# N939FD: 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: 24528 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: December 6, 2010 - Expires: December 31, 2029 - Mode S code: AD0799 - 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=939FD - Page: https://openairdocs.org/aircraft/N939FD 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 N939FD. ## FAA accident and incident reports None matched to N939FD. ## Service difficulty reports (141, 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 FDEA202608201198](https://openairdocs.org/sdr/FDEA202608201198), Aug 20, 2026: BATTERY PACK. FAILED. INTERIOR EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED FWD BATTERY POWER SUPPLY IAW ABOVE REF. AFTER REPLACMENT FOUND CTR EXIT LIGHT AND R1 EXIT LIGHT OPS CHK - [SDR FDEA202606240800](https://openairdocs.org/sdr/FDEA202606240800), Jun 24, 2026: UNKNOWN. ODOR. AFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR - [SDR FDEA202605080570](https://openairdocs.org/sdr/FDEA202605080570), May 8, 2026: SKIN. DAMAGED. LH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND - [SDR FDEA202604180469](https://openairdocs.org/sdr/FDEA202604180469), Apr 18, 2026: FSEU. FAILED. WHILE CONFIGURING FOR LANDING, AS WE SELECTED FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE ON EICAS. INDICATOR REMAINED AT FLAPS 20. COMPLIED WITH QRH. RETRACTED F - [SDR FDEA202603190358](https://openairdocs.org/sdr/FDEA202603190358), Mar 19, 2026: FSEU. FAILED. UPON SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE EICAS. FLAP HANDLE WAS AT 25 BUT THE FLAPS WERE AT 20. RAN QRH, RETRACTED FLAPS TO UP USING ALT FLAPS AND DI - [SDR FDEA202404030435](https://openairdocs.org/sdr/FDEA202404030435), Apr 3, 2024: LAMP. BURNED OUT. L1 MAIN ENTRY DOOR SLIDE LIGHT IS BURNT OUT. REMOVED AND REPLACED BOTH BULBS AND PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00-2-0, TEST SATIS, A/C OK FOR SERVICE. - [SDR FDEA202311101847](https://openairdocs.org/sdr/FDEA202311101847), Nov 10, 2023: RESERVOIR. LEAKING. DURING POST FLIGHT INSPECTION, FOUND LEFT PASSENGER DOOR (#1) EMERGENCY POWER RESERVOIR WITH LESS THAN 2000PSI. REPLACED NO. 1 PASSENGER DOOR EMERGENCY POWER RE - [SDR FDEA202309111573](https://openairdocs.org/sdr/FDEA202309111573), Sep 11, 2023: FITTING. CRACKED. #1 ENG PYLON DRAG FITTINGS REMOVAL REQUIRED PER EA F-5730-T0375771 REPAIR PERFORMED PER EA #F-5730-T0375771 P1 EA TITLE WINGS-PLATES AND SKINS-LH WING UPPER SKI - [SDR FDEA202309111571](https://openairdocs.org/sdr/FDEA202309111571), Sep 11, 2023: FITTING. CRACKED. #2 ENG PYLON DRAG FITTINGS REMOVAL PER EA ORDER # F-5730-T0375772 REPAIR PERFORMED PER EA # F-5730-T0375772 