# N903FD: 1993 Boeing 757-2B7 - Status: Valid registration - Airframe: [Boeing 757-2B7](https://openairdocs.org/model/boeing-757-2b7) (registry code 1384964, 178 seats) - Serial number: 27124 - Year built: 1993 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: April 12, 2007 - Expires: April 30, 2030 - Mode S code: AC7AD2 - 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=903FD - Page: https://openairdocs.org/aircraft/N903FD 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 757-2B7) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N903FD. ## FAA accident and incident reports None matched to N903FD. ## Service difficulty reports (162, 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 FDEA202605300654](https://openairdocs.org/sdr/FDEA202605300654), May 30, 2026: STOWAGE BOX. DAMAGED. WHILE PRE FLIGHTING AC FOUND CAPTS O2 MASK BOX TEST BUTTON BROKEN. REMOVED AND REPLACED CAPTS 02 MASK STOWAGE BOX PER 757 AMM 35-11-51-4-99. OPS CHECK GOOD. MVP - [SDR FDEA202604250500](https://openairdocs.org/sdr/FDEA202604250500), Apr 25, 2026: CIRCUIT BREAKER. TRIPPED. LEFT AND RIGHT FUEL OVERRIDE CIRCUIT BREAKERS ARE TRIPPED ON PREFLIGHT. REINSTALLED THE P33 PANEL. AWAITING RETEST REQUIREMENTS FROM ENGINEERING IAW AMM: 20-11- - [SDR FDEA202602100158](https://openairdocs.org/sdr/FDEA202602100158), Feb 10, 2026: SKIN. CRACKED. ENG # 1 NACELLE STRUT UPPER WING SURFACE SPAR MID-SPAR ATTACH FITTING HAS A BOLT MIGRATED THIS ITEM HAS BEEN ACCOMPLISHED FOLLOWING WORK INSTRUCTIONS AS PER EA - [SDR FDEA202602070144](https://openairdocs.org/sdr/FDEA202602070144), Feb 7, 2026: WEDGE. DAMAGED. NUMBER 9 LEADING EDGE SLAT WEDGE DEBONDED, TWO PLACES. APPLIED A PERMANENT REPAIR TO NR 9 LE SLAT EDGE WEDGE IAW SRM 51-70-10-2R R ESTORED SURFACE IN REPAIRED A - [SDR FDEA202602070143](https://openairdocs.org/sdr/FDEA202602070143), Feb 7, 2026: WEDGE. DAMAGED. NUMBER 7 LEADING EDGE SLAT WEDGE DEBONDED. REPAIRED NR 7 LEADING EDGE SLAT IAW SRM 51-70-10-2R.TAP TEST RESULTED SATIFACTORY IAW SRM 51-10-06-2R. - [SDR FDEA202602040127](https://openairdocs.org/sdr/FDEA202602040127), Feb 4, 2026: STRINGER. DAMAGED. REMOVE EXISTING REPAIR AT STA 1656 ON STRINGER 26L REPAIRED STRINGER SECTION AT BS 1640 11" TO BS1660 10" STR 26L, IAW B757 SRM 53-00-03-2R, FIG 201, DETAIL I A - [SDR FDEA202601300106](https://openairdocs.org/sdr/FDEA202601300106), Jan 30, 2026: FLOOR SUPPORT. MECHANIC ERROR. AFT CARGO FLOOR SUPPORT, BS 1465 MISDRILLED HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT, IAW SRM 51-40-02-0G AND SRM 53-60-53-01, FIG 1, DET VII. - [SDR FDEA202601300105](https://openairdocs.org/sdr/FDEA202601300105), Jan 30, 2026: FLOOR SUPPORT. MECHANIC ERROR. AFT CARGO FLOOR SUPPORT, LBL 7.55 BTW BS 1480 TO 1500 MISDRILLED HOLES REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G AND SRM 53-60-53-0I FIG 1 DET - [SDR