N4880
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
8 reports on file, 2020-03-27 – 2022-04-18.
Part: FUEL CAP — MISSING (NA) · airframe 47,211 hrs · 28,552 cycles
PDA 2 REF LP 8408474 FUEL CAP REPORTED MISSING BY FUELER ITEM ENTERED INTO HISTORY ESFR # 1028336 CREATED
Part: FUEL CAP — MISSING (UNDERWING) · airframe 47,195 hrs · 28,548 cycles
FUEL CAP IS MISSING. FUEL CAP MISSING PLACED ON CDL. NO LEAKS NOTED. FUEL CAP MISSING PLACED ON CDL. NO LEAKS NOTED. DISPATCH DESK: 10 NAME: T W DATE: 09-FEB-22- OK TO DEFER FUEL CAP PER CDL28A. REF LP 8408523 FOR PDA INPUT.
Part: NONE — INOPERATIVE (#1) · airframe 46,256 hrs · 28,067 cycles
SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR CAB PR SYS 1 FAULT AT FL250 NO 1 CPC IS REPLACED ALREADY BY LAX BANAI 104367. SEE LOG PAGE 7597180. DUE TO REPLACEMENT OF CPC 1 AND OUTFLOW VALVE, PERFORMED OPERATIONAL TEST OF THE PRESSUER CONTROL AND MONITORING SYSTEM REF AMM 21-31-00-710. ALSO PRESSURIZED AIRCRAFT MANUALLY WITH NO FAULTS.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 43,810 hrs · 26,816 cycles
BULK CGO FR64 STR42L-43L INNER SKIN DOUBLER PLATE FND CORROSION REF NON-ROUTINE NO.9409176 - ORIGINATED BY EMP V902716, SPEC NO. A3NB-05-3-6022. PERFORMED BY EMP V902716, BULK CGO FR64 STR42L-43L INNER SKIN DOUBLER PLATE REPAIRED AS PER ECRA NO.5341-01225 REV.-
Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,810 hrs · 26,816 cycles
FWD CGO FR30-FR34 STR R41 STRINGER CLIP FOUND CORROSION REF NON- ROUTINE NO.9409147 - ORIGINATED SPEC NO.A3NB-05- 3-6013 FWD CARGO FR30-FR34 STR41R STRINGER REPAIRED PER SRM 53-21-13-30 0-003. REINSPECTION THRESHOLD 60,00 FC FROM FIRST FLIGHT REPEAT INSP TBD PER SRM 53-21-13-205-005. PLACING ON DIP AT ABOVE FREQUENCY. REF HAECO N/R 940-9147 FOR DETAILS OF WORK ACCOMPLISHED. DIP APPROVED FOR CARRY BY TOMC FOR FWD CARGO FR30-FR34 STR41R STRINGER REPAIRED PER SRM 53-21-13-30 0-003. REINSPECTION THRESHOLD 60,00 FC FROM FIRST FLIGHT REPEAT INSP TBD PER SRM 53-21-13-205-005. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED RECORDS UPDATE T/A: 60,000 TAFC ...RJS/U250018
Part: LOCK FITTING — CORRODED (FUSELAGE) · airframe 43,810 hrs · 26,816 cycles
AFT CGO DOOR NO.6 LOCK FITTING FND CORROSION.REF NON-ROUTINE NO. 9409156 - ORIGINATED SPEC NO. A3NB-53-4-6353. AFT CARGO DOOR CUTOUT #6 LOCK FITTING REPLACED AS PER SRM 51-72- 11. INSTALLED PER SRM 51-42-11 AND DWG E53476500. REF HAECO N/R 9409156 FOR DETAILS OF WORK ACCOMPLISHED.
Part: SKIN — DENTED (TAILCONE) · airframe 43,810 hrs · 26,816 cycles
FUSELAGE TAIL CONE UPPER SKIN UPPER SURFACE AT FR85-86 STRINGER 1R-2R FOUND 1EA DENT MARK REF NON-ROUTINE NO.9410324 -ORIGINATED, SPEC NO.A3NB-06-3-6001. FUSE TAILCONE FR85-FR86 STR1R-STR2R REPAIRED AS PER SRM 53-51-30 0-011 REV 132. THIS IS A CATAGORY A REPAIR. REF HAECO N/R 9410324 FOR DETAILS OF WORK ACCOMPLISHED. RII INSPECTION PERFORMED BY HAECO RII QUALIFIED INSPECTOR STAMP NUMBER ON BASE NON-ROUTINE LOG PAGE 9410324.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,810 hrs · 26,816 cycles
AFT CGO FR55-FR56, STR 43L STRINGER FND CORROSION REF NON- ROUTINE NO.9408630 - ORIGINATED, SPEC NO.A3NB-53- 4-6179. AFT CARGO FR55-FR56 STR43L CORROSION REMOVED AND MEASURED REWORK DEPTH .066". CARRIED OUT REPAIR PER SRM 53-41-13-300-010 FIG 00 2. THIS IS A CATAGORY A REPAIR ANREQUIRES NO FURTHER ACTION. REF HAECO N/R 9408630 FOR DETAILS OF WORK ACCOMPLISHED.