- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 42723
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 25, 2016
- Certificate issued
- August 22, 2016
- Expires
- August 31, 2029
- Mode S code
- A0996B
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 N138FEMatched 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 N138FEMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202603300382Skin · damagedNR 5 LT TRAILING EDGE WEDGE HAS A CHIP IN COMPOSITE MATERIAL ON AFT SIDE APPROX 17 INCH FROM OTBD EDGE, APPROX 3/8 X 3/8. REPAIRED LT WING L/E NR 5 SLAT TRAILING EDGE WEDGE AT WS 508 IAW SRM 57-43-02- 2R, FIG 201, REPAIR 1, SHEET 1, & SRM 51-70-10-2R. MAJOSDR FDEA202603300381Skin · gougedLEFT WING, GOUGES ON LWR SKIN OF NR 5 SLAT TRAILING EDGE WEDGE AT APPROX. 42 INCHES FROM INBD EDGE REPAIRED LT WING NR 5 SLAT T/E WEDGE TOP SKIN AT WS 446.4 IAW SRM 57-43-02-2R AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR. SEE JPF STEPS FOR OTHER WORK ACCOMPSDR FDEA202405220717Skin · delaminatedLH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WITH TWO DELAMINATIONS LH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WAS REPAIRED IAW B767 SRM 57-53- 01-2R REP 1 TABLE I FIG 201 AND SRM 51-70-17-0G PAR 4.A FIG 10 REV 88 DEC 15/2023SDR FDEA202405220716Wedge · wornLH WING, OUTBOARD SLAT 5, TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75, PREVIOUS REPAIR WITH WEAR LH WING, OUTBOARD SLAT 5 TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75 WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1-2 PAGE 1-2, AND SRM 51-70-10-2RSDR FDEA202405210713Skin · delaminatedRH WING,INBOARD FLAP, MAIN FLAP WITH DELAMINATION AT WBL 289.4 RH WING, INBOARD FLAP, MAIN FLAP AT WBL 289.4 WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 TABLE II AND SRM 51-70-06-0G PAR 5G FIG 3 REV 88 DEC 15/2023SDR FDEA202405210712Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222CFF SECTION 41 AT MDC. MDC, SECTION 41, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405210711Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF SECTION 41 AT MDC. MDC, SECTION 41, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405180688Skin · delaminatedRH WING OUTBOARD FLAP LEADING EDGE WITH TWO DELAMINATIONS BETWEEN WS 720.2 AND WS 616.2 RH WING OUTBOARD FLAP LEADING EDGE BETWEEN WS 720.2 AND WS 616.2 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 TABLE I PAG 1-5 AND SRM 51-70-03-0G PAR 5.A FIG 5 REV 88 DESDR FDEA202105181293Window · crackedPDIS 138 30-40 4256 18MAY21 ICT WINDOW R3 (FIRST OFFICER REAR MOST WINDOW) EXTREMELY HOT TO THE TOUCH IN LOWER LEFT PORTION OF WINDOW. ALSO, IN THE SAME LOWER LEFT AREA OF THE WINDOW, THERE APPEARS TO BE A BURN MARK AND VERY SMALL CRACK. SHORSDR FDEA202010052418Static Inverter · failedSTATIC INVERTER FAILS DURING EICAS BUS TIE TEST. WILL NOT POWER THE CAPT PFD. INSTALLED ALT STATIC INVERTER, PASSES EICAS BUSS TIE TEST IAW AMM 24-33-03-4.SDR FDEA2020052211029Beam · crackedL/H WING L/E NOSE BEAM WEB AT THE FUEL SVC DOOR CRACKED REPAIRED LH WING LE NOSE BEAM PER B767 SRM 57-41-13-2RSDR FDEA201711293320Warning Message · illuminatedPDIS 138 52-70 1261 29NOV17 MEM SHORTLY AFTER LEVEL OFF AT FL370 "MAIN CARGO DOOR" EICAS ALERT ILLUMINATED. COMPLIED WITH ORH PROCEDURES. DESCENDING THROUGH 17,000 ENROUTE TO 10,000 MAIN CARGO DOOR LITE WENT OUT. CHECKED GAP ON MAIN CARGO
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