FDEA202601280095](https://openairdocs.org/sdr/FDEA202601280095), Jan 28, 2026: SKIN. DENTED. UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 TWO DENTS, APPLIED PERMANENT REPAIR AT UPPER FUSELAGE BETWEEN BS 1941 AND 1963.8 IAW SRM 53-80-01-1A, FIG 101, SHEET 2 - [SDR FDEA202601190068](https://openairdocs.org/sdr/FDEA202601190068), Jan 19, 2026: SKIN. CORRODED. NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 134.76 CORRODED. THIS ITEM HAS BEEN ACCOMPLISHED ON EA # F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- - [SDR FDEA202601190067](https://openairdocs.org/sdr/FDEA202601190067), Jan 19, 2026: SKIN. CORRODED. NR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 200.50 SUSPECTED CORROSION. ACCOMPLISHED ON EA F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATE - [SDR FDEA202512162256](https://openairdocs.org/sdr/FDEA202512162256), Dec 16, 2025: BATTERY PACK. NO TEST. L1 EMERGENCY EXIT LIGHT FAILS TO TEST DURING PRE-FLT. REMOVED AND REPLACED THE BATTERY PACK FOR THE L 1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-07-2 EMERGENCY E - [SDR FDEA202508261543](https://openairdocs.org/sdr/FDEA202508261543), Aug 26, 2025: BATTERY. INOPERATIVE. DURING MX PRE-FLIGHT FOUND OVERHEAD EMERGENCY LIGHTS AT CENTER, AND R1 DOOR AND R1 EXTERIOR LIGHT INOP. ATTEMPTED TO CHARGE BATTERY FOR OVER AN HOUR, NO FIX. RE - [SDR FDEA202501090040](https://openairdocs.org/sdr/FDEA202501090040), Jan 9, 2025: TRANSMISSION. FAILED. TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1 ON APPROACH. FOLLOWED QRH. LANDING UNEVENTFUL. FOLLOWING FIM FOUND ON THE INBOARD UNIT OF THE I - [SDR FDEA202501080037](https://openairdocs.org/sdr/FDEA202501080037), Jan 8, 2025: INDICATION SYS. MALFUNCTIONED. TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1 ON APPROACH. FOLLOWED QRH. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF TRAILING EDGE FLAP - [SDR FDEA202407151020](https://openairdocs.org/sdr/FDEA202407151020), Jul 15, 2024: INDICATOR. INOPERATIVE. OVERHEAD FUEL COUNTER (LEFT TANK) AND TOTALIZER WENT BLANK DURING THE FLIGHT. IT CAME BACK ON AFTER 15 MINUTES WHILE IN FINAL APPROACH. PERFORMED FIM 28-41 FAUL - [SDR FDEA202407120987](https://openairdocs.org/sdr/FDEA202407120987), Jul 12, 2024: CONNECTOR. DIRTY. NOTICED RIGHT ENGINE AMBER REV MESSAGE IN FLIGHT. COMPLIED WITH QRH REVERSER UNLOCKED CHECKLIST. REVERSERS OPERATED NORMALLY ON LANDING. AFTER STOWING AMBER REV - [SDR FDEA202305270965](https://openairdocs.org/sdr/FDEA202305270965), May 27, 2023: UNKNOWN. UNKNOWN. DURING SVC CHECK FOUND AED DEFIBRILATOR WITH RED "X" INSIDE WINDOW. FACT 27MAY23 00:48 CDG U AMM: 25-60-99-2 DURING TS, FOUND AED BATTERY MISSPLACE. REINSTALLED - [SDR FDEA202305100870](https://openairdocs.org/sdr/FDEA202305100870), May 10, 2023: EXTINGUISHER. INOPERATIVE. DURING OFFLOADING , DG CONTAINERS HAS BEEN PULLED OUT WITH FIRE EXTINGUISHER