N350VJ

BOMBARDIER INC BD-100-1A10 · 2015 · Valid Registration

Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
XOJET Aviation LLC (AWKA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

B · 2026-03-18 Matched by certificate designator
ATA 4940

APU FAILED TO START ON PAST 2 APPROACHES. CYAN APU SHUTDOWN CAS POSTED. ON SUBSEQUENT ATTEMPT AFTER LANDING THERE WAS A VERY STRONG SMELL OF FUEL IN THE CABIN. MX C/A: INSPECTED APU INLET AND APU IGNITER, APU INLET WAS CLEAR AND APU IGNITER WAS WITHIN LIMITS BUT SHOWED SIGNS OF WEAR. PERFORMED 4 SATISFACTORY STARTS OVER TWO HOURS WITH NO DEFECTS OR SMELLS NOTED. RECOMMEND CHECKING OIL PRESSURE SWITCH WIRING. NO DEFECTS NOTED AT THIS TIME. WORK PERFORMED IN REF TO HONEYWELL GTC56-150BD LMM 49-40-33. BOMBARDIER CL350 AMM 49-00-00.

Source: SDR U5QA202603180168 · FAA SDRS
E J · 2018-10-16 Matched by certificate designator
ATA 7200

WE WERE CLEARED TO CLIMB TO 15000FT ON RUNWAY HEADING. CLIMBING THROUGH 7000FT A VIBRATION WAS FELT, FOLLOWED BY AN ENGINE VIBRATION CAS MSG AND ENGINE EXCEEDANCE CAS MSG. THE LEFT THRUST LEVER WAS PULLED TO IDLE (THE ENGINE EXCEEDANCE CAS MSG WENT AWAY) AND AN EMERGENCY WAS DECLARED. A VECTOR TO DOWNWIND 36R WAS GIVEN ALONG WITH A DESCENT TO 5000FT. I SET THE AVIONICS FOR LANDING AND RAN THE ENGINE VIBRATION CHECKLIST FROM QRH 2 WITH INSTRUCTED TO LEAVE THE ENGINE RUNNING AT IDLE. THEN THE SINGLE ENGINE LANDING CHECKLIST WAS COMPLETED. THE ENGINE WAS SHUT DOWN VIA FADEC INSIDE OF THE FINAL APPROACH FIX DUE TO A RISE OF ITT AND VIBRATION (THE ENGINE EXCEEDANCE CAS MSG REAPPEARED). DUE TO THE CLOSE PROXIMATE TO LANDING, WE ELECTED TO SELECT THE ENGINE RUN SWITCH TO OFF TO AVOID INADVERTENT RESTART VIA FADEC. THRUST REVERSER WAS NOT USED ON LANDING. THE FMS INDICATED A 700LB OVER WEIGHT LANDING. MAINTENANCE PERSONAL OBSERVED METAL DEBRIS INSIDE THE MIXING NOZZLE AFTER THE EVENT.

Source: SDR KKVA2018102316002 · FAA SDRS