- Registered owner
- Federal Express Corp
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 40675
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 18, 2015
- Certificate issued
- September 22, 2015
- Expires
- September 30, 2028
- Mode S code
- ABF0C7
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 N869FDMatched 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 777-FS2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N869FDMatched 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 777-FS2 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202606050674Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 02EA CRACKS ON RH UPPER WING SKIN COMMON TO FASTENER #5 AS MARKED.SDR FDEA202602080223Safety Wire · wrong partREMOVE RH DOOR SLIDE FOR FEA INSPECTION OF PROPER CAD PLATED COPPER SAFETY WIRE MS20995CY16. REMOVED R1 DOOR SLIDE IN REF TO 777 AMM. SLIDE WAS REMOVED DUE TO THE WRONG WIRE INSTALLED ALSO THE TOP LEVER LATCH CLIP DAMAGED. 10 MAN LIFE RAFT INSTALLED. AMMSDR FDEA202511202194Switch · malfunctionedWHEN EMERGENCY LIGHTS SWITCH COVER IS CLOSED, THE EMERGENCY LIGHTS ARE NOT AUTOMATICALLY ARMED BY THE SWITCH COVER AND STAY IN THE OFF POSITION. MUST MANUALLY ARM SWITCH AND THEN CAREFULLY CLOSE COVER TO ENSURE LIGHTS ARE ARMED. CHECKED SWITCH FUNCTION NORMSDR FDEA202507011144Warning Light · false activationAFTER BLOCK OUT, EMER LIGHTS ICAS ALERT ILLUMINATED. WORKED WITH MANT. TURNED EMER LIGHT ARMING SWITCH TO OFF. CYCLE FLIGHT ATTENDANT EMER LIGHT SWITCH AND REARMED THE EMER SWITCH IN COCKPIT. ICAS CLEARED GMM 6-3-100 AT 37,127:43 HOUR(S), 6,163 CYCLESDR FDEA202503250492Tire · failedTIRE PRESS EICAS. NOSE TIRE #13 WAS 196PSI AT 2000Z. BY 0400Z, PRESSURE HAD DECREASED TO 173PSI. EMERGENCY DECLARED BY ATC FOR GEAR ISSUE. LANDED UNEVENTFULLY, TOWED TO GATE. AFTER LANDING LH NLG TIRE SHOWS 173. REF PDSC, R/R LH NLG TIRE PER AMM. OK TOSDR FDEA202309091568Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 FOUND CRACKED AT STA1014 LBL86. EVALUATED AND MEASURED MAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 CRACKED AT STA 1014 LBL86, DAMAGE SIZE: L=2.75", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00- 50-1A ALLOSDR FDEA201907111534Wheel · leaking5HRS INTO FLIGHT AT FL370 .82M GOT TIRE PRESS EICAS ALERT. GEAR SYNOPTIC SHOWS #9 TIRE AT 181 PSI AND AMBER. TIRE PRESS ON STATUS PAGE ALSO. REMOVED AND REPLACED #9 MAIN WHEEL ASSY REF MM 32-45-01-4. AIR PRESSURE WAS WITHIN NORMAL LIMITS WITH BRAKE TEMP AT .5,SDR FDEA201710273084Slide · malfunctionedL1 DOOR WILL NOT ARM. INSTALLED A NEW L1 DOOR ESCAPE SLIDE AND INSTALLATION CHECKED GOOD IAW AMM 25-66-01-4.SDR FDEA201710213024Slide · unwanted deployL1 DOOR SLIDE DEPLOYED DURING DOOR OPENING. BOTH DOORS DISARMED, GREEN DOORS MANUAL & M M DISPLAYED ON STATUS PAGE. REMOVED AND REPLACED THE L1 DOOR SLIDE ASSY IAW AMM 25-66-00-2, MM 25-66-01-4.SDR FDEA201710152963Warning Message · false activationFLAP OVERSPEED AT FLAPS 1, DURING DESCENT. NO ORAL WARNING, SPEED ABOUT 270-275. MAT IS GIVING THE FAULT CODE 31-71011. AIRPLANE HAS EXCEEDED VFE OVERSPEED BY 15 KNOTS, PHASE 1 INSPECTION IN PROGRESS IAW AMM 05-51-08-2, IAW AMM 27-81-00-022, & 27-51-00SDR FDEA201706101610Lens · looseEMERGENCY LIGHT LENS CAME LOOSE. LT SIDE OF THE L1 DOOR. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-00-2. EMERGENCY LIGHTS TESTED GOOD, OK FOR SERVICE.SDR FDEA201607092345Flap · damagedFOUND LT INB'D AFT FLAP HAS DAMAGE. INSTALLED LT I/B AFT FLAP AND OPS CHECK OK PER AMM27-51-12-4. A/C OK FOR SERVICE.SDR FDEA201606021792Handle · out of adjustL1 DOOR FAILS TO ARM. FOUND THE LT PAX ENTRY DOOR OUTSIDE TEE HANDLE NOT SEATED PROPERLY. COMPLIED WITH PAX ENTRY DOOR ADJUSTMENT TEST IAW MM 52-11-00-5. OPERATIONS CHECKED NORMAL. ACFT OK TO CONTINUE.
STCs 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.