HOSES CONNECTED , RESULTING TO BROKE FIRE EXTINGUISHER RIGID LINE. BOTH MAIN DECK D - [SDR FDEA202204010985](https://openairdocs.org/sdr/FDEA202204010985), Apr 1, 2022: NONE. CORRODED. LOWER FUSELAGE - FRAME ATTACHED OUTER CHORD CORRODED, AT STA1380, BETWEEN STGR27RH AND STGR29RH COMPLIED WITH FEDEX EA: F-5310-T0367786 PT1, EA TITLE: FUSELAGE - [SDR FDEA202203290979](https://openairdocs.org/sdr/FDEA202203290979), Mar 29, 2022: SEAT TRACK. CORRODED. MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - SEAT TRACK CORRODED, BETWEEN STA1600 AND STA1620, LBL60 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - SEA - [SDR FDEA202203280984](https://openairdocs.org/sdr/FDEA202203280984), Mar 28, 2022: DRAG FITTING. CRACKED. RH WING - OUTER WING - UPPER SKIN, DRAG FITTINGS AND DIAGONAL BRACE FASTENER AND SHIM INSPECTIONS, OPEN-HOLE HFEC INSPECTION FOUND HOLE #17 WITH CRACK SIGNAL CO - [SDR FDEA202203280977](https://openairdocs.org/sdr/FDEA202203280977), Mar 28, 2022: DRAG FITTING. CRACKED. RH WING - OUTER WING - UPPER SKIN, DRAG FITTINGS AND DIAGONAL BRACE FASTENER AND SHIM INSPECTIONS, OPEN-HOLE HFEC INSPECTION FOUND HOLE #2 WITH CRACK SIGNAL COM - [SDR FDEA202201180102](https://openairdocs.org/sdr/FDEA202201180102), Jan 18, 2022: SWITCH. FAILED. PDIS 903 31-50 4225 18JAN22 CGN FACT U RTO AT 65KTS FOR MASTER WARNING WITH SPEED BRAKES ON EICAS R/R'D SPEEDBRAKE HANDLE POSITION SWITCH S493 IAW AMM 31-51-03- - [SDR FDEA202201120101](https://openairdocs.org/sdr/FDEA202201120101), Jan 12, 2022: NONE. FAILED. PDIS 903 31-50 4215 12JAN22 MUC FACT U ON INITIAL T/O, UPON TAKEOFF THRUST ADVANCE, MASTER WARNING ILLUMINATED. NO OTHER INDICATIONS. MASTER WARNING WILL NOT RE - [SDR FDEA202112173101](https://openairdocs.org/sdr/FDEA202112173101), Dec 17, 2021: FLAP SYSTEM. FAULTED. TE FLAP DISAGREE MESSAGE WHEN SELECTING FLAPS 25 ON APPROACH. EXECUTED MISSED APPROACH AND COMPLIED WITH QRH. LANDED WITH FLAPS 20 DEGREES. BITE TEST ALL 3 PSEU - [SDR FDEA202112032983](https://openairdocs.org/sdr/FDEA202112032983), Dec 3, 2021: NONE. NONE. PDIS 903 25-60 4081 03DEC21 BSL FACT U AFTER LANDING DISCOVERED THAT THE RIGHT EXIT DOOR SLIDE LIGHT WAS INOP. FOUND INDICATOR LIGHT BULBS BURNED, REPLACED ACC - [SDR FDEA202109152312](https://openairdocs.org/sdr/FDEA202109152312), Sep 15, 2021: LAMP. INOPERATIVE. UNARMED LIGHT OF EMERGENCY POWER SWITCH LAMPS U/S AMM: 33-16-02-2 EMERGENCY UNARMED LIGHT LAMPS REMOVED AND REPLACED. FUNCTION OK. MAINT. ALERT #20-0120 OBSERVE - [SDR FDEA202106151540](https://openairdocs.org/sdr/FDEA202106151540), Jun 15, 2021: PROBE. DIRTY. ON CLIMB OUT L ENGINE EGT WAS AT MAX LIMIT AS WELL AS N2. FUEL FLOW ON LEFT ENGINE WAS DOUBLE RIGHT SIDE. DECLARED EMERGENCY, PERFORMED QRH PROCEDURES AND RETUR - [SDR FDEA202103270788](https://openairdocs.org/sdr/FDEA202103270788), Mar 27, 2021: WIRE. DISCONNECTED. MDIS 903 33-50 