N177FE
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.
22 reports on file, 2021-05-02 – 2023-04-12.
Part: FLAP — DENTED (ZONE 600) · airframe 6,505 hrs · 3,177 cycles
RH WING, OUTBOARD FLAP, LOWER SURFACE, WITH DENT (NEAR TO INBOARD FLAP TRACK). RH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R PAG. 1-9 AND B767 SRM 51-70-10-2R REP. 4 PAG. 150-151 FIG. 201 REV. 85 DEC15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 222CFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: SLAT — WORN (ZONE 600) · airframe 6,505 hrs · 3,177 cycles
RH WING, SLAT #8, TRAILING EDGE, LOWER SURFACE WITH WEAR (ABOVE OF INBOARD AUXILIARY SLAT TRACK). R.H. WING, SLAT # 8, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02- 2R, FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP 4, FIG 202 SHEET 8, PAG 150,163,164. REV 85 DEC 15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 221DFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 221DFF AT SECTION 41 OF MDC MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 222BFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2. REV 85 DEC 15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 222AFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2 REV 85 DEC 15/2022
Part: PANEL — DENTED (ZONE 200) · airframe 6,505 hrs · 3,177 cycles
DENTS ON FLOOR PANEL 221CFF AT SECTION 41 OF MDC. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022
Earlier reports · 2021–2022 · 14 reports
2022
Part: SKIN — GOUGED (RT NR 8 SLAT) · airframe 5,320 hrs · 2,599 cycles
R/W SLAT #8 T/E GOUGED W/S OSS499 REPAIRED REF B767 SRM 57-43-02-2R AND SRM 51-70-10-2R , FIG. 208
2021
Part: FRAME — CRACKED (NR 1 NACELLE) · airframe 3,208 hrs · 1,530 cycles
#1 PYLON, NAC STA 329 MID-SPAR FRAME IS CRACKED ON THE INBD UPPER CORNER REPAIRED MID-SPAR FRAME IAW B767 SRM 54-52-71-2R, FIG 201 REPAIR 4 & FEDEX EA H-5450-T0361425-P1
Part: FORMER — CRACKED (LT WING LE) · airframe 3,208 hrs · 1,530 cycles
LEFT WING FIXED LEADING EDGE @ OSS 499 HAS CRACKED FORMER REMOVED & REPLACED FORMER IAW BAC DWG 114T2161 REV - & FDX EA H-5720-T0361488-P1.
Part: WEB — CRACKED (RT WING LE) · airframe 3,208 hrs · 1,530 cycles
RIGHT WING, FIXED LEADING EDGE NOSE BEAM WEB IS CRACKED @ OSS 679 REPAIRED NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, FIG 201, REPAIR 3
Part: FAIRING — CRACKED (T/R BLOCKER DOOR) · airframe 3,208 hrs · 1,530 cycles
#1 ENGINE, INBD THRUST REVERSER, TRANSLATING COWL (SLEEVE) HAS CRACKED UPPER BLOCKER DOOR CLOSEOUT FAIRING REMOVED & REPLACED FAIRING PLATE IAW STEA CMM 78-32-32 & GE SMP 70-51-00
Part: FORMER — CRACKED (RT WING LE) · airframe 3,208 hrs · 1,530 cycles
RIGHT WING NOSE FORMER IS CRACKED @ OSS 565 REMOVED & REPLACED NOSE FORMER IAW BAC DWG 114T2162 SHT 6, REV - & FEDEX EA H-5720-T0361463-P1
Part: STAND OFF — CRACKED (NR 2 NACELLE) · airframe 3,208 hrs · 1,530 cycles
#2 PYLON, INBD LATCH BEAM, 3RD HYDRAULIC LINE STANDOFF FROM FWD SIDE IS CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 313T2380 REV -
Part: WEB — CRACKED (LT WING LE) · airframe 3,208 hrs · 1,530 cycles
LEFT WING, FIXED LEADING EDGE NOSE BEAM WEB IS CRACKED @ OSS 679 REPAIRED NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, FIG 201 REPAIR 3
Part: FAIRING — CRACKED (T/R BLOCKER DOOR) · airframe 3,208 hrs · 1,530 cycles
#2 ENGINE, INBD THRUST REVERSER TRANSLATING COWL HAS CRACKED BLOCKER DOOR CLOSEOUT FAIRING REMOVED & REPLACED FAIRING IAW STEA CMM 78-32-31 & GE SMP 70-51-00
Part: PLATE — CRACKED (T/R BLOCKER DOOR) · airframe 3,208 hrs · 1,530 cycles
#1 ENGINE, OUTBD THRUST REVERSER, TRANSLATING COWL HAS CRACKED LOWER BLOCKER DOOR CLOSEOUT FAIRING REMOVED & REPLACED CLOSEOUT PLATE IAW STEA CMM 78-32-31 & GE SPM 70-51-00
Part: ATTACH ANGLE — CRACKED (LT WING LE) · airframe 3,208 hrs · 1,530 cycles
LEFT WING FIXED LEADING EDGE, NOSE FORMER ATTACH ANGLE IS CRACKED REMOVED & REPLACED NOSE FORMER ATTACH ANGLE IAW BAC DWG 114T2240 REV - & FEDEX FEDEX EA H-5720-T0361433-P1
Part: FORMER — CRACKED (LT WING LE) · airframe 3,208 hrs · 1,530 cycles
LEFT WING, FIXED LEADING EDGE NOSE FORMER & ATTACH ANGLE ASSY CRACKED @ OSS 441 REMOVED & REPLACED FORMER & ANGLE IAW BAC DWG 114T2241 REV- & FDX EA H-5720- T0361486-P1
Part: BRACKET — CRACKED (RT WING) · airframe 3,208 hrs · 1,530 cycles
RIGHT WING INBD LEADING EDGE CAVITY @ LES 285, TORQUE TUBE GUIDE BRACKET CRACKED REMOVED & REPLACED BRACKET IAW BAC DWG 114T1240, REV -
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 3,208 hrs · 1,530 cycles
MAIN DECK FLOOR PANEL 241FFF IS PUNCTURED REPAIRED FLOOR PANEL IAW B767 SRM 53-00-50-2R