# N920FD: Boeing 757-23A

- Status: Valid registration
- Airframe: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (registry code 1384967, 178 seats)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (The Boeing Company) (OpenAirDocs)
- Serial number: 24289
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: December 13, 2007
- Expires: February 28, 2029
- Mode S code: ACBEAB
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=920FD
- Page: https://openairdocs.org/aircraft/N920FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Boeing 757-23A)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N920FD.

## FAA accident and incident reports

None matched to N920FD.

## Service difficulty reports (222, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202605280647](https://openairdocs.org/sdr/FDEA202605280647), May 28, 2026: ADC. FAULTED. ALTITUDE DISAGREE TWO TIMES DURING DESCENT. FO ALTIMETER MATCHED THE STANDBY AND WAS 400 FEET DIFFERENT THAN CAPTAINS AMM: 34-12-01-4 REMOVED AND REPLACED CAPTA
- [SDR FDEA202501150070](https://openairdocs.org/sdr/FDEA202501150070), Jan 15, 2025: BATTERY. FAILED. EMERGENCY LIGHTS FOR R1 DOOR AND CENTER COURIER AREA INOP. IAW AMM: 33-51-07-2 REMOVED AND REPLACED BATERYPACK ASSY FOR CHARGER ASSEMBLY M730. OPS CHECK GOOD.
- [SDR FDEA202311211876](https://openairdocs.org/sdr/FDEA202311211876), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-13 BTW RBL 46-50 AND STA 720- 780. REMOVED FLOOR PANEL P\N 11864182-13 FROM STA 720-780 IAW B-757 AMM 53
- [SDR FDEA202311211875](https://openairdocs.org/sdr/FDEA202311211875), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-21 BTW RBL 46-50 AND STA 780- 880. REMOVED FLOOR PANEL #11862182-21 FROM STA 780 - 880 IAW (B 757) AMM 5
- [SDR FDEA202311211874](https://openairdocs.org/sdr/FDEA202311211874), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-10 BTW RBL 46-50 AND STA 1320- 1420. REMOVED FLOOR PANEL P\N 11862182-10 FROM STA 1320-1420 BTW RBL 46-5
- [SDR FDEA202311211873](https://openairdocs.org/sdr/FDEA202311211873), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-2 BTW RBL 46-50 AND STA 900- 1020. REMOVED FLOOR PANEL P\N 11862182-2 FROM STA 900-1020 BTW IAW B-757 AM
- [SDR FDEA202311211872](https://openairdocs.org/sdr/FDEA202311211872), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND DENT AT MAIN CARGO FLOOR PANE; P\N: 11862182-28 BTW RBL 46-50 AND STA 880-900 REMOVED FLOOR PANEL P\N 11862182-28 FROM STA 880-900 BTW RBL 46- RBL 50 IAW 
- [SDR FDEA202311211871](https://openairdocs.org/sdr/FDEA202311211871), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 6EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-2 BTW RBL 46-50 AND STA 1200- 1320. REMOVED FLOOR PANEL P\N 11864182-2 FROM STA 1200-1320 IAW B-757 AMM 
- [SDR FDEA202311211870](https://openairdocs.org/sdr/FDEA202311211870), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 4EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-26 BTW RBL 46-50 AND STA 1100- 1200. REMOVED FLOOR PANEL P\N 11863182-26 FROM STA 1100-1200 IAW B-757 AM
- [SDR FDEA202311211869](https://openairdocs.org/sdr/FDEA202311211869), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-38 BTW RBL 46-50 AND STA 1055- 1100. REMOVED FLOOR PANEL P\N 11862182-38 FROM STA 1055-1100 IAW B-757 AM
- [SDR FDEA202311211868](https://openairdocs.org/sdr/FDEA202311211868), Nov 21, 2023: FLOOR PANEL. DENTED. FOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-34 BTW RBL 46-50 AND STA 1020- 1055. REMOVED FLOOR PANEL P\N 11862182-34 FROM STA 1020-1055 IAW B-757 AM