EA TITLE WINGS-PLATES AND SKINS-RH WING UPPER SKIN A - [SDR FDEA202211292855](https://openairdocs.org/sdr/FDEA202211292855), Nov 29, 2022: BULB. INOPERATIVE. MAIN CARGO DECK DOOR CANOPY POSITION LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW SMP, PERFORMED CANOPY POSITION INDICATOR TEST IAW AMM 52-72-02-2. OPS - [SDR FDEA202208121971](https://openairdocs.org/sdr/FDEA202208121971), Aug 12, 2022: PROBE. DIRTY. PDIS 939 77-15 0226 11AUG22 CDG FACT U ON CLIMB OUT LEFT ENGINE PRODUCED APPROX. 1/3 LESS POWER THAN RIGHT ENGINE. CONTACTED GOC/MOC WITH PARAMETERS AND CONTINU - [SDR FDEA202102050296](https://openairdocs.org/sdr/FDEA202102050296), Feb 5, 2021: APU. ODOR. PDIS 939 21-70 8622 05FEB21 LGG OPEN U LOGPAGES:3301364 OBSERVED AN ACRID, BURNING OIL SMELL DURING ALL PHASES OF FLIGHT WITH MARKED INTENSITY ON APU BLEED, CLI - [SDR FDEA202101130073](https://openairdocs.org/sdr/FDEA202101130073), Jan 13, 2021: LOCK. LOOSE. LEFT FWD ENTRY DOOR GIRT BAR IS LOOSE AND NEEDS TO BE RESTOWED. REINSTALLED L/H DOOR GIRT BAR AND GIRT BAR SLIDER WITH HIS PROX SWITCH TARGET AS PER AMM 25-66-1 - [SDR FDEA202010122531](https://openairdocs.org/sdr/FDEA202010122531), Oct 12, 2020: PANEL. DELAMINATED. DELAMINATION FOUND ON RT HORIZ STAB UPPER PANEL, FWD TORQUE BOX UPPER INBOARD PANEL. PERFORMED A CATEGORY C REPAIR, RESIN INJECTION TO UPPER SUFACE OF RT HORIZ - [SDR FDEA202008252031](https://openairdocs.org/sdr/FDEA202008252031), Aug 25, 2020: SEAL. LEAKING. DURING REFUELING FOUND RUNNING FUEL LEAKAGE FROM CENTER TANK (RIGHT WING TO AIR CONDITIONING FAIRING), IAW ENGINEERING (EMAIL) GVI DONE AROUND THE LEAK AREA, NO - [SDR FDEA2020030520480](https://openairdocs.org/sdr/FDEA2020030520480), Mar 2, 2020: COMPUTER. FAILED. ON TAXI OUT WE RECEIVED MULTIPLE WARNING AND CAUTIONS TO INCLUDE: GEAR NOT DOWN, SPOILER, APU FIRE, FWD CARGO FIRE. MULTIPLE CAUTIONS WERE PRESENT. THEY LASTED - [SDR FDEA2019101762663](https://openairdocs.org/sdr/FDEA2019101762663), Oct 16, 2019: STRINGER. DAMAGED. STRINGERS 1 AND 2R @ BS1513 AND BS1507 HAVE INCORRECTLY DRILLED HOLES FOUND DURING ACCOMPLISHMENT OF E.A.#F-2560-150815D. - [SDR FDEA2019101102589](https://openairdocs.org/sdr/FDEA2019101102589), Oct 10, 2019: BRACKET. CRACKED. NR 2 PYLON AFT LOWER PAN HAD TWO MOUNT BRACKETS CRACKED. REPLACED THE MOUNT BRACKETS IAW SRM 51-40-02. - [SDR FDEA2019101092531](https://openairdocs.org/sdr/FDEA2019101092531), Oct 9, 2019: PANEL. DELAMINATED. DELAMINATION FOUND ON AFT CORNER OF LEFT HORIZONTAL STABILIZER TE PANEL 335EB. REPAIRED THE TE PANEL IAW SRM 51-70-17-0G, PARAGRAPH 4A(2), AND FIG 23 SRM REV 12 - [SDR FDEA2019101092530](https://openairdocs.org/sdr/FDEA2019101092530), Oct 