- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 42711
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 28, 2015
- Certificate issued
- February 18, 2015
- Expires
- February 29, 2028
- Mode S code
- A037DA
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 1991 | 4 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 4 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 3 |
| 2008 | 1 |
| 2009 | 4 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
See all 47 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N113FEMatched 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 767-3S2F aircraft
FAA incident reports
No FAA accident or incident reports matched to N113FEMatched 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 767-3S2F aircraft
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202601010001Latch · crackedEMERGENCY LIFE RAFT STOWAGE COMPARTMENT LATCH CRACKED, HINDERING ACCESS. ABLE TO OPEN COMPARTMENT DOOR AND INSP, REF B767 AMM: 25-62-01-4-6/ IPC: 25-62-55-01 FIG01 SH7. FOUND ITEM 360 LATCH ASSY PLASTIC HOUSING CRACKED. AMM: 25-62-01-4-6 AMM: 25-60-00-00SDR FDEA202508281553Skin · dentedR/H OTBD TRAILING EDGE FLAP HAS A DENT LOCATED ON THE LOWER SURFACE INBOARD OF THE INBOARD HINGE FAIRING (MWT). REPAIRED R/H WING OTBD TRAILING EDGE FLAP LOWER SKIN SURFACE DENT (3.3" X 2.0") AT LOCATION INBD OF THE INBOARD HINGE FAIRING AT WS 601, IN REF.SDR FDEA202405100639Bracket · bentL FWD ENTRY DOOR EICAS MESSAGE WITH DOOR CLOSED AND SECURE. WOULD GO OUT WHEN CLOSING THE DOOR THEN APPEAR AGAIN. CREW ENTRY DOOR INDICATION SYSTEM - INOP. VERIFY THAT CREW ENTRY DOOR IS CLOSED, LATCHED, AND LOCKED BEFORE EACH DEPARTURE. USE HAND SIGNSDR FDEA202301200157Exciter · failedPDIS 113 49-99 8422 20JAN23 CDG FACT U APU START ATTEMPT UNSUCCESSFUL. FL350, -59 DEGREES CELSIUS, AND THREE ATTEMPTS MADE. NEED TO INITIATE ETOPS VERIFICATION FLIGHT FOR APU IN-FLIGHT START PER GMM 15-9-0 (REF ITEM 49-99/8422) REFER TO ITSDR FDEA202301100064Slat · dentedLEFT WING SLAT NO. 3 WITH DENTS. LEFT WING SLAT NO. 3 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 51-70-10-2R REPAIR 4 FIG. 201 SHEET 1 AND SRM 57-43-02-2R FIG. 201, (SHEET 1) REV. 85 DEC15/2022SDR FDEA202301090058Skin · wornRH WING, SLAT # 8, TRAILING EDGE WEDGE, BOTTOM SKIN WITH WEAR. RH WING, SLAT #8, TRAILING EDGE WEDGE BOTTOM SKIN WAS REPAIRED IAW SRM 51-70-10-2R PAG. 163, FIG. 202 REV. 85 DEC15/2022 AND SRM 57-43-02-2R FIG. 201, (SHEET 1) REV. 85 .SDR FDEA202210292695Skin · chafedL/H WING NO. 5 LEADING EDGE SLAT LOWER TRAILING EDGE CHAFFED AT APROX OSS 441 M.W.T. REPAIRED #5 SLAT PER EA H-5750-T0371376SDR FDEA202201180100None · nonePDIS 113 34-61 7217 18JAN22 MAD FACT U BOTH CAPT AND FIRST OFFICER FMSS LOCKED UP ON DEPARTURE PASSING THROUGH 5000, COULD NOT SELECT OR CHANGE PAGES ON EITHER FMS FOR ABOUT 2 MINUTES. INITIALLY USED HEADING SELECT TO COMPLY WITH ATC CLEARANCSDR FDEA201905051002Transmitter · failedTE FLAP DISAGREE/AT FLAPS 20. RAN QRH TE FLAP DISAGREE WHICH TOOK US TO FLAP ASYMMETRY. LANDED FLAPS 20. NO ROLL NOTICED IN FLIGHT. REMOVED AND REPLACED NR 1 AND NR 4 FLAP TRANSMITTERS IAW AMM 27-51-45-2. REMOVED AND REPLACED LEFT FLAP/STAB POSITION MODULE ASSDR FDEA2019020740263Skin · damagedBETWEEN STRINGER 38R AND 39R AT STATION 603 PREVIOUS DAMAGE WAS BLENDED OUT. REMOVED PAINT FROM SUSPECT AREA . THIS AREA REQUIRES NDT TO MEASURE FOR MATERIAL REMAINING THICKNESS PER. E.A. H-5330-T0345021. C/W SKIN THICKNESS CHECK OF BLENDED AREA IAW B76SDR FDEA201709222673Hook And Loop · detachedDURING POST FLIGHT, FOUND BOTH PILOT AND COPILOT EVAS ATTACH POINT HOOK AND LOOP STRIPS DETACHED FROM GLARESHIELD. INSTALLED NEW GLARESHIELD HOOK AND LOOP IAW AMM 25-99-99-6, AND DWG 6305. AIRCRAFT OK FOR SERVICE.SDR FDEA201702240655Control Panel · failedON TAXI OUT THE TRANSPONDER RESET ITSELF TO 0000. PUT ASSIGNED CODE BACK IN. DURING CLIMBOUT ATC REPORTED A 600' DISCREPENCE BETWEEN OUR ALTITUDE AND THER RADAR, SWITCHED TRANSPONDERS AND THAT DID NOT HELP. SHUT OFF THEN ON, THEN IT WORKED. REMOVER AND SDR FDEA201606162030Escape Rope · unsecureREADY FOR PUSH BACK TUG, CREW OBSERVED CREW DOOR HAD OBJECT STICKING OUT OF DOOR 1. INSTALLED ESCAPE ROPE IAW AMM 25-61-04-2-1.SDR FDEA201605121537Skin · dentedNUMBER 4 SLAT TOP TE HAS DENT 3" X 5". EVALUATED, REPAIRED, TAP TESTED, SEALED, PRIMED, TOP COATED. REMOVED & RE-INSTALLED & PERFORMED SATISFACTORY SENSOR SWITCH TEST & SATISFACTORY TAI DUCT CLAMP LEAK TEST OF NR 4 LE SLAT IAW SRM 57-43-02-1A FIG 101 NOTE J SDR FDEA201506201928Lanyard · out of positionMAIN ENTRY DOOR L1, DOOR JAM LANYARD MISSING ON PREFLIGHT. FOUND LANYARD STOWED IN CEILING. ROUTED PROPERLY THROUGH DOOR CHANNEL IAW MM 25-10-00-2.
STCs that may be installed · 5
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF6-80C2B6F
STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.STC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES
Earlier aircraft with this N-number · 1
This aircraft carried N113FE before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.