- [SDR FDEA202311201865](https://openairdocs.org/sdr/FDEA202311201865), Nov 20, 2023: FLOORBEAM. CORRODED. MAIN CABIN FLOOR BEAM AT STA 880 LBL 48 TO 62 LBL SURFCE CORROSION. DOT 101. ACCOMPLISHED EA F-5321-T0376857 P1 "FUSELAGE MAINFRAME SECTION 43, FLOOR BEAM ASSY 
- [SDR FDEA202311191864](https://openairdocs.org/sdr/FDEA202311191864), Nov 19, 2023: FRAME. UNKNOWN. DURING FUSELAGE MAINFRAME - AFT CARGO COMPARTMENT FRAME INSPECTION PER EO NO. F- 5310-E0347443 B P1 EXISTING REPAIR WAS FOUND AT STA 1300 BTW STRG 26L-27L CONTA
- [SDR FDEA202311061834](https://openairdocs.org/sdr/FDEA202311061834), Nov 6, 2023: SLAT. DEBONDED. #5 SLAT FOUND DISBONDED. INSTALLATION OF #5 SLAT TO BE ACCOMPLISHED ON NR00110. NR ATTACHED. REPAIRED DISBONDING ON #5 SLAT IAW B757 SRM 51-70-10-2R, B757 SRM 5
- [SDR FDEA202311061833](https://openairdocs.org/sdr/FDEA202311061833), Nov 6, 2023: SLAT. DEBONDED. #2 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #2 SLAT FOR DISBONDING REPAIR IAW B757 AMM 27-81-02-4, B757 SRM 51-70-10-2R, B757 SRM 51-20-01-0G, B757 AMM 51-
- [SDR FDEA202311061832](https://openairdocs.org/sdr/FDEA202311061832), Nov 6, 2023: SKIN. DEBONDED. #8 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #8 SLAT FOR DISBONDING REPAIR IAW B757 SRM 51-70-10-2R, B757 AMM 27-81-02-4, B757 AMM 51-21-15-7, AND B757 SRM 
- [SDR FDEA202309261652](https://openairdocs.org/sdr/FDEA202309261652), Sep 26, 2023: UNKNOWN. UNKNOWN. PDIS 920 32-51 5203 26SEP23 TLV FACT U AFTER LANDING NOSEWHEEL MADE A CLUNKING SOUND WHEN ENGAGING TILLER TO TURN. I.A.W FIM 32-51 FAULT TREE 813 BLOCK 1, STEER
- [SDR FDEA202302220331](https://openairdocs.org/sdr/FDEA202302220331), Feb 22, 2023: NONE. NONE. PDIS 920 25-60 4604 22FEB23 CDG FACT U SLIDE LIGHT DOES NOT ILLUMINATE WHEN MAIN ENTRY DOOR CLOSED AND ARMED. FACT 22FEB23 02:16 CDG U AMM 25-66-01-6 PERFORMED 
- [SDR FDEA202301190139](https://openairdocs.org/sdr/FDEA202301190139), Jan 19, 2023: BULB. FAILED. PDIS 920 52-10 4503 19JAN23 CDG FACT U DOOR L1 SLIDE LIGHT BURNT OUT FACT 19JAN23 18:59 CDG U AMM: 52-11-25-5 REBULBED SLIDE LIGHT AS PER SWPM AND TESTED OK IAW
- [SDR FDEA202301110068](https://openairdocs.org/sdr/FDEA202301110068), Jan 11, 2023: BULB. FAILED. PDIS 920 33-50 4480 11JAN23 BER FACT U SLIDE ARMED LIGHT ON L1 OUT FACT 11JAN23 11:26 BER U AMM: 33-51-06-2-1 REV.130.13 BULB,S REPLACED ON SLIDE LIGHT ARMED / 
- [SDR FDEA202208302101](https://openairdocs.org/sdr/FDEA202208302101), Aug 30, 2022: CONTROL VALVE. FAULTED. RIGHT PACK OVERTEMP AND FAILED INFLIGHT. LEFT WAS MEL ED,DESCENDED BELOW 10000 ON OXYGEN. EMERGENCY DECLARED. AMM21-51-00-5, FIM21-51 TREE 803, 805. PERFORMED O
- [SDR FDEA202205121193](https://openairdocs.org/sdr/FDEA202205121193), May 12, 2022: TRANSMITTER. FAULTED. PDIS 920 27-50 3732 12MAY22 CDG OPEN U TE FLAP DISAGREE WHEN SELECTING FLAP 20. RAN QRH, USED ALTN FLAP CONTROLLER TO LAND FLAPS 20. ***EMERGENCY DECLARED*** SH
- [SDR FDEA202203090595](https://openairdocs.org/sdr/FDEA202203090595), Mar 19, 2022: ADC. UNKNOWN. PDIS 920 34-16 3550 19MAR22 CDG OPEN U ON CLIMB THRU APPROXIMATELY FL280, THE FIRST OFFICER S SPEED TAPE READ, NO SPD AND THE ALTIMETER JUMPED SEVERAL HUNDRED F
- [SDR FDEA202201190099](https://openairdocs.org/sdr/FDEA202201190099), Jan 19, 2022: FLOOR PANEL. WORN. MAIN DECK FLOOR PANEL #223MDF STATION 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005 REF. ENGINEERING DISPOSITION OF RFTA NO:02841-0205. 
- [SDR FDEA202201190098](https://openairdocs.org/sdr/FDEA202201190098), Jan 19, 2022: FLOOR PANEL. WORN. MAIN DECK FLOOR PANEL #221BF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRX-25-005 REF. ENGINEERING DESPOSITION OF RFTA NO:02841-0205. MAJOR
