N358FX
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.
8 reports on file, 2017-11-13 – 2025-06-10.
Part: FCE — FAULTED (ZONE 100) · airframe 10,109 hrs · 7,021 cycles
PITCH TRIM BACKUP FAIL CAS DURING TRIM CHECK WHEN SELECTING NOSE DOWN. REPLACED #1 FCE IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTS FOUND.
Part: FCE — FAULTED (ZONE 100) · airframe 10,074 hrs · 6,993 cycles
CREW RECEIVED FLAP FAIL CAS AFTER SELECTING FLAPS 1 FROM 0 IN FLIGHT BEFORE LANDING. REPLACED THE FCE #1 IAW EMB 505 AMM 27-03-01. PERFORMED FLAP RIGGING PROCEDURE AND ALL REQUIRED OPS CHECKS.
Part: TORQUE TUBE — CRACKED (RUDDER) · airframe 8,935 hrs · 6,211 cycles
DURING MAINTENANCE, LEFT RUDDER TORQUE TUBE STABILIZER ROD FOUND CRACKED. REPLACED BOTH LEFT AND RIGHT RUDDER TORQUE TUBE STABILIZER RODS IAW PHENOM 300 AMM 27-21-01.
Part: FLT CONTROLS — FAULT MESSAGE · airframe 7,172 hrs · 4,932 cycles
DIVERTED DUE TO FLAP FAIL AND SPOILER FAULT CAS DURING CLIMB THROUGH 12,000 FT. FOLLOWED QRH; CYCLED FLAPS 3 TIMES WITH X ON FLAP INDICATOR. EXECUTED NO FLAP LANDING WITHOUT INCIDENT AT KMCO. REPLACED # 1 FLIGHT CONTROL ELECTRONIC (FCE) UNIT IAW PHENOM 300 AMM 27-03-01-408. RIGGED IAW AMM 27-50-00-820. OPS CHECKS GOOD.
Part: ELECTRONIC UNIT — FAILED (FLT CONTROL) · airframe 6,433 hrs · 4,416 cycles
GROUND SPOILER FAIL ILLUMINATED IN FLIGHT. REPLACED FCE 2. OPS CHECKED GOOD. WORK COMPLETED IAW AMM 27-03-01. P/N S/N 0871.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,844 hrs · 4,036 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY, IAW AMM 33-52-01, NO DEFECTS NOTED. P/N OFF/ON: G450LS-00; S/N OFF: 001013; S/N ON: 001023.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 3,976 hrs · 2,737 cycles
PITCH TRIM ACTUATOR LEAKING OIL. REMOVED AND REPLACED THE PITCH TRIM ACTUATOR IAW AMM 27-41-01.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 3,584 hrs · 2,460 cycles
PTRIM NML FAIL AFTER ABOUT 1.5 HOURS AT FL430. PERFORMED WM 27-43-50-13 SHEET 3. NO DEFECTS NOTED. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPERATIONAL CHECK GOOD IAW AMM 27-41-00. NO FURTHER DEFECTS NOTED.