9, 2019: RETAINER. CORRODED. RIGHT WING UPPER FIXED TE AREA OUTBOARD OF AILERON ACTUATORS, FIXED TE SEAL RETAINER CORRODED. THE SEAL RETAINER WAS REPLACED IAW DRAWING 113N1640 AND GMM 7-0-1 - [SDR FDEA2019101082492](https://openairdocs.org/sdr/FDEA2019101082492), Oct 8, 2019: SUPPORT ANGLE. DAMAGED. FORWARD CARGO DOOR ANGLE SUPPORT DAMAGED AT LOWER FORWARD DOORSTOP AREA. REPLACED ANGLE SUPPORT (BRACKET) IAW SRM 51-40-02, BOEING DRAWING 140N2891 AND GMM 07-0 - [SDR FDEA201910072482](https://openairdocs.org/sdr/FDEA201910072482), Oct 7, 2019: SUPPORT BRACKET. CRACKED. NR 2 PYLON AFT FAIRING AREA SUPPORT BRACKET CRACKED, BELOW FLOW LIMITER, REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, REV 128, AND DRAWING 313N5021. - [SDR FDEA201910072481](https://openairdocs.org/sdr/FDEA201910072481), Oct 7, 2019: FLOOR PANEL. DAMAGED. FLOOR PANEL, BS 560 - 680, RT OTBD WAS DAMAGED. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50, REV 128. - [SDR FDEA201910072480](https://openairdocs.org/sdr/FDEA201910072480), Oct 7, 2019: SKIN. SCRATCHED. SURFACE SCRATCHES ON THE FUSELAGE SKIN AT BS 900 - 920. FOUND TO BE OUTSIDE PERMITTED LIMITS. REPAIRED IAW EA F-5330-T0349853 P (1). - [SDR FDEA201909262602](https://openairdocs.org/sdr/FDEA201909262602), Sep 26, 2019: BEAM. CORRODED. FWD CARGO DOOR LOWER EDGE BEAM AND SPLICES FOUND CORRODED REMOVED CORROSION IAW SRM 52-30-02-1A FIG 101 DETAIL IV AND FOUND TO BE OUT OF LIMITS.MAX ALLOWABLE BL - [SDR FDEA2019101122585](https://openairdocs.org/sdr/FDEA2019101122585), Sep 26, 2019: SKIN. CORRODED. FWD CARGO DOOR LOWER SKIN CORROSION ON INTERNAL SKIN REMOVED CORROSION ON LOWER INNER SKIN AT LOCATIONS 12" AND 18" FROM FORWARD EDGE AND 12" FROM AFT EDGE AND - [SDR FDEA201909172293](https://openairdocs.org/sdr/FDEA201909172293), Sep 17, 2019: GATE. CORRODED. DOOR 2L UPPER GATE HAS EVIDENCE OF PITTING AT HINGE LINE AT EXTERIOR SURFACE. DOOR 2L UPPER GATE REPLACED IAW DWG #146N6105. - [SDR FDEA2019101462611](https://openairdocs.org/sdr/FDEA2019101462611), Sep 16, 2019: SKIN. DELAMINATED. RIGHT STAB HAS UPPER SURFACE DELAMINATION IN AREA JUST ADJACENT TO THE FUSELAGE, RT HORIZONTAL STABILIZER UPPER INBOARD FIXED LE PANEL MPN.185N3001-50 REPAIRED - [SDR FDEA2019091432634](https://openairdocs.org/sdr/FDEA2019091432634), Sep 13, 2019: SKIN. DELAMINATED. THE R/H I/B MAIN FLAP LOWER SURFACE PANEL 113N2402-4 HAS DELAM AND REQUIRES REPAIR REPAIRED THE R/H I/B MAIN FLAP LOWER SURFACE PANEL IAW SRM 57-53-01-0I FIG 1, - [SDR FDEA2019101092534](https://openairdocs.org/sdr/FDEA2019101092534), Sep 13, 2019: SKIN. WORN. RIGHT WING OTBD FLAP UPPER INBD PANEL WAS WORN FROM MAKING CONTACT WITH THE NUMBER 10 