N5310
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, 2006-05-16 – 2014-02-26.
Part: FLOOR SUPPORT — CORRODED (FRAMES 87-89) · corrosion level 2 · airframe 26,516 hrs · 16,485 cycles
RT FLOOR SUPPORT BETWEEN FRAMES 87-89 CORRODED. R & R FLOOR SUPPORT.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,408 hrs · 43,444 cycles
DURING ROUTINE C CHECK INSPECTION, ELECTRONIC COMPARTMENT STRINGER 26R CORRODED AT BS 460 REF NR 0973.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,299 hrs · 12,356 cycles
CROSSBEAM AT FS 280.00, RBL 9.00, WL 70.00 IS CRACKED IN THE LOWER RADIUS. CROSSBEAM REPAIRED IAW REO 601R-53-11-171, REV D, SCHEME B. (K)
Part: STRINGER — CORRODED (FUSELAGE) · airframe 12,433 hrs · 12,860 cycles
PDX: C3. X35 TO X47 AT STRINGER 31L HAS LIGHT CORROSION. MAINTENANCE REPAIRED IAW Q400 SRM 51-21-00, NDTM PART 6, 51-00-01-250-801, HORIZON EA 6-53-690 AND SRM 51-42-05.