- [SDR FDEA202201190096](https://openairdocs.org/sdr/FDEA202201190096), Jan 19, 2022: FLOOR PANEL. WORN. MAIN DECK FLOOR PANEL #222 MAF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ 25-005 REF. ENGEENIRING DISPOSITION OF RFTA NO: 02841-0205. MA
- [SDR FDEA202201160075](https://openairdocs.org/sdr/FDEA202201160075), Jan 16, 2022: FLOOR PANEL. WORN. MAIN DECK FLOOR PANEL #221MBF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005. REF ENGINEERING DISPOSITION OF RFTA NO: 02841-0205. MAJ
- [SDR FDEA202201060169](https://openairdocs.org/sdr/FDEA202201060169), Jan 6, 2022: SEAT TRACK. CORRODED. STA 480-620, LBL 45.50, FOUND CORROSION ON SEAT TRACK WORK ACCOMPLISHED IN ACCORDANCE WITH EO #F-5310-T0366384. MAJOR REPAIR.
- [SDR FDEA202112280178](https://openairdocs.org/sdr/FDEA202112280178), Dec 28, 2021: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BL 0, STA 1330-1320. WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5310-T0366212
- [SDR FDEA202112280168](https://openairdocs.org/sdr/FDEA202112280168), Dec 28, 2021: NONE. CORRODED. FOUND CORROSION ON FLOOR BEAM EXISTING REPAIR AT STA 1320 BETWEEN RBL24 TO RBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EO # F-5310-T0366466
- [SDR FDEA202112280167](https://openairdocs.org/sdr/FDEA202112280167), Dec 28, 2021: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK RBL 45 BETWEEN STA 1320 TO 1420 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED 2 EA SEAT TRACKS SECTION, 2 EA SPLICES , AND 1 EA
- [SDR FDEA202112280166](https://openairdocs.org/sdr/FDEA202112280166), Dec 28, 2021: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK RBL 24 ON STA 1320 AND STA 1410 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED SEAT TRACK SECTION, 2 EA SPLICES , AND 1 EA STRAP
- [SDR FDEA202112280122](https://openairdocs.org/sdr/FDEA202112280122), Dec 28, 2021: FRAME. UNKNOWN. FOUND UNDOCUMENTED WEB REPAIR AT STA 1375 OUTBD CREASE BEAM ON R/H SIDE PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W BOEING SR:1-198375510 AND NO DAMA
- [SDR FDEA202112090121](https://openairdocs.org/sdr/FDEA202112090121), Dec 9, 2021: FRAME SPLICE. UNKNOWN. EVALUATE SUPPORT AT STA 1020, STR 5L & 5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W EA F-5310-T0366310 AND NO DAMAGE OR DEVIATIO
- [SDR FDEA202112090120](https://openairdocs.org/sdr/FDEA202112090120), Dec 9, 2021: FRAME SPLICE. UNKNOWN. EVALUATE SUPPORT AT STA 980, S-5L PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366306 AND NO DAMAGE OR DEVIATIONS NOTED.
- [SDR FDEA202112090119](https://openairdocs.org/sdr/FDEA202112090119), Dec 9, 2021: FRAME SPLICE. UNKNOWN. EVALUATE SUPPORT AT STA 1100, S5L TO S-5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366309 AND NO DAMAGE OR DEVIATION
- [SDR FDEA202111222930](https://openairdocs.org/sdr/FDEA202111222930), Nov 22, 2021: NONE. DAMAGED. PDIS 920 25-10 3302 22NOV21 CDG FACT U FO SHOULDER RESTRAINTS DO NOT RETRACT. FACT 23NOV21 11:54 CDG INSPECTED F/O SEAT SHOULDER HARNESS PER MM 25-11-00-17 OPS 
- [SDR FDEA202108262099](https://openairdocs.org/sdr/FDEA202108262099), Aug 26, 2021: LINE. UNSECURE. L1 DOOR DIFFICULT TO CLOSE AND ARM FOUND EMERGENCY SLIDE STATIC LINE LOOSE AND BUCKLE DANGLING CAUSING INTERFERENCE. REPOSITIONED IAW AMM 25-66-01-4. OPS TEST O
- [SDR FDEA202106291620](https://openairdocs.org/sdr/FDEA202106291620), Jun 29, 2021: SENSOR. DIRTY. L1 DOOR SLIDE LIGHT INOP UPON LANDING. DOOR 1L GIRT BAR FITTINGS, SLIDER AND PROXIMITY SENSOR CLEANED FROM DEBRIS. GIRT BAR CYCLED SEVERAL TIMES AND SLIDE ARMED