SPOILER. REPAIRED IAW EA F-5750-T0349728 P1. - [SDR FDEA201909132356](https://openairdocs.org/sdr/FDEA201909132356), Sep 13, 2019: SKIN PANEL. CORRODED. FUSELAGE SKIN HAS EVIDENCE OF CORROSION ON INNER SURFACE AT APU INLET DOOR PANEL FORWARD ATTACHMENT AREA CORROSION FOUND TO BE OUTSIDE LIMITS ,SKIN PANEL REPLAC - [SDR FDEA201909132355](https://openairdocs.org/sdr/FDEA201909132355), Sep 13, 2019: SUPPORT ANGLE. CORRODED. APU INLET DOOR PANEL SUPPORT ANGLE CORRODED AT LOWER FORWARD CUTOUT BS1792 APU INLET DOOR PANEL SUPPORT ANGLE REPLACED IAW BOEING DWG #148N3105 AND SRM 51-40-02 - [SDR FDEA2019101402612](https://openairdocs.org/sdr/FDEA2019101402612), Sep 10, 2019: SKIN. DENTED. NR 5 SLAT LEADING EDGE DAMAGED. REPAIRED IAW SRM 57-43-01-2R REPAIR 9 FIG 201 DETAIL VII AND EA F-5750-T0349924 P1. - [SDR FDEA2019101192588](https://openairdocs.org/sdr/FDEA2019101192588), Sep 9, 2019: SUPPORT. CORRODED. FORWARD CARGO DOOR EVIDENCE OF BULGING OF LEVELING COMPOUND AT LOWER DOOR AREA REMOVED LEVELLING COMPOUND, CORROSION FOUND AT LOWER DOOR INNER SKIN ,EDGE BEAM A - [SDR FDEA2019101192587](https://openairdocs.org/sdr/FDEA2019101192587), Sep 9, 2019: TEE FITTING. CORRODED. FORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM FORWARD EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWE - [SDR FDEA2019101192586](https://openairdocs.org/sdr/FDEA2019101192586), Sep 9, 2019: SKIN. CORRODED. FORWARD CARGO DOOR EVIDENCE OF CORROSION ON DOOR INNER SKIN AT LOWER CUTOUT AREA 12" FROM AFT EDGE OF CARGO DOOR COROSION REMOVED AT DOOR INNER SKIN AT LOWER CU - [SDR FDEA201909092475](https://openairdocs.org/sdr/FDEA201909092475), Sep 9, 2019: SKIN. GOUGED. LEFT STAB CUT-OUT LOWER SKIN HAD GOUGES AT 10.5, 22, 33, AND 43.5 INCHES FROM THE FWD EDGE. EVALUATED AND FOUND THE GOUGES AT 10.5 AND 22 INCHES WERE OUT OF LIM - [SDR FDEA2019100792445](https://openairdocs.org/sdr/FDEA2019100792445), Sep 9, 2019: RIB. CORRODED. RIGHT AILERON ATTACHMENT RIB AT WING STA 810 WAS CORRODED AT BONDING LEAD ATTACHMENT. CORROSION REMOVED IAW SRM 51-10-02 AND EVALUATED IAW SRM 57-51-09-1A FIG 1 - [SDR FDEA201909092349](https://openairdocs.org/sdr/FDEA201909092349), Sep 9, 2019: SKIN. GOUGED. BLEND IN FUSELAGE SKIN AROUND FASTENER AT BS1350 BETWEEN S5L AND S6L MEASURED AND EVALUATED PREVIOUS BLEND ON FUSELAGE SKIN AT BS 1350 BETWEEN S.5L AND S.6L IAW - [SDR FDEA2019100762476](https://openairdocs.org/sdr/FDEA2019100762476), Sep 6, 2019: SKIN. WORN. WEAR FOUND ON THE SKIN PANEL FWD SIDE OF HORIZONTAL STAB CUT OUT LT SIDE AT THE BRACKET MOUNTED ON LWR LONGERON. EVALUATED THE SKIN PANEL AND FOUND TO BE OUTSID - [SDR FDEA2019101042495](https://openairdocs.org/sdr/FDEA2019101042495), Sep 