- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 32967
- Year built
- 2009
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 2, 2010
- Certificate issued
- March 23, 2010
- Expires
- December 31, 2029
- Mode S code
- AC1E56
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2007 | 1 |
|---|---|
| 2010 | 1 |
| 2012 | 1 |
| 2013 | 4 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2020 | 5 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 2 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 1 |
See all 27 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N880FDMatched 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 777F28 aircraft
FAA incident reports
No FAA accident or incident reports matched to N880FDMatched 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 777F28 aircraft
Service difficulty reports · 37
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202602170225Safety Wire · wrong partRIGHT SIDE DOOR SLIDE INSPECTION REVEALED THAT THE WRONG SAFETY WIRE WAS USED. THE WO REQUIRES REPLACING THE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. RH DOOR SLIDE RAFT RETURN TO NORMAL OPS, AIRCRAFT READY FOR SERVICESDR FDEA202508021365Light · malfunctionedEMERGENCY LIGHTS ILLUMINATED DURING BEFORE START CHECKLIST. AMM 33-51-00-5 FOUND EMERGENCY LIGHT SWITCH AT THE OVERHEAD PANEL IN THE OFF POSITION. SWITCH PUT BACK TO ARM POSITION AND OPERATIONAL TEST PERFORMED IAW AMM 33-51-00-5SDR FDEA202503140410Skin · crackedRH WING NO.8 SLAT OUTER SKIN FOUND CRACKED AT 51 IN TO IB EDGE. RH WING NO.8 SLAT OUTER SKIN AT 51 INCH TO I/B EDGE CRACK AREA REPAIRED AS PER B777 SRM51-10-02-0G,51-20-01-0G,51-20-05-0G,51-40-02-0G,51-40-05-0G,51-40-08-0G,57-43-01-2R REPAIR 13 REV:47.5 AN
See all 37 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.