N495AX
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.
10 reports on file, 2019-09-12 – 2023-06-22.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND A CRACK ON THE LOWER CHORD VERTICAL FLANGE, STA 850 TO STA 860, RBL 74.75
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND CORROSION ON TEAR STRAP, STA 1197+88, STR 39L TO STR 38R
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND SEVERAL DELAMINATION ALONG WITH EDGE CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 92 TO FSS 270
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND RHREE (3) CORROSION REAS ON LONGERON CHORD AT STA 1065 TO STA 1087, STR 23R TO STR 24R.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,272,311 hrs · 19,899 cycles
FOUND SEVER DELAMINATION ALONG WITH CRUSHING DAMAGE AT SEVERAL LOCATION ON VERTICAL STBILIZER, RH SIDE, EXTERNAL SKIN PNEL, FSS 11 TO FSS 92
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,723 hrs · 19,899 cycles
FOUND SEVERAL DISBONDING ON LEFT HORIZONTAL STABILIZER LOWER SURFACE ON PANEL 335HB.
Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 90,938 hrs · 19,630 cycles
DURING CRUISE FLIGHT, AUTOTHROTTLES DISCONNECTED FOLLOWED BY ALL AUTOPILOTS DISENGAGED AND LEFT FLIGHT DIRECTOR FAILED. REPLACED THE CAPTAIN'S ASA IAW AMM 22-14 AND LEFT TPM IAW AMM 24-32. AUTOPILOTS & AUTOTHROTTLE CHECKED IAW MCDP, GROUND TESTED, NO FAULTS AT THIS TIME ALSO REPLACED CB.
Part: CONNECTOR — DEFECTIVE (RT ENGINE) · airframe 89,762 hrs · 19,433 cycles
INFLIGHT LOST EGT INDICATION ON RIGHT ENGINE ON BOTH UPPER EICAS AND STBY INDICATION. ACCOMPLISHED FIM 77-21. FAULT TREE 806. REMOVED & REPLACED JUNCTION BOX PER AMM 77-21. OPS CHECK NORMAL.