N359FX
Registered owner: FLEXJET LLC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Flexjet, LLC (J7SA) | Certificate holder | — | Matched by certificate designator |
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, 2016-04-06 – 2026-07-13.
Part: FLT CONTROLS — MULTIPLE FAIL · airframe 11,106 hrs · 7,806 cycles
DIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01.
Part: WARNING MESSAGE — FALSE ACTIVATION (BRAKE SYSTEM) · airframe 5,428 hrs · 3,818 cycles
ON TAXI OUT, BRK FAIL CAS MESSAGE APPEARED. NO BRAKE ACTION AVAILABLE FROM MAIN BRAKES. USED EMERGENCY/PARKING BRAKE TO SAFELY POSITION AND STOP THE AIRPLANE.PERFORMED MAIN BRAKE SYSTEM FUNCTIONAL TEST I.A.W PHENOM 300 A.M.M 32-41-00-720-801-A. NO DEFECTS NOTED BRAKE SYSTEM PASSED THE TEST.
Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 4,439 hrs · 3,111 cycles
DIVERTED DUE TO SWPS FAULT, PITRIM BKP FAIL, FLAP FAIL, SPOILER FAULT, RED XS IN FLAP INDICATOR BOX AND RED XS IN PITCH INDICATOR BOX AT ALTITUDE. R & R #1 FCE. PERFORMED RIGGING AND OPS CHECKS WITH NO DEFECTS NOTED AT THIS TIME.
Part: STARTER GEN — FAILED (LT ENGINE) · airframe 2,932 hrs · 2,025 cycles
DIVERTED DUE TO A BANG AND VIBRATION IN FLIGHT, FOLLOWED BY LT GENERATOR GOING OFFLINE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LT ENGINE STARTER/GENERATOR WITH NEW. OPS CHECKS NORMAL PER AMM 24-31-01. PERFORMED FIM 24-31-00-810-829-A NO DEFECTS NOTED AFTER REPLACING THE LT STARTER/GEN. PERFORMED EMM TASK 05-50-00-210-821 NO DEFECTS OR LEAKS NOTED. PERFORMED RT ENGINE STARTER/GEN BRUSHWEAR CHECK. SHORTEST IS 0.050" PER AMM 24-31-01-220-801-A. P/N 400SG180Q S/N 500956XL
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 2,137 hrs · 1,443 cycles
DURING CLIMB OUT, CAS MESSAGE NML PITCH TRIM FAIL CAME ON. NORMAL PITCH TRIM HAD FAILED CONTINUED TO 450FL USED BACKUP TRIM. REMOVED THE PITCH TRIM ACTUATOR AND REPLACED WITH A REPAIRED ACTUATOR IAW P-300 AMM 27-41-01. PERFORMED HORIZONTAL STABILIZER ELECTRICAL STOP FUNCTIONAL CHECK IAW AMM 27-0-01.