- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 63131
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 29, 2022
- Certificate issued
- March 31, 2022
- Expires
- March 31, 2029
- Mode S code
- A304D8
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 327
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 5 |
|---|---|
| 1985 | 4 |
| 1986 | 9 |
| 1987 | 6 |
| 1988 | 7 |
| 1989 | 9 |
| 1990 | 20 |
| 1991 | 15 |
| 1992 | 8 |
| 1993 | 9 |
| 1994 | 14 |
| 1995 | 6 |
| 1996 | 10 |
| 1997 | 5 |
| 1998 | 9 |
| 1999 | 9 |
| 2000 | 21 |
| 2001 | 16 |
| 2002 | 11 |
| 2003 | 12 |
| 2004 | 15 |
| 2005 | 11 |
| 2006 | 7 |
| 2007 | 11 |
| 2008 | 8 |
| 2009 | 11 |
| 2010 | 11 |
| 2011 | 8 |
| 2012 | 10 |
| 2013 | 8 |
| 2014 | 13 |
| 2015 | 6 |
| 2016 | 5 |
| 2017 | 4 |
| 2018 | 7 |
| 2019 | 1 |
| 2020 | 7 |
| 2021 | 7 |
| 2022 | 3 |
| 2023 | 6 |
| 2024 | 1 |
| 2025 | 5 |
| 2026 | 6 |
See all 378 ADs
Information bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Boeing 767-300F
SAIB NM-20-07Navigation - Glideslope SystemSAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-18-33Engine Fuel and ControlSAIB NM-17-17Oxygen SystemSAIB NM-17-10Maintenance PracticesSAIB NM-17-09Flight Control SystemSAIB NM-15-03Flight ControlsSAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-09-03Engine Fuel and Control - Implementing Fuel Tank System Airworthiness LimitationsSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.NTSB investigations
No NTSB investigations matched to N294FEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 767-300F aircraft
FAA incident reports
No FAA accident or incident reports matched to N294FEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 767-300F aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202512312299Skin · dentedLEFT WING, INBOARD MAIN FLAP, LOWER SURFACE, 89" FROM OUTBOARD EDGE, 10" DOWN FROM LEADING EDGE, LOWER SKIN IS DENTED AS MARKED. BONDED REPAIR ON L/H WING, I/B MAIN FLAP, LOWER SURFACE, 89" FROM O/B EDGE, 10" DOWN FROM L/E, LOWER SKIN (WS 341). SEE JPF FORSDR FDEA202512302298Skin · delaminatedRH OUTBD FLAP HAD A DENT/IMPACT DAMAGE WITH AREA OF DELAM ON THE LEADING EDGE OF THE FLAP AT APPROX WS STA 741.0 REPAIRED RH WING OUTBD FLAP TRAILING EDGE NOSE SKIN L/E PNL (MPN: 113T3112-402) AT WS STA.741.0 (MARKED AREA) IN REF. TO 767 SRM 57-53-01-2R SDR FDEA202512232286Floor Panel · dentedMAIN DECK FLOOR PANEL 241ZFF REQUIRES REPAIR. REPAIRED MAIN DECK FLOOR PANEL 241ZFF, MPN: 145T5876-111 AT STA 980-114.82, LBL 54.75-LBL 77.50 IN REF 53-00-50-2R. THIS IS A MAJOR REPAIR. SEE JPF FOR ALL WORK PERFORMED. FLOORBOARD WILL BE INSTALLED ON WO#914SDR FDEA202512222278Floor Panel · damagedMAIN DECK - THE TOP OF FLOOR PANEL 221DFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 221DFF, MPN: 141T5856-117, LBL 11- LBL 33, STA 285-412 IN REF. TO BOEING DWG 141T5856-117, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLSDR FDEA202512222281Floor Panel · damagedMAIN DECK - THE TOP OF FLOOR PANEL 222CFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 222CFF, MPN: 141T5856-116, RBL 54.75- RBL 77.50, STA 285-412 IN REF. TO BOEING DWG 141T5856-116. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF TSDR FDEA202512222280Floor Panel · damagedMAIN DECK - THE TOP OF FLOOR PANEL 222BFF IS DAMAGED (DOT#15). FABRICATED NEW FLOOR PANEL 222BFF, MPN: 141T5856-106, RBL 33- RBL 54.75, STA 285-412 IN REF. TO BOEING DWG 141T5856-106, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPSDR FDEA202512222279Floor Panel · damagedMAIN DECK - THE TOP OF FLOOR PANEL 221CFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 221CFF, MPN: 141T5856-105, LBL 11- RBL 11, STA 282-412 IN REF. TO BOEING DWG 141T5856-105, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLASDR FDEA202512212277Floor Panel · dentedMAIN CARGO DECK, FLOOR PANEL 242TFA DAMAGED. REPAIRED FLOOR PANEL 242 TFA, MPN: 145T5876-96, RBL33- RBL54.75, STA 984.95- 1087, IN REF B767 SRM 53-00-50-2R, FIG 201, SHEET 1. SEE JPF FOR WORK PERFORMED. THIS IS A MAJOR REPAIR. FLOOR PANEL 242TFA WILL BE INSDR FDEA202512212276Floor Panel · dentedMAIN CARGO DECK, FLOOR PANEL 242LFA HAS DAMAGE REPAIRED FLOOR PANEL 242 LFA, MPN: 145T5876-110, RBL 54.75- RBL 75.25, STA 933- 984.95 IN REF TO B767 SRM 53-00-50-2R, FIG 201, SHEET 1. SEE JPF FOR WORK ACCOMPLISHED. THIS IS A MAJOR REPAIR. FLOOR PANEL 242 LSDR FDEA202512202274Floor Panel · damagedMAIN DECK - THE TOP OF FLOOR PANEL 222AFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 222AFF, RBL11-RBL33, BS 285-412 IAW DRAWING 141T5856-107, AND SR67-53-009. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO#91439 NR#142.SDR FDEA202512202273Floor Panel · dentedMAIN CARGO DECK, FLOOR PANEL 242UFF DAMAGED. REPAIRED MAIN DECK FLOOR PANEL 242UFF, AT BS 980-114.82, RBL 54.75- RBL 74.25 IAW 53-00-50-2R. THIS IS A MAJOR REPAIR. SEE JPF FOR ALL WORK PERFORMED. FLOORBOARD WILL BE INSTALLED ON WO 91439, SEQ 114.SDR FDEA202405240725Former · crackedWING FIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 499.6 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE AT OSS 499.6. INSTALLED A NEW NOSE FORMER ANGLE. FEDEX DRAWING SR67-57-002 REV. A.SDR FDEA202405240724Former · crackedFIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 441 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE. INSTALLED A NEW FORMER ANGLE, B67-57-002-01. FEDEX DRAWING SR67-57-002 REV. A.SDR FDEA202403150316Skin · crackedRT WING: FIXED WING L/E - LOOKING THROUGH LIGHTENING HOLE APPROX 8-12 INCHES OUTBD OF OUTBD SLAT TRACK FOR SLAT #8 BRACKET/ANGLE IS CRACKED. HFEC VERIFIED. (MARKED AND DOT 33) REMOVED FORMER P/N 114T2511-14, AND ANGLE P/N 114T2511-12 AND REPLACED WITH NEW
STCs that may be installed · 788
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 788 STCs