# N930FD: Boeing 757-2YO

- Status: Valid registration
- Airframe: [Boeing 757-2YO](https://openairdocs.org/model/boeing-757-2yo) (registry code 1384922, 178 seats)
- Serial number: 25240
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: September 9, 2009
- Expires: May 31, 2028
- Mode S code: ACE62A
- 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=930FD
- Page: https://openairdocs.org/aircraft/N930FD

From the FAA registry file of October 21, 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 757-2YO)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N930FD.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20161206023399I](https://openairdocs.org/incident/20161206023399I), Dec 6, 2016: Boeing 757-2YO (N930FD), Chattanooga, TN, Minor damage. Delta MD 80 aircraft was preparing to depart cha rwy 02 and the jet blast blew a door off a cargo container and into a parked fedex B-757. There is damage to…
- [Incident 20120412004479I](https://openairdocs.org/incident/20120412004479I), Apr 12, 2012: Boeing 757-2YO (N930FD), Brentwood, TN, No damage. At approximately 4:00 pm on Thursday April 12, 2012, [privacy data omitted] contacted the nashville FSDO to report that what appeared to be an aircraft part…

## Service difficulty reports (176, newest 50)

As reported by operators and repair stations.

- [SDR FDEA202608121114](https://openairdocs.org/sdr/FDEA202608121114), Aug 12, 2026: LAMP. INOPERATIVE. L1 EXTERIOR SLIDE LIGHT INOP. AMM: 33-51-06-2-1 RELAMPED L1 SLIDE LIGHT I/A/W AMM REFERENCED ABOVE, GOOD FOR SERVICE.
- [SDR FDEA202606270817](https://openairdocs.org/sdr/FDEA202606270817), Jun 27, 2026: BATTERY PACK. FAILED. R1 EMERGENCY LIGHT DOESN'T STAY ON FOR THE COMPLETE LIGHT TEST. L1 LIGHT NORMAL. AMM 33-51-07-2 REMOVED POWER SUPPLY BATTERY PACK, HAS POWER AT POWER SUPPLY, RE
- [SDR FDEA202605200624](https://openairdocs.org/sdr/FDEA202605200624), May 20, 2026: BATTERY PACK. INOPERATIVE. DURING MX PRE-FLIGHT FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT, R1 DOOR EXIT SIGN, AND CENTER OVERHEAD SIGN INOP. AMM: 33-51-07-2-2 ALLOWED EMERGENCY LIGHT BATTERY
- [SDR FDEA202603240369](https://openairdocs.org/sdr/FDEA202603240369), Mar 24, 2026: BATTERY PACK. FAILED. DURING MX PRE-FLIGHT, FOUND THE R1 OVERHEAD EMERGENCY LIGHT, EMERGENCY LOCATOR SIGN, AND R1 OUTDOOR EMERGENCY LIGHT WAS OUT. FOUND EMERGENCY LIGHT BATTERY PACK,
- [SDR FDEA202603150352](https://openairdocs.org/sdr/FDEA202603150352), Mar 15, 2026: BATTERY. NO TEST. DURING SERVICE CHECK FOUND R1 DOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED BATTERY AT M730.
- [SDR FDEA202602270287](https://openairdocs.org/sdr/FDEA202602270287), Feb 27, 2026: GIRT BAR. DAMAGED. WHEN OPENING THE MAIN CABIN DOOR, A METAL PIECE ON THE BOTTOM OF THE DOOR FELL OFF. LOOKS LIKE A PIECE OF THE GIRT BAR. REINSTALLED GIR BAR END, NO RII AT BHM P
