N346FX
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.
10 reports on file, 2014-06-23 – 2026-04-08.
Part: GLARE SHIELD — SMOKE (ZONE 200) · airframe 12,787 hrs · 8,674 cycles
DIVERTED TO KMRY DUE TO AN ELECTRICAL BURNING SMELL IN THE CABIN. DURING CRUISE, THE PIC NOTED A RED X APPEAR OVER COM2 WHICH THEN EXTINGUISHED AND REAPPEARED MULTIPLE TIMES SHORTLY THEREAFTER. THE CREW OBSERVED SMOKE EMANATING FROM THE GLARESHIELD PROMPTING THEM TO DON THEIR OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED GIA 2 IAW EMB 505 AMM 31-41-05. ALL FOLLOW-ON CHECKS PASSED.
Part: ELECTRONIC UNIT — ABNORMAL (TE FLAPS) · airframe 11,148 hrs · 7,509 cycles
DIVERTED DUE TO FLAP FAIL CAS DURING APPROACH WITH GEAR DOWN AT 1500FT AGL. CREW PERFORMED GO AROUND, RAN QRH, AND LANDED WITHOUT INCIDENT AT KAUS. REPLACED THE FCE 1 IAW EMB 505 AMM 27-03-01. RIG AND OPS CHECKS GOOD.
Part: CONTROL UNIT — FAILED (NR 1) · airframe 11,145 hrs · 7,508 cycles
CREW RECEIVED FLAP FAIL, SWPS FAULT, PTRIM BKP FAIL, AND SPOILER FAULT ON POWER UP AND PERFORMED TWO UNSUCCESSFUL RESETS. REPLACED # 1 FCE IAW PH300 AMM 27-03-01. RIGGED AND OPS TESTED WITH NO DEFECTS FOUND.
Part: ELECTRONIC UNIT — UNSERVICEABLE (UNKNOWN) · airframe 10,279 hrs · 6,910 cycles
ON DESCENT, SWPS FAIL AND PTRIM BKP FAIL CAS ILLUMINATED. CREW RAN QRH, DETERMINED THIS WAS A TRUE FLAP FAILURE, DECLARED EMERGENCY WITH ATC, NOTIFIED PAX, AND LANDED WITHOUT INCIDENT AT KRAP. TROUBLESHOT ISSUE TO FCE # 1. REPLACED FCE #1 IAW EMB P300 AMM 27-50-00 AND 27-03-01. PERFORMED RIGGING AND OPS CHECKS WITH NO DEFECTS NOTED.
Part: NONE — NONE · airframe 9,014 hrs · 5,980 cycles
AIR TURN BACK DUE TO BLEED 1 OFF AND BLEED 1 FAIL CAS. RAN QRH, TURNED BLEED 1 SWITCH OFF FOR 60 SECONDS. DURING 60 SECOND PERIOD, BLEED 2 OFF AND BLEED 2 FAIL CAS ILLUMINATED. PERFORMED EMERGENCY DESCENT; DECLARED EMERGENCY; MANUAL PAX MASK DEPLOYMENT. CABIN ALTITUDE SEEN AT 19,000'. AT 20,000â RE-PERFORMED QRH AND ALL BLEED FAULTS CLEARED. AIRCRAFT LANDED SAFELY AT KNEW. REPLACED RH PRECOOLER DUE TO BROKEN INTERNAL FIN. COMPLETED SL505-36-0003 REV 2. OPS AND LEAK CHECK GOOD IAW PH 300 AMM 36-11-05/400 AND SL505-36-0003 REV 2.
Part: NONE — NONE · airframe 8,896 hrs · 5,910 cycles
DIVERTED DUE TO CABIN ALTITUDE PRESSURIZATION INCREASING AT A RATE OF 800FT PER MINUTE. THE CREW IMMEDIATELY INSTRUCTED ATC THEY NEEDED TO DESCEND. THE PRESSURIZATION RATE WAS NOT DECREASING DURING DESCENT, CAUSING THE CREW TO DECLARE AN EMERGENCY. THE CABIN ALTITUDE WENT ABOVE 10,000FT AND THE AIRCRAFT WENT INTO EMERGENCY DESCENT. ONCE THEY DESCENDED TO 15,000FT THE CABIN RATE BEGAN DECREASING TO THE PROPER PRESSURIZATION. AIRCRAFT LANDED WITHOUT INCIDENT AT KJAX. REPLACED PRESSURE RELIEF VALVE WITH A NEW GASKET IAW PHENOM 300 AMM 21-31-04/400. OPS, PRESSURIZATION, AND LEAK CHECK GOOD. P/N 103918-2; S/N 13918-00622.
Part: RUDDER CONTROL — MALFUNCTIONED · airframe 8,845 hrs · 5,877 cycles
VENTRAL RUDDER FAIL CAS ON SHORT FINAL IN HEAVY CROSS WIND CONDITIONS. DURING POST FLIGHT, FOUND VENTRAL RUDDER FULLY DEFLECTED AND FROZE TO THE LEFT. PERFORMED VISUAL INSPECTION OF AIRCRAFT, NO DAMAGE NOTED. TROUBLESHOT IAW FIM 22-11-00. PERFORMED VENTRAL RUDDER SERVICE OPERATIONAL CHECK THREE TIMES AS DIRECTED BY FIM IAW AMM 27-26-01. NO FAULTS FOUND. INSPECTED VENTRAL RUDDER SURFACE DRIVE MECHANISM, LINKAGE CABLES, AND STOPSâNO DEFECTS NOTED. VENTRAL RUDDER SURFACE OPS CHECK GOOD IAW AMM 27-26-01. PERFORMED CMC DOWNLOAD FOR FURTHER REVIEW.
Part: CONTROL UNIT — FAILED (BRAKES) · airframe 5,294 hrs · 3,572 cycles
BRAKES FAILED CAS MESSAGE ON LANDING. MAIN BRAKES DID NOT WORK. BOTH MAIN TIRES HAD FLAT SPOTTED. R & R THE BRAKE CONTROL UNIT AND BOTH MAIN WHEEL AND TIRE ASSYS. OPS CHECKED GOOD.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 2,427 hrs · 1,623 cycles
PITCH TRIM NORMAL FAIL CAS (MSG) COMES ON IN FLIGHT. REMOVED PITCH TRIM ACTUATOR P/N 467500-1003 S/N 0038 AND INSTALLED REPAIRED ACTUATOR P/N 467500-1003 S/N 0047. OPS CHECKED GOOD.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 2,168 hrs · 1,432 cycles
PTRIM BKP FAIL CAS MESSAGE. REMOVED AND REPLACED THE PITCH TRIM ACTUATOR WITH REPAIRED UNIT. REMOVED SN 0047 AND INSTALLED SN 0038.