3354 27MAR21 MUC OPEN U INTERIOR EMERGENCY LIGHT COURIER AREA (L26) INOP FACT 30MAR21 17:46 CDG FOUND WIRE #2 DISCONNECTED FROM EMEGENCY LIGHPLAT - [SDR FDEA202009212285](https://openairdocs.org/sdr/FDEA202009212285), Sep 21, 2020: HANDLE. GOUGED. FWD CARGO DOOR HANDLE HAS GOUGE ON INNER SURFACE. REPAIRED FWD CARGO DOOR HANDLE GOUGE, IAW FEDEX EA F-5230-T3056468 P1 TITLE: DOORS-CARGO DOOR/HYD SYS-NO 1 CAR - [SDR FDEA202009112234](https://openairdocs.org/sdr/FDEA202009112234), Sep 11, 2020: STRAP. DAMAGED. FLOOR BEAM STABILIZER STRAP AT BSTA 377.7 LBL 24.75 IS DAMAGED. REPAIRED FLOOR BEAM STABILIZER STRAP AT BSTA 377.7 LBL 24.75, IAW SRM 53-00-51-2R REPAIR 12. - [SDR FDEA202009102235](https://openairdocs.org/sdr/FDEA202009102235), Sep 10, 2020: STRAP. DAMAGED. UPON CLOSE UP INSP FOUND STABILIZER STRAP AT BSTA 580 LBL 24 DAMAGE ON LOWER SIDE OF FLOOR BEAMS REPAIRED STABILIZER STRAP AT BSTA 580 LBL 24, IAW SRM 53-00-51- - [SDR FDEA202009092361](https://openairdocs.org/sdr/FDEA202009092361), Sep 9, 2020: PANEL. CRACKED. '9 LEADING EDGE COVE PANEL CRACKED OUTBOARD OF INBOARD MAIN TRACK. FABRICATED NEW COVE PANEL P/N 114N4076-18, IAW BOEING DRAWING 114N4003 AND FEDEX GMM 7-0-1001 - [SDR FDEA202009072283](https://openairdocs.org/sdr/FDEA202009072283), Sep 7, 2020: BRACKET. BROKEN. BRACKET FOUND DAMAGED ON FWD SIDE OF DOOR 3R SECOND FROM TOP FABRICATED BRACKET FROM DOOR 3R SECOND FROM TOP, IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING 411N2035 - [SDR FDEA201811263393](https://openairdocs.org/sdr/FDEA201811263393), Nov 26, 2018: CIRCUIT BREAKER. TRIPPED. AFTER TROUBLE SHOOTING FINISHED THE LDG ALT EXT C/B POPPED OUT AGAIN DURING T/S FOUND "ALT GEAR EXTENSION CONT" C/B FAULT , C/B SWAPPED CB C41177 WITH CB C00773 - [SDR FDEA2018091432511](https://openairdocs.org/sdr/FDEA2018091432511), Sep 13, 2018: SKIN. WORN. RT MAIN FLAP TOP SURFACE HAS 2 WEAR MARKS OPPOSITE NR 10 SPOILER ACTUATOR. REPLACED DAMAGED REPAIR PLATE ON RT MAIN FLAP TOP SURFACE IAW SRM 57-53-01-2R REPAIR - [SDR FDEA2018091432492](https://openairdocs.org/sdr/FDEA2018091432492), Sep 13, 2018: STRAP. CORRODED. INTERCOSTAL STRAP PUNCTURED AND CORRODED AT BS 1020 BETWEEN RBL 25 AND RBL 45. PUNCTURE DAMAGE IS NOT ALLOWED AS PER SRM 53-00-51-1A FIG 101 REV 124. FABRICATED - [SDR FDEA2018091432491](https://openairdocs.org/sdr/FDEA2018091432491), Sep 13, 2018: BRACKET. CRACKED. RT OB FLAP OB TOP TO LWR SKIN AFT BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET IAW GMM 7-00-1001 REV 150 AND DRAWING 113N3370 SHEET 2 REV C AND SRM 51- - [SDR FDEA2018091432490](https://openairdocs.org/sdr/FDEA2018091432490), Sep 13, 2018: FRAME. DAMAGED. FRAME 231.25 AT FWD E&E BAY DOOR HAS STRUCTURAL DAMAGE. PERFORMED REPAIR TO FRAME 231.25 IAW SRM 53-00-07-2R FIG 202 REV 125. - [SDR FDEA2018091432489](https://openairdocs.org/sdr/FDEA2018091432489), Sep 13, 