEA202209062212), Sep 6, 2022: FLOOR PANEL. DAMAGED. FLOOR PANEL 232MAF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FLOOR BOARD 232MAF ON VTMAE TRAVELER #T22/1632417 IAW DWG SRZ- 25-005 REVISON R
- [SDR FDEA202209062211](https://openairdocs.org/sdr/FDEA202209062211), Sep 6, 2022: FLOORBOARD. DAMAGED. FLOOR PANEL 231MAF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED ZONE 230 FLOOR BOARD 231MAF ON VTMAE TRAVELER # T22/1632425 IAW DWG SRZ- 25-005 REVISION
- [SDR FDEA202209062210](https://openairdocs.org/sdr/FDEA202209062210), Sep 6, 2022: FLOORBOARD. DAMAGED. FLOOR PANEL 232MBF HAS IMPACT DAMAGED AS MARKED FABRICATED ZONE 230 FLOOR BOARD 232MBF ON VTMAE TRAVELER # T22/1632420 IAW DWG SRZ- 25-005 REVISION R, MAJOR REP
- [SDR FDEA202209062209](https://openairdocs.org/sdr/FDEA202209062209), Sep 6, 2022: FLOORBOARD. DAMAGED. FLOOR PANEL 231MFF HAS MULTIPLE IMPACT DAMAGE AND WEAR MARKS FABRICATED FLOOR BOARD 231MFF ON VTMAE TRAVELER # T22/1632450 IAW DWG SRZ-25-005 REVISION R, MAJOR 
- [SDR FDEA202208302108](https://openairdocs.org/sdr/FDEA202208302108), Aug 30, 2022: DOOR. DENTED. AFT CARGO DOOR AFT LOWER CORNER BENT AND SECTIONS MISSING REPAIRED AFT CARGO DOOR LOWER AFT CORNER IAW SRM 52-30-01-2R CARGO DOOR EXTERNAL SKIN REPAIR 4, MAJOR 
- [SDR FDEA202208302107](https://openairdocs.org/sdr/FDEA202208302107), Aug 30, 2022: FLOORBOARD. DELAMINATED. COURIER AREA FLOOR BOARD 222MEF IS DELAMINATED FABRICATED COURIER AREA FLOOR BOARD 222MEF ON TRAVELER T22/1631880 IAW DWG SRZ-25- 005 REV R, MAJOR REPAIR
- [SDR FDEA202208282090](https://openairdocs.org/sdr/FDEA202208282090), Aug 28, 2022: FLOORBOARD. DELAMINATED. FLOOR BOARD 222MDF IS DELAMINATED FABRICATED COURIER AREA FLOOR BOARD 222MDF FROM TRAVELER T22/1631882 IAW DWG SRZ- 25-005 REV. R "MAJOR REPAIR"
- [SDR FDEA202208282089](https://openairdocs.org/sdr/FDEA202208282089), Aug 28, 2022: FLOORBOARD. DELAMINATED. COURIER AREA FLOOR BOARD 221BF IS DELAMINATED FABRICATED COURIER AREA FLOOR BOARD 221BF FROM TRAVELER T22/1631832 IAW DWG SRZ- 25-005 REV R, MAJOR REPAIR.
- [SDR FDEA202101220172](https://openairdocs.org/sdr/FDEA202101220172), Jan 22, 2021: GUARD. DAMAGED. DURING PREFLIGHT FOUND EMERGENCY LIGHT GUARDED SWITCH CARD BROKEN INOPERABLE. IDENTIFIED PARTS SWITCH GUARD MPN: 402-112 CPN: 3313437 QTY: 1 PART 22JAN21 05:20 
- [SDR FDEA202101120072](https://openairdocs.org/sdr/FDEA202101120072), Jan 12, 2021: BULB. INOPERATIVE. L1 DOOR ''SLIDE'' LIGHT INOPERABLE WHEN THE DOOR IS CLOSED AND THE SLIDE IS ARMED. FOLLOWING FIM 25-66-00-FT 802, REBULB PERFORMED, IAW WDM 25-66-11. TEST OK.
