N178FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | on 2025-03-01 | Operator named in NTSB report |
Accident & incident history
Operated by FEDERAL EXPRESS CORP (per NTSB report)
Not yet finalized — may be revised.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.
23 reports on file, 1995-02-24 – 2025-06-02.
Part: SKIN — GOUGED (ZONE 200) · airframe 9,216 hrs · 4,526 cycles
SEQ:001131_53304585_REF 53-30/4495 REF WRI 53-30/ 4431 FOUND 2 EA GOUGES BTW STA 632AND STA 654 AND BTW S-15R AND S-16R. FIRST ONE IS 0.6" L BY 0.2" W LOCATED AFT STA 632 0.5" BLW S-15R 5T H FASTENER. 2ND DAMAGE MEASURES 0.8" L BY 0.3" W LOCATED 6.0" AFT STA 632 0.8" BLW S-15R 7TH FASTENER AFT STA 632. LABLED "F2 FOR EWR MX RH FUSELAGE SKIN BTWN STA 632/654 AND STGR 14/16 WAS REPAIRED IAW SEQ 1122 EA H-5330- T0382675B
Part: SKIN — GOUGED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
FOUND 2EA GOUGES BTW STA 632AND STA654 AND BTW S-15R AND S-16R. FIRST ONE IS 0.6" L BY 0.2" W LOCATED AFT STA 632.05" BLW S- 15R 5T H FASTENER. 2ND DAMAGE MEASURE 0.8" L BY 0.3" W LOCATED 6.0" AFT 632.08" BLW S-15R 7TH FASTENER AFT STA 632. LABLED "F2 FOR EWR MX. NO ACTIONS REQUIRED.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
PUNCTURE ON MDC FLOOR PANEL 241WFF MDC FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024
Part: SKIN — WORN (ZONE 500 FLAP) · airframe 9,214 hrs · 4,525 cycles
LEFT WING FLAP OUTBOARD ON EDGE BETWEEN ACCESS PANEL 573BB AND OUTBOARD SIDE WITH EROSION LH WING OUTBOARD FLAP BTW ACCESS PANEL 573BB AND OUTBOARD SIDE WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 51-70-30-0G PAR 5A FIG 5 SHEET 1 REV 90 AUG 15-2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
MDCC, FLOOR PANEL 242UFF WITH PUNCTURE MDCC FLOOR PANEL 242UFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15, 2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
PUNCTURE ON MDC FLOOR PANEL 251KFF. MDC FLOOR PANEL 251KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15, 2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
PUNCTURE ON MDC FLOOR PANEL 241ZFF. MDC FLOOR PANEL 241ZFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15, 2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
MDCC, SECTION 46, FLOOR PANEL 252FFF WITH PUNCTURE MDCC SECTION 46, FLOOR PANEL 252FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15, 2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
PUNCTURE ON FLOOR PANEL 231 EFF SECTION 43 OF MDC FLOOR PANEL 231 EFF SECTION 43 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15,2024
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 9,214 hrs · 4,525 cycles
MDCC, FLOOR PANEL 241AGF WITH PUNCTURE MDCC FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15, 2024
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 9,125 hrs · 4,475 cycles
MAIN CARGO COMPARTMENT HAS DAMAGE/PUNCTURED FLOORBOARD ON RH SIDE STA 1000- 1010.MWT REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD AT STA. 1000-1010, RBL 74.25"-RBL- 86.25 (MPN:145T5876-114 / PNL# 242VFF) IN REF. TO B767 SRM 53-00-50-2R REPAIR 1 FIG.201 SHEET 1. THIS IS A MAJOR REPAIR. FLOORBOARD (PNL# 242VFF) WAS NOT REMOVED, REPAIR ACCOMPLISHED ON AIRCRAFT.
Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 9,107 hrs · 4,468 cycles
BIRD STRIKE ON INITIAL TAKEOFF RWY 22L, ENGINE FIRE INDICATIONS ON RIGHT ENGINE WITH MODERATE TO SEVERE VIBRATION. QRC AND QRH COMPLIED WITH. RIGHT ENGINE SHUTDOWN AND BOTH BOTTLES DISCHARGED. RETURN TO EWR FOR FULL STOP ENGINE OUT LANDING. ***EMERGENCY DECLARED*** INSPECTED RIGHT ENGINE. FOUND TO BE UNSERVICEABLE DUE TO BIRD STRIKE. REPLACED RIGHT ENGINE, INLET COWL, AND BOTH THRUST REVERSER HALVES.
Earlier reports · 1995–2023 · 11 reports
2023
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR.4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: SLAT — WORN (ZONE 500) · airframe 6,479 hrs · 3,184 cycles
LH WING, SLAT# 5, TRAILING EDGE, LOWER SURFACE (INTERIOR) WITH WEAR ON TWO POINTS. LH WING, SLAT #5, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP.1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REP. 4 FIG. 202 SHEET 8 REV. 85 DEC15/2022
Part: SLAT — WORN (ZONE 500) · airframe 6,479 hrs · 3,184 cycles
LH WING, SLAT# 5, TRAILING EDGE, LOWER SURFACE (INTERIOR) WITH WEAR ON TWO POINTS. LH WING, SLAT #5, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP.1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REP. 4 FIG. 202 SHEET 8 REV. 85 DEC15/2022
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 6,479 hrs · 3,184 cycles
MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022
2022
Part: FORMER — CRACKED (LT WING LE) · airframe 5,381 hrs · 2,645 cycles
NOSE FORMER AT WING FIXED LEADING EDGE LH/WING OSS 441.596 HAS CRACKED. REMOVED AND REPLACED FIXED LEADING EDGE NOSE FORMER L/H WING OSS 441.N596 REF E.A 5720- T0367775 A P3 AND 767 SRM 51-40-02-OG. ORIG SUB DATE: 9/6/2022
Part: FORMER — DAMAGED (WING) · airframe 4,637 hrs · 2,270 cycles
SECONDARY WING STRCT - FIELD SERVICE EVALUATION LH SIDE OSS 441.596 REPL COMPLY WITH E..A. H-5720-T0367775 REV NO. POS. P1 INFO 31MAR22 19:01 REPAIRED DAMAGED FORMER REF EA H-5720-T0367775 P1 REPLACED BOEING FORMER 114T2120-5 WITH PN B67-57-002-01 USING EA H-5720- T0367775.
1995
Part: AIR DISTR — ODOR (FLIGHT DECK)
DURING CLIMB THROUGH APPROX 20,000 AN ACRID ODOR BECAME EVIDENT IN THE COCKPIT. ODOR DISSIPATED WHEN PACKS SECURED ON LANDING. REMOVED AND REPLACED LEFT AND RIGHT CONDENSOR BAG & LEAK CHECKED GOOD. CHECKED ALL PNUEMATICS DUCTS LEAKAGE, NO LEAKS.