- [SDR FDEA202106111497](https://openairdocs.org/sdr/FDEA202106111497), Jun 11, 2021: BULB. INOPERATIVE. DOOR 1L SLIDE ARM LIGHT INTERMITTENT, MOSTLY INOP LH SLIDE ARMED INDICATOR LIGHT BOTH BULBS REPLACED IAW SWPM 20-84-18 IAW AMM 52-11-00, LH SLIDE HAS BEEN ARMED
- [SDR FDEA202105261402](https://openairdocs.org/sdr/FDEA202105261402), May 26, 2021: BULB. INOPERATIVE. PDIS 920 25-60 2709 26MAY21 CDG OPEN U LOGPAGES:3001081 1L SLIDE ARMED LIGHT DID NOT ILLUMINATE WHEN ARMED RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : 
- [SDR FDEA202104210963](https://openairdocs.org/sdr/FDEA202104210963), Apr 21, 2021: CASE. CORRODED. ENGINE #1 LP COMPRESSOR FRONT CASE OUTER SURFACE FORWARD OF KEVLAR WRAPPING IS CORRODED FROM 4 O'CLOCK TO 12 O'CLOCK POSITION (AFT LOOKING FORWARD) SNRM RECTIFI
- [SDR FDEA202104010808](https://openairdocs.org/sdr/FDEA202104010808), Apr 1, 2021: VALVE. FAILED. LEFT ENGINE WOULD NOT SHUTDOWN WHEN FUEL CUTOFF MOVED TO CUTOFF. IT RAN FOR APPROXIMATELY 25 SECONDS BEFORE SHUTTING DOWN. REMOVED L/H ENGINE FUEL FLOW GOVERNOR
- [SDR FDEA202009142212](https://openairdocs.org/sdr/FDEA202009142212), Sep 14, 2020: MECHANISM. BROKEN. DURING PRE-FLIGHT CHECK, FLIGHT CREW NOTE L1 DOOR MECHANISM IS BROKEN. REMOVED AND REPLACED COLLAR ASSY FROM THE L1 DOOR MECHANISM PER AMM 52-11-08-8. OPENED AN
- [SDR FDEA2020061981284](https://openairdocs.org/sdr/FDEA2020061981284), Jun 18, 2020: GIRT BAR. OUT OF ADJUST. R1 DOOR IS VERY STICKY TO DISARM. PERFORMED RT DOOR GIRT BAR ADJUSTMENT PER AMM 52-11-25-5-0. PERFORMED OPERATIONAL CHECK ON RT DOOR AND FOUND OK PER THE SAME A
- [SDR FDEA2020061091158](https://openairdocs.org/sdr/FDEA2020061091158), Jun 9, 2020: UNKNOWN. MALFUNCTIONED. UNABLE TO ARM RIGHT FWD ENTRY DOOR. OPS CHECK PER AMM 52-11-00-5, TEST SATIS, A/C OK FOR SERVICE.
- [SDR FDEA2020051390843](https://openairdocs.org/sdr/FDEA2020051390843), Apr 29, 2020: SLIDE. UNSERVICEABLE. L1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBE
- [SDR FDEA2020043090843](https://openairdocs.org/sdr/FDEA2020043090843), Apr 29, 2020: SLIDE. OUT OF LIMITS. L1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBE
- [SDR FDEA2020021490329](https://openairdocs.org/sdr/FDEA2020021490329), Feb 9, 2020: SKIN. DAMAGED. MDIS 920 51-00 1440 09FEB20 LGG OPEN U AFT CARGODOOR AND SKIN BEHIND GOT HIT BY ULD ON THE DRIFT WITH HIGH WINDS, CARGO DOOR HAS A HOLE , SKIN BEHIND IS DEFORME
- [SDR FDEA201912133242](https://openairdocs.org/sdr/FDEA201912133242), Dec 13, 2019: FLOOR PANEL. DAMAGED. AFT CARGO PANEL # 161AF DAMAGED REPLACED AFT CARGO PANEL 161AF IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING # 453N1805.

All 222: https://openairdocs.org/aircraft/N920FD/reports.md

## STCs that may be installed (OpenAirDocs) (5)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Boeing 757-23A)

- [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 757 Series
- [STC ST01675CH](https://openairdocs.org/stc/ST01675CH): Installation of Butterfly Valve Ring AIR23028 in starter control valves, part number 775538 or 799700. Cook Airtomic. Lists 757 Series
- [STC ST02296AT](https://openairdocs.org/stc/ST02296AT): Upgrade existing HF Voice Communication System to provide HF datalink capability. ARINC, Inc. Lists 757 Series
- [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 757 Series
- [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 757 Series

## Related

- Other Boeing 757-23A aircraft: https://openairdocs.org/model/boeing-757-23a/aircraft.md

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