- Registered owner
- Federal Express Corporation
- Location
- Memphis, TN
- Owner type
- Corporation
- Serial number
- 41065
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 31, 2012
- Certificate issued
- September 5, 2012
- Expires
- September 30, 2028
- Mode S code
- AC34A0
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 N886FDMatched 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 N886FDMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FDEA202602160216Safety Wire · wrong partFOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FOR SERVICE.SDR FDEA202602010111Light · no testDURING PREFLT, EMERGENCY LIGHT TEST IN GALLEY, SMALL SQUARE LIGHT ABOVE L1 DID NOT ILLUMINATE IAW TEST REQUIREMENTS. REPLACED SMALL SQUARE LIGHT (AREA LIGHT) ASSY ABOVE L1 DOOR PER REFERENCE ABOVE. EMERGENCY LIGHT TEST OK. VERIFIED SMALL SQUARE LIGHT ILLUSDR FDEA202511052126Skin · damagedFOUND A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT RUD STA 487 & 4" FWD OF RUDDER TRAILING EDGE. REPAIRED A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT RUD STA 487 AS PER B777 SRM 55-40-01-2R-1 FIGURE 202, SRM 51-70-04-2R-1 FIGURE 201, SRM 51-6SDR FDEA202410241580Lamp · inoperativePOST-FLT INSP, (1EA) SUPRMNRY OVRHD EMERGENCY LT INOP. AMM: 33-50-00-2 RE-LAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.SDR FDEA202305160877Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA 1660 RBL1.DAMAGE SIZE L=2.7", OUT OF ALLOWABLE LIMIT .AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV.43.SDR FDEA202305160876Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1780 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 CRACKED AT STA1780 RBL1 DAMAGE SIZE L=2.5", OUT OF ALLOWABLE LIMIT. AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV.4SDR FDEA202305160875Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INCH DENT.DAMAGE SIZE LXW=1.8"X1. OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01-1A ALLOWABLE DASDR FDEA202305160874Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5INCH ONE DENT DAMAGE SIZE LXW=2.6"X2.5" OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01-1A ALLOSDR FDEA202305160873Flap · delaminatedLH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH FOUND DELAMINATION . EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH. DELAMINATION DAMAGE SIZE LXW=2"X1.5" OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01- 1ASDR FDEA202208242044Lamp · inoperativePRE-FLT MX INSP, (1) OVRHD EMERGENGY LT INOP SUPRNMRY AREA. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.SDR FDEA202008242000Floor Support · crackedLOWER BULK CARGO COMPARTMENT FLOOR PANEL ATTACHMENT STRINGER FOUND CRACK AT STATION 1958 RBL 41.5. LOWER BULK CARGO COMPARTMENT FLOOR PANEL ATTACHMENT STRINGER AT STATION 1958 RBL 41.5 REPAIR CARRIED OUT AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2. RESDR FDEA201901100084Indication Sys · malfunctionedAIRCRAFT DIVERTED TO RKSI, DUE TO HIGHER THAN PLANNED FUEL BURN RATE. REVIEWED MAT, COULDN'T FIND ANY RELATED MSG, REVIEWED FMC AND INDICATED FUEL ONBOARD WAS 162,700LBS, REMAIN FUEL : 20,700LBS, BURNED FUEL WAS 142,000LBS. ALSO PERFORMED EXTERNAL FUEL LEAK INSDR FDEA201712303475Skin · dentedLEFT WING NR 4 SLAT DENTED. REPAIRED THE LT WING NR 4 SLAT NOSE SKIN IAW SRM 57-43-01-2R, REPAIR.2, FIGURE.203. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405261196Unknown · malfunctionedON TAKEOFF ROLL AT APROX 1100-120KTS ALL PERFORMANCE DATA DUMPED V1,VR DISAPPEARED SPEED DATA ONLY SHOWED V2 BECAUSE IT WAS SET IN SPEED WINDOW. COMMANDED ROTATE AT V2 & WE CLIMBED OUT AT V2 20. SET 240 IN WINDOW FOR CLEAN UP ON SCHEDULE AT 3500 FT. ENGAGED
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.