N894FD
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 2021-08-05 – 2024-10-08.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 19,840 hrs · 3,405 cycles
WHEN ACCOMPLISH EA G-5321-T0377185 REV B, FOUND THE PANEL STILL CAN BE REPAIRED, PLEASE EVALUATE TO REVISTE THE EA. REPAIRED MAIN DECK CARGO FLOOR PANEL AT APPROX STA 1736/LBL49.5 AS PER B777 SRM 53- 00-50 REPAIR 4 REV 47.0 AND EA:G-5321-T0377185C P4 TITLE: FUSELAGE-CARGO COMP FLOORS-MDC FLOOR PANEL UPPER FACE SHEET DAMAGE AT APPROX STA 1736/LBL49.5-INTERIM AND PERMANENT REPAIR. DETAIL PLS REF TO WRI:53215304. THIS IS A MAJOR REPAIR PER GMM 6-2-100.
Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 19,840 hrs · 3,405 cycles
RH WING OB FLAP LWR SURFACE FOUND DENT AT 4.5 IN TO AFT EDGE AND 211.5 IN TO OB. DENT LOACTION RH OB FLAP OTEF STA 316. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 316 AS PER B777 SRM 57-53-01- 2R-2 AND SRM 51-70-04-2R-14 REV 47.0 AND EA:G-5750-T0380926 P1 TITLE:WING-FLIGHT SURFACES-RH OUTBD FLAP TE WEDEG DENT AT OTEF STA 316-SRM REPAIR-RSC TRACKING. DETAIL FLS REF TO WRI:57505542. THIS IS A MAJOR REPAIR PER GMM 6-2-100.
Part: OVEN — FAILED (ZONE 900) · airframe 14,406 hrs · 2,494 cycles
PDIS 894 25-30 4173 22MAY23 ANC ACRID SMELL COMING FROM OVEN AREA. TURNED OVEN OFF AND NO MORE SMELL. NEEDS TROUBLESHOOTING. FACT 22MAY23 17:57 ANC REMOVED OVEN WITH THE STANK, REPLACED WITH NEW OVEN REF B777 AMM 25-32-52-4-2 OPS CHECK GOOD, CLEANED EXISTING RACK AND TRAYS, NO MORE SMELL NOTICED.
Part: DOOR — CRACKED (ZONE 800) · airframe 10,298 hrs · 1,817 cycles
FOUND CRACKS OF THE FORWARD LARGE CARGO DOOR UPPER BEAM WEB. THE LOWER FORWARD CARGO UPPER BEAM WEB CRACKED AREA REPAIRED AS PER EA G-5230- T0367803 P1. TITLE :DOORS -CARGO DOOR /HYD SYS - -PUNCTURE ON LOWER FORWARD CARGO DOOR UPPER BEAM WEB AT STA530 .REFER TO WRI:52303277 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100
Part: FLOOR PANEL — DAMAGED (200) · airframe 10,298 hrs · 1,817 cycles
MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND DELEMINATION AT STA1660 BL0. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT STA 1660 BL 0 REPAIRED AS PER B777 SRM 53-00-50-2R, REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
Part: GCU — FAILED (LEFT) · airframe 7,864 hrs · 1,387 cycles
DURING CRUISE L GEN DROPPED POWER (ON ELECTRIC SYNOPTIC PAGE) AND L MAIN AC BUS WAS NOT POWERED INTERMITTENTLY. R/I 03AUG21 13:10 CGN U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 756603E POS: P1 SRL: AAA3002714 TAG NBR: 14G788 ON MPN: 756603F CPN: 2413479 SRL: AAA3005031 TAG NBR: 787H36 FACT 03AUG21 13:10 CGN U FOUND MX-MSG: 24-11786. PERFORMED TS AS PER FIM 24-51-00-2-0 TASK 24-51-00-810-833 AND RELOADED ELMS SOFTWARE IN SIU#2(P110) (BOTH CHANNELS) AS PER AMM 24-09-00-2-2. VERIFIED CORRECT SOFTWARE PN. RELOAEDED SOFTWARE INTO BPCU AS PER AMM 24-41-05-2. VERIFIED CORRECT PN INSTALLED. PRECAUTIONARY REMOVED AND REPLACED LH GCU AS PER AMM 24-22-02-4. VERIFIED CORRECT SOFTWARE PN. PERFORMED OPERATIONAL CHECK OF THE AC SYSTEM PER AMM 24-22-00-5 DURING ENGINE RUN. NO DEFECTS NOTED. NO ACTIVE FAULTS. FACT 08AUG21 00:44 IND REMOVED & REPLACED LEFT GCU & OP`S CHECKED REF FDX B777 AMM 24-22-02-4. & FDX B777 JRH. OK FOR SERVICE.