- [SDR FDEA202012183185](https://openairdocs.org/sdr/FDEA202012183185), Dec 18, 2020: BULB. INOPERATIVE. DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERABLE. BULB REPLACED ACC AMM 33-51-06-2-1 REV 126.7. OPERATIONS TEST SATISFACTORY.
- [SDR FDEA202012013094](https://openairdocs.org/sdr/FDEA202012013094), Dec 1, 2020: SKIN. DELAMINATED. LT OUTBOARD AFT FLAP LOWER SURFACE REPAIR AT 102 INCHES FROM INBOARD EDGE AND 10 INCHES FROM THE AFT EDGE REPAIR, REQUIRES EVALUATION TO DETERMINE IF IT WAS ACC
- [SDR FDEA202011282987](https://openairdocs.org/sdr/FDEA202011282987), Nov 28, 2020: SKIN. NOT REPORTED. FUSELAGE SKIN REPAIR WAS REPLACED BS 727-743 S21R-S22R SRM 53-00-01-2R REPAIR 16 FIG 201. ON WO 61602 SNRM N00005 18 AUG 2014. NEW SDR RAISED DUE WRONG SDR ATTA
- [SDR FDEA202011253086](https://openairdocs.org/sdr/FDEA202011253086), Nov 25, 2020: FLOORBEAM. WORN. CABIN FLOOR BEAM INTERCOSTALS ABOVE FWD CARGO AFT BULKHEAD STACHNIONS AT BSTA 845 LBL & RBL 16.05 HAVE ELONGATED HOLES WHERE STACHION PINS LOCATE. REPLACED INTE
- [SDR FDEA202011253066](https://openairdocs.org/sdr/FDEA202011253066), Nov 25, 2020: SKIN. DENTED. LT INBOARD MAIN FLAP UPPER SURFACE HAS SMALL PUNCTURE HOLE. REPAIRED DAMAGES, IAW SRM 51-70-07-0G AND FEDEX EA F-5730-T0358461 "WING-FLIGHT SURFACES-LT INBOARD 
- [SDR FDEA202011243052](https://openairdocs.org/sdr/FDEA202011243052), Nov 24, 2020: PANEL. DENTED. RT VERTICAL STABILIZER PANEL 175N2001 IS DAMAGED. DAMAGE IS 13.5" FROM L EDGE OF PANEL AND 15" FROM BOTTOM OF PANEL PLEASE EVA. REPAIRED SMALL PUNCTURE ON THE O
- [SDR FDEA2020031210533](https://openairdocs.org/sdr/FDEA2020031210533), Mar 11, 2020: DOOR. LACK OF LUBE. PDIS 916 52-00 2660 11MAR20 CDG FACT U LEFT ENTRY DOOR DIFFICULTY TO CLOSE. PERFORMED LEFT ENTRY DOOR LUBRICATION AS PER AMM 12-21-18-3. OPS CHECK OK. DOOR NO M
- [SDR FDEA201912203274](https://openairdocs.org/sdr/FDEA201912203274), Dec 20, 2019: LIGHT. INOPERATIVE. DURING SERVICE CHECK FOUND RT EXTERIOR EMERGENCY LIGHT INOP. SERVICED RIGHT EMERGENCY SLIDE LIGHT WITH NEW BULB P/N 767 AS PER MM 33-51-06-2-1. ALL TEST PASSED,
- [SDR FDEA201909072150](https://openairdocs.org/sdr/FDEA201909072150), Sep 7, 2019: SHUTOFF VALVE. FAILED. PDIS 916 36-11 2170 07SEP19 CPH OPEN U LOGPAGES:2531648 R ENG BLEED OFF EICAS MSG JUST BEFORE V1. COMPELED WITH QHR PROCEDURE. SHGN 07SEP19 20:50 CPH U PROCEEDI
- [SDR FDEA201907121536](https://openairdocs.org/sdr/FDEA201907121536), Jul 12, 2019: WARNING SYSTEM. FALSE ACTIVATION. RECEIVED "GEAR DISAGREE" EICAS WHEN THE GEAR WAS RAISED. THE EICAS REMAINED ON FOR APPROXIMATLEY 4 SEC. ALL OTHER INDICATIONS WERE NORMAL. PSEU BITE PERFORMED N

All 242: https://openairdocs.org/model/boeing-757-27b/reports.md

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