Registered owner
Federal Express Corp
Location
Memphis, TN
Owner type
Corporation
Serial number
42704
Year built
2017
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
November 13, 2017
Certificate issued
November 14, 2017
Expires
November 30, 2027
Mode S code
AC3C0E

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 91

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2000In forceSuperseded2026
ADs by the year they took effect: 112 ADs
20001
20071
20092
20103
20112
20129
20138
201411
20157
20166
20175
20183
20192
202010
20214
20228
202310
20248
20256
20266
See all 113 ADs

Information bulletins that may apply · 9

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N888FDMatched 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 777F aircraft

FAA incident reports

No FAA accident or incident reports matched to N888FDMatched 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 777F aircraft

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR FDEA202602150250Reservoir · failedPREFLIGHT CHECK FOUND LEFT ENTRY DOOR EPAS RESERVOIR PRESSURE DROP TO 0. REMOVED AND REPLACED LH EPAS RESERVOIR REF B777 AMM 52-11-22-4.Feb 15, 2026 · N888FD · Boeing 777F · Emergency EquipmentSDR FDEA202509051622Skin · dentedRIGHT WING OB FLAP LWR SURFACE FOUND DENT AT 248 INCHES TO IB EDGE AND 6 INCHES TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 261 AS PER B777 SRM 57-53-01-2R- 2 AND SRM 51-70-04-2R-1 REV 47.6 AND EA: G-5750-T0384798 P1. TITLE: WING-FLSep 5, 2025 · N888FD · Boeing 777F · Trailing Edge FlapsSDR FDEA202303310534Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 CRACK.SIZE:L=1.6" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00Mar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202303310533Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1475/RBL27-29 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6) AT STA1475/RBL27-29 CRACK.SIZE:L=1.8" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-50-1Mar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202303310532Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 CRACK.SIZE:L=1.4" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM Mar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202303310531Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1391.25/LBL42.75-44.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF (P/N:152W8652-21) AT STA1391.25/LBL42.75-44.5 CRACK.SIZE:L=1.7" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PERMar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202303310530Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 CRACK.SIZE:L=1.5" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-Mar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA202303310529Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 CRACK.SIZE:L=1.2" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777Mar 31, 2023 · N888FD · Boeing 777FS2 · Fuselage Floor PanelSDR FDEA2018110213076Slide · inoperativeAFTER BLOCK IN AND BEFORE AIR CREW COULD DISARM TLH ENTRY DOOR, RAMP PERSONEL OPENED DOOR FROM OUTSIDE SLIDE FELL OUT BUT DID NOT DEPLOY. INSTALLED L1 DOOR MOUNTED ESCAPE SLIDE IAW AMM : 25-66-01-4. FOUND EPAS RESERVOIR PRESSURE AT ZERO. REMOVED AND RENov 1, 2018 · N888FD · Boeing 777FS2 · Escape Slide

STCs that may be installed · 61

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 61 STCs