N486AX
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
5 reports on file, 2021-04-10 – 2026-04-08.
Part: COOLING FAN — VIBRATION · airframe 78,518 hrs · 16,005 cycles
FAINT ELECTRICAL SMELL BEGAN, ACCOMPANIED BY LIGHT VIBRATION FWD EQ EXH FAN STATUS MESSAGE DISPLAYED, FOLLOWED BY DISAPPEARANCE OF VIBRATION AND ELECTRICAL SMELL.
Part: CDU — INTERMITTENT (UNKNOWN) · airframe 74,509 hrs · 15,073 cycles
L CDU FAILURE, L FMC FAILURE: DURING FLIGHT CREW REPORT THE L FMC FAILED. DISCUSSIONS WITH MOC AND DO. ALL PARTIES AGREED TO CONTINUE. CREW CALLED BACK 1 HOUR LATER AND STATED THE L CDU FAILED AND WENT BLANK. FIGHT DIVERTING TO ANC DUE TO ETOPS AND FUEL RESTRICTIONS.
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 71,898 hrs · 14,466 cycles
CORROSION TOP OF STABILIZER BOX ASSESSMENT FRONT RIGHT SPLICE. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED DAMAGE ON H-STAB BOX UPPER SKIN FROM FRONT SPAR TO S-11 AT RBL 13.833 IAW STS EA 79-2022-141 REV IR AND OMNI AIR INTERNATIONAL EO B7655-10 INITIAL ISSUE REFERENCE Q1 AVIATION W/O 139617-2, 139617-3 AND 139617-16 FOR ALL NDT HFEC, RHEC AND UT REQUIREMENTS NIL FINDINGS THIS IS A CAT B REPAIR WITH FIRST STAGE APPROVAL WHICH APPROVES THE STATIC STRENGTH DATA AND WHICH PROVIDES THE SCHEDULE FOR SUBMITTAL OF THE DT DATA WHICH MUST BE SUBMITTED NO LATER THAN 24 MONTHS FROM THE DATE OF THIS FORM.
Part: TRANSMITTER — FAILED (HYD SYSTEM) · airframe 68,902 hrs · 13,786 cycles
LE SLAT DISAGREE CAUTION MESSAGE AT 35,000 FT ~ REMOVED AND REPLACED CENTER HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-31. OPS CHECK NORMAL.
Part: SENSOR — CONTAMINATED (SLAT SYS) · airframe 68,251 hrs · 13,639 cycles
LE SLAT DISAGREE EICAS ON DEPARTURE CLIMB AND ENROUTE. CORRECTIVE ACTION: PERFORMED BITE PROCEDURE AND GAVE MESSAGE 2781045 WHICH LEADS TO B762 FIM 278100 101 FIG 106 PSEU BITE TARGET PROCEDURE LEADS TO S305 ON #7 INBD SLAT FIM 3209 00 101 FIG 104 S305 SENSOR FOUND WITH PAINT ON IT SANDED AND WITHIN LIMITS OPS CHECKED GOOD NO FURTHER MESSAGES PREVIOUS FSEU BITE PROCEDURE DONE IAW B762 FIM 2751 FAULT TREEE 809