N344FX
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, 2016-05-25 – 2025-11-20.
Part: TORQUE TUBE — DAMAGED (RUDDER) · airframe 11,239 hrs · 7,659 cycles
BINDING NOTED ON TWO SEPARATE FULL RIGHT RUDDER FULL RIGHT BRAKE APPLICATIONS. ACCOMPLISHED A GIV OF THE CONTROL PEDALS IAW AMM 27-01-02 AND THE RUDDER FORWARD TORQUE TUBE IAW AMM 27-21-06. FOUND THE TOP BRACKET HOLDING THE CENTER RUDDER FORWARD TORQUE TUBE FLEXING / MOVING WHEN THE RUDDER IS MOVED FULL RIGHT AND FULL LEFT. REPLACED THE MOUNTING HARDWARE TO THE AIRFRAME FROM THE CENTER RUDDER FORWARD TORQUE TUBE TOP BRACKET AND APPLIED TORQUE TO 42 IN-LBS IAW AMM 27-21-05. NO FURTHER DEFECTS NOTED.
Part: FLT CONTROLS — UNSERVICEABLE (ZONE 100) · airframe 10,608 hrs · 7,196 cycles
PTRM NML FAIL CAS MESSAGE RECEIVED DURING AIRCRAFT SETUP. RESET ATTEMPTED WITH NO SUCCESS. REPLACED #2 FLIGHT CONTROL ELECTRONIC IAW EMBRAER 505 AMM 27-03-01. PERFORMED OPS AND RIGGING CHECKS; ALL CHECKS GOOD WITH NO DEFECTS NOTED.
Part: CONTROL UNIT — UNSERVICEABLE (NR 2) · airframe 10,072 hrs · 6,820 cycles
CREW RECEIVED PTRIM NML FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT AFTER STARTUP. REPLACED FCE # 1. REPLACED FCE # 2. RIG COMPLETED WITH NO DEFECTS NOTED. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01/SB505-27-0022.
Part: WIRE HARNESS — FAULTED (NR 2 FIRE DETECT) · airframe 10,057 hrs · 6,808 cycles
DURING CLIMB, THE RED LIGHT ON #2 FIRE SHUTOFF BUTTON WAS ILLUMINATED. CREW CONSULTED QRH AND INSPECTED FOR ANY OTHER INDICATIONS BUT FOUND NO EVIDENCE OTHERWISE THAT THERE WAS ANY FIRE. AIRCRAFT LANDED AT KLUK WITHOUT INCIDENT. REPLACED #2 ENGINE HARNESS IAW EMB PHENOM 300 AMM 71-50-00. NO FURTHER DISCREPANCIES NOTED. OPS CHECK GOOD.
Part: LANDING GEAR — FALSE INDICATION · airframe 8,659 hrs · 5,799 cycles
AT CRUISE ALTITUDE, 43,000FT, LG LEVER DISAG, ADS 2 SLIP FAIL AND ADS 1 SLIP FAIL CAS MESSAGES ILLUMINATED. DURING DESCENT, CREW LEVELED AT 16,000FT, ENTERED A HOLD, AND PERFORMED LG LEVER DISAG QRH CHECKLIST. GEAR WAS CYCLED DOWN-UP-DOWN. NO CHANGE IN THE CAS MESSAGES. AFTER FREE-FALL HANDLE PULLED, NO CHANGE IN MESSAGES. AT THIS TIME, CREW DECLARED AN EMERGENCY AND COMPLETED THE QRH CHECKLIST. AFTER THE TOWER VISUALLY CONFIRMED THAT THE GEAR WAS DOWN, CREW LANDED WITHOUT FURTHER INCIDENT AT KCLT. ACCOMPLISHED GEAR SWINGS AND FREE FALL INSPECTIONâNO DEFECTS FOUND. REPLACED GEAR RELAY K0169. VERIFIED CURRENT INPUT FROM NOSE UPLOCK SENSOR THROUGH RELAY K0169 TO ADS SYSTEM. ACCOMPLISHED ADDITIONAL GEAR SWINGSâNO DEFECTS FOUND. WORK COMPLETED IAW PHENOM 300 AMM 32-31-00.
Part: ACTUATOR — FAILED (PITCH TRIM) · airframe 4,673 hrs · 3,086 cycles
BACKUP PITCH TRIM FAIL CAS MESSAGE IN FLIGHT. INSTALLED A REPAIRED PITCH TRIM ACTUATOR.