- [SDR FDEA202602140201](https://openairdocs.org/sdr/FDEA202602140201), Feb 14, 2026: CREASE BEAM. CORRODED. MCC STA 880 SIDE LH CREASE BEAM WITH CORROSION CUT AND REMOVED DAMAGE AREA M.C.C STA 852 TO STA 900 CREASE BEAM IAW B757 SRM 53-00- 13-2R REP 1 FABRICATED TRIMM
- [SDR FDEA202602140200](https://openairdocs.org/sdr/FDEA202602140200), Feb 14, 2026: FLOORBEAM. CORRODED. MAIN DECK FLOOR BEAM STA 1200 BTW BL 0 RBL 58 CORRODED REMOVED DAMAGE T CAP SECTION INSTALLED T CAP SECTION AND REPAIR SPLICE PARTS MAIN DECK FLOOR BEAM STA 120
- [SDR FDEA202602140199](https://openairdocs.org/sdr/FDEA202602140199), Feb 14, 2026: SKIN PANEL. CORRODED. NR 2 ENGINE ACCESS PANEL # 443GL FRAME SKIN CUT OUT CORRODED (EXFOLIATED) REMOVED AND REPLACED # 2 ENGINE FWD NACELLE STRUT NEW SKIN PANEL IAW DWG 311N5002 REV 
- [SDR FDEA202602120191](https://openairdocs.org/sdr/FDEA202602120191), Feb 12, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK BETWEEN BS 1620 - 1420, LBL 58.22 MULTIPLE SPOTS OF CORROSION. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G, TRIMMED, LOCATED, & DRILLED A N
- [SDR FDEA202602100162](https://openairdocs.org/sdr/FDEA202602100162), Feb 10, 2026: CREASE BEAM. CORRODED. MAIN CARGO COMPARTMENT BS 660 R/H CREASE BEAM INB CHORD WITH CORROSION
- [SDR FDEA202602100161](https://openairdocs.org/sdr/FDEA202602100161), Feb 10, 2026: CREASE BEAM. CORRODED. MAIN CABIN CREASE BEAM RBL 64.50 FROM STA 1490 TO STA 1640 MULTIPLES SPOTS WITH CORROSION CUT OUT DAMAGE SECTION (TRIMMED) MAIN CABIN CREASE BEAM RBL 64.5 FROM 
- [SDR FDEA202602100159](https://openairdocs.org/sdr/FDEA202602100159), Feb 10, 2026: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK FLANGE WITH CORROSION BETWEEN B.S 1280-1300 RBL 24.75 REMOVED SEAT TRACK SECTION MAIN CABIN BETWEEN STA 1200 TO 1320 LBL 24.75 IAW B757 SR
- [SDR FDEA202602030118](https://openairdocs.org/sdr/FDEA202602030118), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 1540 AND 1640 RBL 45.50 SEAT TRACK WITH CORROSION (TWO LOCATIONS). REMOVED SEAT TRACK SECTION MAIN CARGO COMP BETWEEN STA 1540
- [SDR FDEA202602030117](https://openairdocs.org/sdr/FDEA202602030117), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BS 1320 RBL 45.50 SEAT TRACK WITH CORROSION.
- [SDR FDEA202602030116](https://openairdocs.org/sdr/FDEA202602030116), Feb 3, 2026: SEAT TRACK. CORRODED. MAIN CARGO SEAT TRACK BS 1320 TO 1540 LBL 45.50 WITH MULTIPLE CORROSION. REMOVED SEAT TRACK SECTION MAIN CABIN STA 1320 TO 1540 LBL 45.50 TRIMMED, LOCATED AND D
- [SDR FDEA202601300108](https://openairdocs.org/sdr/FDEA202601300108), Jan 30, 2026: SEAT TRACK. CORRODED. MCC STA 1280 LBL 58.22 SEAT TRACK WITH CORROSION. REMOVED AND REPLACED THE SEAT TRACK SRA 1180-1420 LBL 58.22 IAW SRM 51-40-02-0G, & DWG 657N3332, REV A.
