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
FOUND RHREE (3) CORROSION REAS ON LONGERON CHORD AT STA 1065 TO STA 1087, STR 23R TO STR 24R.
FOUND A CRACK ON THE LOWER CHORD VERTICAL FLANGE, STA 850 TO STA 860, RBL 74.75
FOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12
FOUND SEVERAL DELAMINATION ALONG WITH CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 11 TO FSS12
FOUND SEVERAL DELAMINATION ALONG WITH EDGE CRUSHING DAMAGE ON VERTICAL STABILIZER, LH SIDE EXTERNAL SKIN PANEL, FSS 92 TO FSS 270
FOUND SEVER DELAMINATION ALONG WITH CRUSHING DAMAGE AT SEVERAL LOCATION ON VERTICAL STBILIZER, RH SIDE, EXTERNAL SKIN PNEL, FSS 11 TO FSS 92
FOUND CORROSION ON TEAR STRAP, STA 1197+88, STR 39L TO STR 38R
FOUND SEVERAL DISBONDING ON LEFT HORIZONTAL STABILIZER LOWER SURFACE ON PANEL 335HB.
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.
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.