N406FX
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.
9 reports on file, 2002-02-18 – 2022-09-06.
Part: GENERATOR — FAULTED (NR 1) · airframe 6,074 hrs · 3,874 cycles
DIVERTED DUE TO AMBER BATT 1 DISCHARGING CAS FOLLOWED BY A GEN 1 OFF BUS. ELECTRICAL SYNOPTIC PAGE SHOWED GEN 1 OFF AND BOTH SHED BUSSES OFF, WITH GEN 2 POWERING THE SYSTEM. AIRCRAFT LANDED WITHOUT INCIDENT AT KCHS. WHILE TAXIING IN, ENG 1 OIL CHIP DETECT CAS MESSAGE ILLUMINATED. INSPECTED GEARBOX. REPLACED #1 GENERATOR. OPS AND LEAK CHECK NORMAL. ALL WORK PERFORMED IAW EMB 545 AMM 24-31-01 AND HONEYWELL AS907-3-1E LMM 72-61-01.
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 4,041 hrs · 2,618 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED AFT NR 2 EMERGENCY LIGHT POWER SUPPLY. OPERATIONS CHECK GOOD, IAW AMM 33-51-00. P/N 6450LS-00 S/N 001360.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 3,902 hrs · 2,530 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY WITH TESTED UNIT. OPS CHECK GOOD, IAW LEGACY 450 AMM 33-51-01. P/N 6450LS-00; S/N 001734.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 3,629 hrs · 2,368 cycles
DURING ROUTINE MAINTENANCE, DISCOVERED EMERGENCY LIGHT NOT ARMED AMBER CAS DISPLAYS WHEN EMERGENCY LIGHT SWITCH IS IN THE ARMED POSITION. REPLACED BOTH EMERGENCY LIGHT POWER SUPPLIES WITH INSPECTED UNITS. OPS CHECK GOOD. NR 1 PN ON: 6450LS-00; SN ON: 001040. NR 2 PN ON: 6450LS-00; SN ON: 002187.
Part: FAIRING — ERODED (VERTICAL STAB) · airframe 2,233 hrs · 1,481 cycles
V-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. REMOVED AND REPLACED VERT STAB AFT UPPER FAIRING REF AMM 55-32-31. DUE TO WATER INTRUSION. AFT RED BEACON WAS ALSO REPLACED REF.
Part: FAIRING — DAMAGED (VERTICAL STAB)
V-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.
Part: RELAY — FAILED (ANTI ICE SYS) · airframe 4,362 hrs · 3,390 cycles
RED CAS STAB OVERHEAT, BURNING SMELL IN CABIN. CREW ADVISED THE RED (STAB OVHT) CAS MESSAGE ILLUMINATED WITH CWP AND TRIPLE CHIME DURING CLIMB THROUGH FL 30.0. THE THRUST LEVERS WERE JUST BELOW MCR, 82% N1 AND -29 TEMP. CREW SELECTED ANTIICE *OFF* AND PULLED POWER BACK. THE CAS MESSAGE EXTINGUISHED. CREW SELECTED ANTI-ICE BACK *ON* 2 MINUTES LATER AND CAS MESSAGE DID NOT RETURN. PER FSR RECOMMENDATIONS AND T/S, REPLACED THE P-40 RELAY PANEL. OPS CHECKS PERFORMED, NO DEFECTS NOTED.
Part: VALVE — FAULTY (NLG) · airframe 3,910 hrs · 2,928 cycles
NOSE GEAR REMAINED UP ON FIRST 4 CYCLES OF THE GEAR HANDLE THEN LOWERED NORMALLY ON 5TH ATTEMPT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL VALVE. OPS CHECK NORMAL. NO DEFECTS NOTED AND NO RE-OCCURRENCE
Part: SQUAT SWITCH — MISSING (RT MLG)
DURING OUT GOING INSPECTION FOUND ONE SET SCREW MISSING AND ONE SET SCREW LOOSE ON RIGHT MAIN LANDING GER OUT BOARD SQUAT SWITCH SWING ARM. PROBABLE CAUSE: THE SCREWS VIBRATED LOOSE. RECOMMEND THAT AN INSPECTION FOR LANDING GEAR SQUAT SWITCH BE ADDED TO THE 300 HOUR INSPECTION; ALSO A STEP BE ADDED TO MM TO APPLY LOCTITE TO THE TWO SET SCREWS DURING INSTALLATION.