N367FX
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, 2018-09-01 – 2021-03-04.
Part: VALVE — MALFUNCTIONED · airframe 4,433 hrs · 2,983 cycles
AIR TURN BACK DUE TO BURNING SMELL AND DUCT 1 OVERTEMP CAS MESSAGE ON CLIMB. CREW RAN QRH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT AT KCOS. REPLACED LH TMV IAW EMB 505 AMM 21-61-01. SYSTEM OPS/LEAK CHECK GOOD. P/N OFF/ON: 1300330-11, S/N OFF: 1656, S/N ON: 666.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,008 hrs · 2,757 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. R & R FWD EMERGENCY BATTERY, IAW EMB 505 AMM 33-52-01. OPERATIONS CHECKS GOOD.
Part: LIGHT — MALFUNCTIONED (EMERGENCY) · airframe 3,822 hrs · 2,644 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED THE FWD AND AFT EMERGENCY LIGHT POWER SUPPLIES WITH INSPECTED UNITS. WORK COMPLETED IAW AMM 33-52-01. OPERATIONAL CHECK SATISFACTORY IAW 33-50-00.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,749 hrs · 2,611 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. ACCOMPLISHED REMOVAL AND REPLACEMENT OF FWD AND AFT EMERGENCY LIGHT POWER SUPPLIES. OPS CHECK SATISFACTORY IAW AMM 33-52-00.
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 3,726 hrs · 2,595 cycles
DISCOVERED EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH IN FLIGHT. REMOVED AND REPLACED BOTH FWD AND AFT EMERGENCY BATTERY SUPPLY WITH A MODIFIED BATTERY FOR THE FWD AND TESTED BATTERY PACK FOR THE AFT. OPERATIONS CHECK SATISFACTORY. REFERENCE CHAP 33-52-01. FWD PN 640-13560-00; FWD SN 001950; AFT PN 640-13560-00; S/N 000647.
Part: TRIM SYSTEM — MALFUNCTIONED (TE FLAP)
IN FLIGHT WE HAD SWPS FAULT CAS AND SPOILER FAULT CAS ONLY. ON THE MFD IN YELLOW "X" FLAP POSITION, FLAP INDICATION AND PITCH TRIM FLAPS STAYED AT ZERO AND WOULD NOT EXTEND. PITCH TRIM WORKED/ BACKUP PITCH TRIM DIDN'T WORK. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH FLAP SYSTEM OPERATIONAL CHECK REF AMM 27-50-00-710-801-A OPS CHECK GOOD. PERFORMED HORIZONTAL STAB PITCH TRIM SYSTEM OPS CHECK IAW AMM CH 27-40-00-710-801-A. OPS CHECK GOOD. PERFORMED PUSHER CUTOUT SWITCH OPERATIONAL CHECK IAW AMM CH 27-36-03-710-801-A. OPS CHECK GOOD.
Part: STARTER GEN — MALFUNCTIONED (NR 2 ENGINE) · airframe 2,195 hrs · 1,543 cycles
WHILE INFLIGHT WE FELT A VIBRATION IN THE AIRCRAFT AFTER 10-15 MINUTES RIGHT GENERATOR OFF LINE CAS MESSAGE, FOLLOWING CHECKLIST AND LANDED EYW. MX ASK US TO DO A RESET AND START ENGINES. UNSUCCESSFUL. WHILE INFLIGHT WE FELT A VIBRATION IN THE AIRCRAFT AFTER 10-15 MINUTES RIGHT GENERATOR OFF LINE CAS MESSAGE, FOLLOWING CHECKLIST AND LANDED EYW. MX ASK US TO DO A RESET AND START ENGINES. UNSUCCESSFUL. WHILE INFLIGHT CREW FELT A VIBRATION IN THE AIRCRAFT AFTER 10-15 MINUTES RIGHT GENERATOR OFF LINE CAS MESSAGE, FOLLOW CHECKLIST AND LANDED WITHOUT INCIDENT. R&R NR 2 ENGINE STARTER/GENERATOR AND C/W UNSCHEDULED REMOVAL INSPECTION/PROCEDURE.
Part: STARTER GEN — MALFUNCTIONED (LT ENGINE) · airframe 1,897 hrs · 1,342 cycles
DURING MVF - VIBRATION COMING FROM LEFT ENGINE. HEARD LOW RUMBLE DURING TAKEOFF ROLL. AFTER ROTATION, WE COULD HEAR AND FEEL VIBRATION. WITH CONSTANT AIRSPEED DURING CLIMBOUT / CRUISE FLIGHT, WE MANIPULATED EACH POWER LEVER INDIVIDUALLY - LEFT ENGINE THROTTLE POWER UP / DOWN GREATLY CHANGED VIBRATION. RIGHT THROTTLE - NO CHANGE. REMOVED AND REPLACED NR 1 ENGINE STARTER/GEN AND OPS CHECKED GOOD. IAW AMM 24-31-01. NO DEFECTS NOTED AT THIS TIME.P/N 00SG180Q S/N S00297XL.