4, 2019: BRACKET. CORRODED. BRACKET ON AFT SIDE OF BULKHEAD BS 1787, UPPER SIDE OF APU INTAKE DUCT WAS CORRODED. BRACKET FABRICATED IAW DWG 148N3141 AND INSTALLED IAW SRM 51-40-02. - [SDR FDEA201909042358](https://openairdocs.org/sdr/FDEA201909042358), Sep 4, 2019: SUPPORT ANGLE. CORRODED. STRAP ON LOWER SIDE OF APU INTAKE DUCT BS 1787-1825 IS CORRODED RECTIFY REMOVED AND REPLACED APU INTAKE LOWER SUPPORT ANGLE (STRAP), IAW BOEING DWG #148N3105 AN - [SDR FDEA2019100732456](https://openairdocs.org/sdr/FDEA2019100732456), Sep 3, 2019: SKIN. CRACKED. UPPER HINGE CUTOUT R2 DOOR HAD A SUPECTED CRACK ON THE LOWER CORNER. A REPAIR WAS CARRIED OUT IAW SRM 52-10-02-2R, REPAIR 1, FIG 201, AND EA F-52-10-T0349827 P1 - [SDR FDEA201909032111](https://openairdocs.org/sdr/FDEA201909032111), Sep 3, 2019: FILLER. NICKED. SMALL MARK (NICK) FOUND ON UPPER AFT EDGE OF FRAME AT BSTA 231.25 BL 0. REMOVED DAMAGED FILLER OF PREVIOUS REPAIR AND REPLACED FILLER IAW SRM 53-00-07 REPAIR 7. - [SDR FDEA201904260925](https://openairdocs.org/sdr/FDEA201904260925), Apr 26, 2019: WARNING MESSAGE. FALSE ACTIVATION. CLIMBING OUT OF FL 300 WE RECEIVED AN EICAS "CAB ALT" MESSAGE. CABIN ALTITUDE EXCEEDED 10,000 FT. AS INDICATED BY THE CABIN ALT INDICATOR, WE COMPLIED WITH PHAS - [SDR FDEA201902130401](https://openairdocs.org/sdr/FDEA201902130401), Feb 13, 2019: COUNTERBALANCE. DEFECTIVE. L1 DOOR IS BINDING WHEN OPENING UNSAFE. R&R COUNTERBALANCE ASSY PER MM 52-11-11-4. ALSO R&R SNUBBER ASSY ROTARY PER MM 52-11-10-4. - [SDR FDEA201901170163](https://openairdocs.org/sdr/FDEA201901170163), Jan 17, 2019: NOT REPORTED. MALFUNCTIONED. PDIS 939 52-10 6607 17JAN19 VIE OPEN U LOGPAGES:3019080 ENTRY DOOR 1L WOULD NOT FULLY OPEN MEL 17JAN19 20:56 VIE U RELEASED FOR SERVICE PER MEL : 52-11-01-A CAT - [SDR FDEA201811263371](https://openairdocs.org/sdr/FDEA201811263371), Nov 26, 2018: HINGE. LACK OF LUBE. DURING TRANSIT CHECK UNABLE TO OPEN L1 ENTRY DOOR MORE THAN 45 DEGREES. PERFORMED A VISUAL INSPECTION OF R1 DOOR IAW AMM 52-11-00-6. LUBRICATED HINGE POINTS AND - [SDR FDEA201809192592](https://openairdocs.org/sdr/FDEA201809192592), Sep 19, 2018: INTERCOSTAL. CORRODED. INTERCOSTAL AT BS 1037-1060 AT BL 65 LT SIDE IS CORRODED. REPLACED INTERCOSTAL AT BS 1037-1060 AT BL 65 LT SIDE IAW SRM 51-40-02 REV 125. - [SDR FDEA201809192591](https://openairdocs.org/sdr/FDEA201809192591), Sep 19, 2018: BRACKET. CRACKED. 198AR FWD BRACKET HAS SUSPECT CORROSION EVA OF BRACKET WAS FOUND TO BE CRACKED AND OUT OF LIMITS PER SRM 51-40-02. FABRICATED NEW BRACKET PN:149N7553-26 IAW GMM All 141: https://openairdocs.org/aircraft/N939FD/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.