N368FX
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.
6 reports on file, 2018-12-26 – 2026-07-22.
Part: FCE — FAULTED (ZONE 100) · airframe 9,920 hrs · 6,740 cycles
P-TRIM NML FAIL DURING TRIM TESTS. REPLACED FCE 2 AND PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW EMB 505 AMM 27-03-01 AND 27-60-00.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,359 hrs · 2,946 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REPLACED FWD EMERGENCY BATTERY, IAW P300 AMM 33-52-01. P/N 6450LS-00; S/N 002518.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,231 hrs · 2,874 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK. NO FURTHER DEFECTS FOUND, IAW PHENOM 300 AMM 33-52-01. P/N 6450LS-00; S/N 002685.
Part: ELECTRONIC UNIT — MALFUNCTIONED (SPEED BRAKES) · airframe 3,724 hrs · 2,630 cycles
DESCENDING THROUGH 10,000 FEET MSL AT 260 KIAS, OPENED SPEED BRAKE AND RECEIVED A CAS GND SPLR FAIL, CAS SPOILER FAULT, AND FAIL UNDER SPOILER ON MFD. REMOVED AND REPLACED FCE NR 2 IAW AMM 27-03-01. PERFORMED RIGGING AND OPS CHECK WITH NO DEFECTS NOTED.
Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 3,717 hrs · 2,626 cycles
DISCOVERED EMERGENCY LIGHTS FLASH ON AND OFF IN ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY LIGHT BATTERIES IAW AMM 33-52-01. OPS CHECKED GOOD.
Part: STARTER GEN — MALFUNCTIONED (NR 1 ENGINE) · airframe 2,218 hrs · 1,585 cycles
DIVERTED DUE TO VIBRATION NOTICED FOLLOWED BY A "GEN 1 OFF BUS" CAS. NR 1 ENGINE WAS THEN SHUT DOWN IAW CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. R&R STARTER/GEN AND COMPLIED WITH 05-50-02 UNSCHEDULED STARTER/GEN REMOVAL INSP WITH NO DEFECTS NOTED.