- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 24965
- Year built
- 1992
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 19, 2011
- Certificate issued
- November 19, 2009
- Expires
- November 30, 2028
- Mode S code
- ADDE49
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 2 |
| 2012 | 1 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2019 | 1 |
| 2021 | 1 |
| 2024 | 1 |
| 2026 | 1 |
Engine · Pratt & Whitney PW2037
AD 2026-07-06Turbine SectionAD 2024-12-04Turbine SectionAD 2021-14-13Turbine SectionInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N993FDMatched 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 757-2Q8 aircraft
FAA incident reports
No FAA accident or incident reports matched to N993FDMatched 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 757-2Q8 aircraft
Service difficulty reports · 134
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202608281248Strut · crackedNR 2 NACELLE STRUT, RIGHT SIDE SKIN, THROUGH ACCESS 443AR, SHOWS A CRACK WITH NO VISIBLE STOP HOLE. THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5430-T0388382 P1.SDR FDEA202608281247Skin · debondedLEFT WING INBD T/E MAIN FLAP, AFT PANEL, REAR EDGE HAD DEBONDING. APPLIED PERMANENT REPAIR ON THE LT WING FLAP AFT PANEL IAW SRM 57-53-01-2R, REP 1, DETAIL I, FIG 201, SHEET 2, IAW IAW SRM 51-70-10-2R, REP 4.SDR FDEA202608261233Strap · crackedON THE LEFT SIDE BS 1640 BTW S-13L AND LOWER HINGE INTERCOSTAL STRAP, A CRACK WAS FOUND IN THE INNER CHORD STRAP; THE CRACK WAS LOCATED AT THE EDGE OF THE SECOND FASTENER HOLE FROM S-13L TO LOWER HINGE INTERCOSTAL WITH A LENGTH OF 0.190 INCHES AT THE 5 O
See all 134 reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.