N714CX
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.
3 reports on file, 2020-04-14 – 2020-04-15.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles
AIRCRAFT GROUNDED FOR CHECK-C24. STRINGER SPLICE AT STA. 434 S31R CORRODED. REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,834 hrs · 26,361 cycles
AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD 53-460-00-01, " DET - INTERNAL - BODY BELOW FORWARD CARGO COMPARTMENT FLOOR" THE FOLLOWING FINDS WERE NOTED: CORROSION ON S36L, F.S.588. REPAIRED STRINGER IAW B767-200 SRM 53-00-03 REPAIR 2.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 85,834 hrs · 26,361 cycles
AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD 53-682-00-01, "GVI - INTERNAL - FUSELAGE UPPER LOBE INTERIOR" THE FOLLOWING FINDS WERE NOTED: FOUND STRINGER CRACKED AT STATION 682 S12 LEFT. REPLACED STRINGER SECTION AT S12 L/H STA 682 AND SPLICED AT AFT END IAW B767 SRM 53-00-03 TYPE 11.