- [SDR FDEA202601300107](https://openairdocs.org/sdr/FDEA202601300107), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BS 1620 RBL 58.22 SEAT TRACK WITH CORROSION. REMOVED SEAT TRACK SECTION MAIN CARGO STA 1180-1420 RBL 58.22 IAW B757 SRM 51-40-02-0G TRIMM
- [SDR FDEA202601300104](https://openairdocs.org/sdr/FDEA202601300104), Jan 30, 2026: SKIN. DELAMINATED. LEFT WING MAIN INBOARD FLAP LOWER SURFACE HAS SKIN CRACKED. UPON FURTHER EVALUATION ON L/WING MAIN FLAP INBD LOWER SURFACE FOUND DELAMINATION DIM L = 10.5" W=1.
- [SDR FDEA202601300103](https://openairdocs.org/sdr/FDEA202601300103), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK LBL 58.00 FROM 1180 TO STA 900 MULTIPLES SPOTS CORRODED
- [SDR FDEA202601300102](https://openairdocs.org/sdr/FDEA202601300102), Jan 30, 2026: SEAT TRACK. CORRODED. MCC STA 880 TO 840 LBL 58.22 SEAT TRACK FOUND CORRODED. REMOVED SEAT TRACK SECTION STA 660 TO STA 885 RBL 58.22 M.C.C IAW SRM 51-40-02-0G. TRIMMED, LOCATED AND 
- [SDR FDEA202601300101](https://openairdocs.org/sdr/FDEA202601300101), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 740 AND 860 RBL 58.22 SEAT TRACK WITH CORROSION (03 LOCATION). REMOVED SEAT TRACK SECTION MAIN CABIN BETWEEN STA 660 TO 885 RB
- [SDR FDEA202601300100](https://openairdocs.org/sdr/FDEA202601300100), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 58.00 BTW BS 900 - 1180, MULTIPLES SPOTS WITH CORROSION. REMOVED SEAT TRACK SECTION BETWEEN STA 900 TO 1180 RBL 58.0 M.C.C IAW B757 SRM
- [SDR FDEA202601300099](https://openairdocs.org/sdr/FDEA202601300099), Jan 30, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK STA 1205, RBL 58 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G.
- [SDR FDEA202601280094](https://openairdocs.org/sdr/FDEA202601280094), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK LBL 58.00 FROM BS 1180 TO 900 MULTIPLES SPOTS CORRODED. REMOVED SEAT TRACK SECTION MAIN DECK STA 900 TO 1180 LBL 58.00 IAW B757 SRM 51-40-0
- [SDR FDEA202601280093](https://openairdocs.org/sdr/FDEA202601280093), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT BETWEEN BS 1280 AND 1320 RBL 45.50 SEAT TRACK WITH CORROSION. REMOVED AND REPLACED SEAT TRACK MAIN CARGO COMPARTMENT BETWEEN BS 1280-1320
- [SDR FDEA202601280092](https://openairdocs.org/sdr/FDEA202601280092), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 45 BTW BS 1180 TO 1200 CORRODED. REMOVED SEAT TRACK MAIN DECK RBL 45 BETWEEN STA 1180 TO 1280 IAW B757 SRM 51-40-02-0G TRIMMED, LOCATED
- [SDR FDEA202601280091](https://openairdocs.org/sdr/FDEA202601280091), Jan 28, 2026: SEAT TRACK. CORRODED. MAIN DECK SEAT TRACK RBL 58.00 BTW STA 900 TO STA 1180 MULTIPLES SPOTS WITH CORROSION.
- [SDR FDEA202601090016](https://openairdocs.org/sdr/FDEA202601090016), Jan 9, 2026: HOUSING. DAMAGED. COURIER AREA CENTER EMERGENCY LIGHT WITH R1 DOOR OVERHEAD EMERGENCY LIGHT AND EXTERIOR SLIDE LIGHT INOP. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-07-2, R
