N348FX
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.
7 reports on file, 2015-09-13 – 2024-09-23.
Part: FCE — UNSERVICEABLE (ZONE 100) · airframe 10,386 hrs · 7,196 cycles
CREW RECEIVED FLAP FAIL CAS AND INDICATION DURING FLAP SELECTION TO 1 AFTER START. REPLACED FAULTY FCE #1 IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD, NO FURTHER FAULTS NOTED.
Part: FCE — FAULTED (FLAP SYS) · airframe 10,386 hrs · 7,196 cycles
FLAPS FAIL CAS AND INDICATION WHEN FLAPS 1 WAS SELECTED DURING THE AFTERSTART FLOW. THE CAS MESSAGE REMAINED AFTER AN ELECTRICAL RESET. REPLACED FAULTY FCE 1 WITH A REPAIRED UNIT IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTS FOUND.
Part: CONTROLLER — FAULTED (TRIM SYSTEM) · airframe 10,092 hrs · 6,968 cycles
DURING CRUISE AT FL340, PTRIM NML FAIL CAS ILLUMINATED. CREW RAN CHECKLIST AND HAND FLEW THE AIRCRAFT TO DESTINATION USING BACKUP TRIM. REPLACED FCE # 2. PERFORMED SPOILER RIGGING AND FOLLOW-ON OPS CHECKS. OPS CHECKED GOOD. WORK COMPLETED IEW EMB 505 AMM 27-03-01.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 9,125 hrs · 6,268 cycles
GO AROUND DUE TO FLAP FAIL CAS WHEN SELECTING FLAPS 3 FROM FLAPS 2 (STUCK AT FLAP 2). CREW EXECUTED A FLAP 2 LANDING PER QRH, AIRCRAFT LANDED WITHOUT INCIDENT AT KDAL. REPLACED FCE #1 IAW PHENOM 300 AMM 27-03-01. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,230 hrs · 4,966 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REPLACED THE FWD AND AFT EMERGENCY LIGHT BATTERIES WITH INSPECTED UNITS, IAW EMB 505 AMM 33-52-01. PERFORMED THE BATTERY OPERATIONS CHECKS ON BOTH UNITS. FWD P/N 6450LS-00; S/N 001283. AFT P/N 6450LS-00; S/N 001662.
Part: STARTER GEN — FAILED (NR 2 ENGINE) · airframe 5,870 hrs · 4,028 cycles
DIVERTED DUE TO ENGINE VIBRATION FOLLOWED BY GEN FAIL. SHUT DOWN NR 2 ENGINE PER THE CHECKLIST. DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. R&R NR 2 STARTER/GENERAL AND C/W UNSCHEDULED STARTER/GENERATOR SPECIAL INSPECTION. ALL CHECKS NORMAL.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 3,087 hrs · 2,080 cycles
PITCH TRIM BACK UP FAIL CAS MESSAGE DISPLAYED. REMOVED AND REPLACED THE PITCH TRIM ACTUATOR. REMOVED SN 0122 AND INSTALLED SN 0044. OPS CHECK GOOD.