N714QX
Registered owner: LEWIS JUSTIN S P, OK (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.
2 reports on file, 2012-04-14 – 2012-04-18.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 20,144 hrs · 20,262 cycles
STRINGER 30P, STRINGER SPLICE BETWEEN STA X-39.00 AND X -18.250 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801. DAMAGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4456. ALODINED, PRIMED AND PAINTED IAW RD 8/4-53-4456. APPLIED CPC IAW AMM 51-25-01-390-801. COMPLIED WITH TASK CARD RD 8/4-53-4456.
Part: THRESHOLD — CORRODED (FUELAGE) · airframe 20,144 hrs · 20,262 cycles
STUB FRAME FLANGE ANGLE BELOW PAX DOOR THRESHOLD HAS CORROSION OTBD OF STRINGER 25P AT STA X9.00. REMOVED FLANGE ANGLE IAW SRM 51-42-05-02-01. MATCH DRILLED NEW ANGLE, ALODINED AND INSTALLED STUB FRAME FLANGE ANGLE IAW SRM 51-40-07-02-01, 51-21-10-02-01 AND 51-42-05-02-01. APPLIED PROTECTIVE COATINGS IAW SRM 51-25-10-02-01, 51-25-15-02-01 AND AMM 51-25-01-390-801.