- [SDR FDEA202501160075](https://openairdocs.org/sdr/FDEA202501160075), Jan 16, 2025: POWER SUPPLY. FAILED. R1 SLIDE EXTERIOR EMERGENCY EXIT LIGHT INOP. SHGN 15JAN25 14:01 BNA AMM: 33-51-06-2-1 WDM: 33-51-12 PG 11 SH 1FX1 IPC: 33-51-07-100 RELAMPED R1 SLIDE LIGHT ASSY
- [SDR FDEA202406090785](https://openairdocs.org/sdr/FDEA202406090785), Jun 9, 2024: GUST LOCK. DAMAGED. GUSTLOCK BROKEN ON L1 DOOR REPLACED THE NO 1 (LH) PASSENGER DOOR HOLD OPEN LOCK COLLAR PER ABOVE AMM. OK FOR SERVICE.
- [SDR FDEA202402190187](https://openairdocs.org/sdr/FDEA202402190187), Feb 19, 2024: FITTING. DAMAGED. DURING INSP OF R/H WING OUTER-UPPER SKIN FITTINGS AND DIAGONAL BRACE FASTENNERS AND SHIM PER E 5730-E0340076 L P12 STEP:3 HOLE 14 FASTENNER FOUND SECOND OVER SI
- [SDR FDEA202310241794](https://openairdocs.org/sdr/FDEA202310241794), Oct 24, 2023: ACTUATOR. FAILED. AFTER TAKEOFF & GEAR RETRACT APPEARED TO COMPLETE, A SHORT BUMP NOISE & FEEL UNDER COCKPIT, BUT ALL INDS APPEARED NORMAL. ON MLG EXTENSION, A SIGNIFICANT BANG &
- [SDR FDEA202307251288](https://openairdocs.org/sdr/FDEA202307251288), Jul 25, 2023: CONTROLLER. FAILED. ABOUT 2 MINUTES AFTER LEVEL OFF AT FL330, CABIN ALTITUDE MASTER WARNING MESSAGE APPEARED. ABOUT 1 MINUTE LATER, CABIN AUTO INOP MASTER CAUTION MESSAGE APPEARED.
- [SDR FDEA202203310795](https://openairdocs.org/sdr/FDEA202203310795), Mar 31, 2022: DOOR FRAME. CORRODED. FUSELAGE CUT-OUT FOR ACCESS DOOR 313AL AFT FRAME CORRODED. EVALUATED CORROSION AT FUSELAGE CUT-OUT FOR ACCESS DOOR 313AL AFT FRAME AND FOUND TO BE CORRODED 100%
- [SDR FDEA202203290744](https://openairdocs.org/sdr/FDEA202203290744), Mar 29, 2022: FLOOR PANEL. DAMAGED. ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VTMAE TRAVELER #T22/1604260 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202203220646](https://openairdocs.org/sdr/FDEA202203220646), Mar 22, 2022: SKIN. DENTED. L/H LOWER LOBE FUSE SKIN AT STA. 247 AT STR23L HAS A CREASE BULGE ON FWD SIDE OF FRAME, NEEDS EVAL. EVALUATED DENT AT STA 247 S-23L, DAMAGE LOCATION IS LESS THA
- [SDR FDEA202203130495](https://openairdocs.org/sdr/FDEA202203130495), Mar 13, 2022: SKIN. CORRODED. FUSELAGE SKIN BETWEEN ACCESS DOOR 313AL CUT-OUT AND APU COMPARTMENT, INNER SURFACE IS CORRODED. REMOVED CORROSION FROM FUSELAGE SKIN BETWEEN ACCESS DOOR 313AL C
- [SDR FDEA202011172886](https://openairdocs.org/sdr/FDEA202011172886), Nov 17, 2020: PUMP. FAILED. EMERGENCY DECLARED. LT HYD QTY AMBER CAS FOLLOWED LT ENGINE PUMP AMBER CAS, FOLLOWED BY LT HYD RESERVOIR AND LOSS OF FLUID .01 RF SHOWING. ALTN FLAP AND ALTN GE
- [SDR FDEA2020040630685](https://openairdocs.org/sdr/FDEA2020040630685), Apr 3, 2020: INTERCOSTAL. CRACKED. AFT CARGO COMPT. AFT BULKHEAD INTERCOSTAL BETWEEN FLOOR BEAMS BS. 1681.8 AND BS. 1701, IS CRACKED AT FWD SIDE ON RADIOUS AT BS. 1681.8 BL-0. REMOVED INTERCOASTA