2018: SUPPORT BRACKET. CORRODED. TOP LT WING WTB PANEL SUPPORT NR 4 FROM FWD REQUIRES EVALUATION AND REPROTECTION. FABRICATED WTB PANEL SUPPORT BRACKETS IAW DRAWING 149N7210 SHEET 7 REV B AND G - [SDR FDEA2018091432488](https://openairdocs.org/sdr/FDEA2018091432488), Sep 13, 2018: STRIP. CORRODED. LT ELEVATOR TIP UPPER AND LOWER STATIC DISCHARGE STRIP HAS SUSPECT CORROSION UNDERNEATH. UPON EVALUATION, BOTH STATIC DISCHARGE STRIPS FOUND TO BE OUT OF LIMITS - [SDR FDEA2018091412454](https://openairdocs.org/sdr/FDEA2018091412454), Sep 11, 2018: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LBL 58- RBL 58 BS 1200. FLOORBEAM FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51-1A FIG 101 DETAILIII REV 124 ON SNRMS N00331, N003 - [SDR FDEA201809112443](https://openairdocs.org/sdr/FDEA201809112443), Sep 11, 2018: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK AT BS 900-1180 RBL 58. CORROSION DAMAGE ON SEAT TRACK RBL 58 BSTA 900-1180 OUT OF LIMITS IAW SRM 53-00-52-1A REV 124. SEAT TRACK SECTION - [SDR FDEA201809112453](https://openairdocs.org/sdr/FDEA201809112453), Sep 11, 2018: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LBL 58 BSTA 900-1060. REMOVED AND EVALUATED CORROSION ON SEAT TRACK LBL58 BSTA 900-1070 IAW SRM: 53- 00-52-1A ALLOWABLE DAMAGE 1 FIG 101 - [SDR FDEA201809112452](https://openairdocs.org/sdr/FDEA201809112452), Sep 11, 2018: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK LBL 58 BSTA 1100-1180. REMOVED AND EVALUATED CORROSION ON SEAT TRACK LBL58 BSTA 1100-1180 IAW SRM 53- 00-52-1A ALLOWABLE DAMAGE 1 FIG 10 - [SDR FDEA201809112451](https://openairdocs.org/sdr/FDEA201809112451), Sep 11, 2018: SKIN. CORRODED. BONDING FUNCTIONAL TEST OF LEFT WING TANK OVERFILL PORT FAILED TEST. UPON EVALUATION, CORROSION FOUND ON SURFACE OF THE UPPER SKIN AT THE OVERWING FILL PORT. RE - [SDR FDEA201809112449](https://openairdocs.org/sdr/FDEA201809112449), Sep 11, 2018: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT BS 1020 LBL 0 TO LBL 25. CORROSION ON INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A FIG 101 DETAIL II REV 124. ORIGINAL - [SDR FDEA201809112448](https://openairdocs.org/sdr/FDEA201809112448), Sep 11, 2018: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT BS 1020 RBL 0 - RBL25. CORROSION ON INTERCOSTAL FOUND TO BE OUTSIDE OF LIMITS IAW SRM 53-00-04-1A FIG 101 DETAIL II REV 124. ORIGINA - [SDR FDEA201809112444](https://openairdocs.org/sdr/FDEA201809112444), Sep 11, 2018: STRAP. DAMAGED. INTERCOSTAL STRAP PUNCTURED AND CORRODED AT BS 1020 BETWEEN LBL 25-45. PUNCTURE DAMAGE NOT ALLOWED AS PER SRM 53-00-51-1A FIG 101 REV 124. FABRICATED NEW INTERC All 162: https://openairdocs.org/aircraft/N903FD/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 757-2B7 aircraft: https://openairdocs.org/model/boeing-757-2b7/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.