N4879
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.
4 reports on file, 2019-12-24 – 2019-12-30.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 44,628 hrs · 22,749 cycles
BULK CGO REAR FR65-FR66 STR31R STRINGER FND CORROSION REFER NON- ROUTINE NO.:9493202, ORIGINATED SPEC NO.A3NB-53- 3-6185. PERFORMED, BULKCARGO FR64-FR66 STR 31R STRINGER REPLACED AS PER ECRA 5341-01202 REV A.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,628 hrs · 22,749 cycles
L2 DOOR DOOR SILL UPPER SURFACE FOUND CORROSION FROM FR66 TO FR68 Y1512 REFER NON-ROUTINE NO.:9493534, ORIGIANTED SPEC NO.A3NB-53-3-6222. PERFORMED ,THE L2 DOOR DOOR SILL UPPER SURFACE CORROSION FROM FR66 TO FR68 Y1512 REPLACED AS PER SRM 51-42-11 REV129 AND SRM 51-72-11 REV 129 AND DWG D53480505 ISSUE CE.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,628 hrs · 22,749 cycles
R2 DOOR SILL UPPER SURFACE FOUND CORROSION FROM FR66 TO FR68 Y-1512(2 LOCATIONS) REFER NON-ROUTINE NO.:9493398, ORIGINATED SPEC NO.A3NB-53-3-6187. PERFORMED ,THE R2 DOOR DOOR SILL UPPER SURFACE CORROSION FROM FR66 TO FR68 Y-15.12,REPLACED AS PER SRM 51-42-11 REV129 AND SRM 51-72-11 AND AS PER DWG D53480505 ISSUE:CE.
Part: SKIN — CORRODED (CARGO DOOR) · airframe 44,628 hrs · 22,749 cycles
FWD CGO DOOR FR26-FR26A INNER STRUCTURE LOWER SURFACE FND CORROS ION REF NON-ROUTINE NO.9493539,SPEC NO.A3NB-52-3-6038. WORK WAS ACCOMPLISHED ON HAECO XMN NR 9497255 AND 9493539. DIP FOR RE-INSPECTION CREATED ON LP 4135069.