- [SDR FDEA2020040320659](https://openairdocs.org/sdr/FDEA2020040320659), Apr 2, 2020: STRAP. MISSING. AFT CARGO COMPT. AFT BULKHEAD FLOOR BEAM BETWEEN BS 1681.8 AND BS 1701,FLOOR BEAM IS MISSING STABILIZER STRAP ON INTERCOSTAL WEB LOWER FLANGE AT BL-0. FABRICATE
- [SDR FDEA2020021420331](https://openairdocs.org/sdr/FDEA2020021420331), Feb 12, 2020: LINE. LEAKING. AFTER TAKEOFF, RAISED GEAR HANDLE TO UP. RECEIVED A GEAR DOORS EICAS AND DOORS LIGHT. COMPLED WITH QRH. NO OTHER ASSOCIATED PROBLEMS. PERFORMED B757 FIM 32-09 F
- [SDR FDEA201907251689](https://openairdocs.org/sdr/FDEA201907251689), Jul 25, 2019: CARGO. FUMES. DURING CLIMBOUT HAD STRONG UNKNOWN FUMES IN COCKPIT FOR 2-3 MINUTES. THAN SEEMED TO BE DISSAPPATING, BUT AT LEVEL OFF AT FL 380 STARTED COMING BACK. DECLARED AN
- [SDR FDEA201905121036](https://openairdocs.org/sdr/FDEA201905121036), May 12, 2019: CONTROL VALVE. MALFUNCTIONED. DURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. NOTICED OUTFLOW VALVE IN FULL CLOSED POSITION WITH RIGHT 
- [SDR FDEA201905101022](https://openairdocs.org/sdr/FDEA201905101022), May 10, 2019: SHUTOFF VALVE. FAILED. PDIS 930 21-30 7416 10MAY19 MEM OPEN U LOGPAGES:3112369 DURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. N
- [SDR FDEA201901110094](https://openairdocs.org/sdr/FDEA201901110094), Jan 11, 2019: INSERT. UNSECURE. FOUND L1 DOOR SLIDE COVER FWD UPPER LATCH, UNLATCHED. REPAIRED POTTED INSETS REF. AMM 25-00-00-8. REINSTALLED L-1 DOOR SLIDE COVER, DOOR OPS CHECKS NORMAL REF A
- [SDR FDEA201810092843](https://openairdocs.org/sdr/FDEA201810092843), Oct 9, 2018: BOTTLE. INOPERATIVE. ON POST FLIGHT FOUND R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE DEPLETED. REPLACED R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE PER AMM 52-11-30-4. A/C OK FOR SERVICE
- [SDR FDEA201805161248](https://openairdocs.org/sdr/FDEA201805161248), May 16, 2018: SWITCH. FAILED. ON SELECTING FLAPS 15 FROM 5, LE SLAT ASYMETERY CAUTION MESSAGE WAS RECEIVED. LE SLAT DISAGREE DISPLAYED AT THE COMPLETION OF THE QRH THE FLAPS WERE SELECTED IN
- [SDR FDEA201804120970](https://openairdocs.org/sdr/FDEA201804120970), Apr 12, 2018: HYDRAULIC SYSTEM. OVERSERVICED. DURING A MAIN DECK CARGO FIRE PROTECTION CHECK, SMOKE CAME OUT BOTH FLIGHT DECK VENT DIFFUSERS. RAN QRH AND SMOKE CLEARED. OPERATED PACKS WITH ENGINES AS PNUEMA
- [SDR FDEA201804040851](https://openairdocs.org/sdr/FDEA201804040851), Apr 4, 2018: SKIN. DELAMINATED. DURING SANDING, FOUND LEFT WING T/E OTBD AFT FLAP UPPER SURFACE TABS DELAMINATED, WS 481 AFT OF THE NR 3 SPOILER. ACCOMPLISHED PERMENANT REPAIR IAW SRM 57-53-01

All 176: https://openairdocs.org/aircraft/N930FD/reports.md

## Related

- Other Boeing 757-2YO aircraft: https://openairdocs.org/model/boeing-757-2yo/aircraft.md
- STCs for the Boeing 757-2YO: https://openairdocs.org/model/boeing-757-2yo/stcs.md

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