N351FX
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
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED THE NR 1 AND NR 2 EMERGENCY BATTERIES AND INSTALLED INSPECTED UNITS. OPERATIONS TEST GOOD. WORK PERFORMED IAW EMB-505 AMM 33-52-01.
DIVERTED DUE TO ELECTRICAL EMERGENCY CAS WHILE FLYING AT FL430 IN CRUISE. CREW LOST POWER, UNDERTOOK AN EMERGENCY DESCENT, AND OXYGEN MASKS DEPLOYED. GENERATORS WERE RESET UPON REACHING 10,000 FEET; #2 GEN AND AHARS DID NOT RESET (ALL OTHER SYSTEMS OPERATIONAL). AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 AND 2 ENGINE STARTER/GENERATORS ALONG WITH NR 1 AND 2 GCUS. OPS CHECKED GOOD.
AIR TURN BACK DUE TO FUEL 1 FEED FAULT. MOTIVE FLOW PUMP 1 RED X DISPLAY. AIRCRAFT LANDED WITHOUT INCIDENT.REPLACED LH WING ENGINE FEED CHECK VALVE. REPLACED LH FUEL TANK VENT TUBE DRAIN VALVE FOUND BROKEN OFF IN FUEL TANK. PERFORMED HIGH POWER ENGINE RUN AND MOTIVE FLOW NO LONGER DISPLAYS RED X . OPS CHECK AND LEAK CHECK GOOD.
FLAP FAIL, SPWS FAULT, SPOILER FAULT. PERFORMED CMC DOWNLOAD FINDING FAULT CODE27522041 AND 27020141. COMPLIED WITH FIM TASK 27-53-00-810-808 FINDING CONDITION TO BE TRANSITORY. PER CUSTOMER REQUEST SWAPPED FCE 1 AND FCE 2 IAW AMM 27-03-01. PERFORMED FLAP SYSTEM RIGGING AND MULTIFUNCTION SPOILER SYSTEM RIGGING IAW AMM 27-50-00 AND 27-62-00. PERFORMED OPS CHECK OF FLAP SPOILER AND HS PITCH TRIM SYSTEM IAW AMM 27-50-00, 27-60-00 AND 27-40-00 WITH NO DEFECTS. SYSTEM OPS CHECK GOOD AT THIS TIME P/N 4629.
BACKUP PITCH TRIM FAIL CAS MESSAGE ON PDFS. POWERED AIRCRAFT DOWN AND BACKUP, MESSAGE STILL THERE ON PDFS. REMOVED AND REPLACED #1 FCE AND ACCOMPLISHED ELECTRONIC RIGGING PROCEDURE. ACCOMPLISHED IAW PHENOM 300 AMM 27-03-00. OPS CHECKS GOOD IAW PHENOM 300 AMM 27-03-00. PN OFF AND ON: 462900-1017 SN OFF: 0779 SN ON: 0414Â Â TSN: 467.3 CSN: 308
GND SPLR FAIL CAS MESSAGE IN FLIGHT. REMOVED AND REPLACED FCE 2 UNIT AND PERFORMED SATISFACTORY RIGGING/OPERATIONAL TEST OF THE SPOILER SYSTEM PER EMB 505 AMM 27-03-01 P/N 462900-1017 S/N 0938
DIVERTED DUE TO VIBRATION GEN NR 1 FAIL CAS MSG APPEARED SHORTLY AFTER. CREW RAN CHECKLIST. VIBRATION WENT AWAY WITH REDUCED POWER BUT GEN WOULD NOT RESET. AIRCRAFT LANDED WITHOUT INCIDENT. R&R NR 1 GEN, STARTER PAD SEAL MAGNETIC SEAL, ACCESSORY DRIVE GEARSHIFT SEAL, AND INLET FUEL PRESSURE TUBE. OPS AND LEAK CHECK GOOD.
PITCH TRIM NORMAL FAIL CAS MESSAGE AT HIGH ALTITUDE. WHEN BACKUP TRIM ENGAGED PTRM BKP FAIL CAS MESSAGE. TRIM FULL DOWN AT 14.1. REPLACED THE PITCH TRIM ACTUATOR. OPS CHECKED GOOD. R & R TELESCOPING DUCT O-RING SEALS. LEAK CHECKED GOOD.
PITCH TRIM NORMAL FAIL, CAS MESSAGE ILLUMINATED ON CLIMB PASSING 16,000FT. REPLACED THE STAB TRIM ACTUATOR WITH REPAIRED UNIT. REPLACED FCE NR 2 WITH MODIFIED UNIT. OPS CHECKED GOOD AND NO DEFECTS NOTED.
PASSING FLIGHT LEVEL 390, PTRIM NML FAIL, CAS MESSAGE ILLUMINATED AND REMAINED ON FOR REMAINDER OF FLIGHT. OPS CHECK GOOD AT THIS TIME.
PITCH TRIM NEUTRAL FAIL CASS MESSAGE COMES ON IN DESCENTS (BETWEEN SETTINGS OF 13.5 -13,9 ). REMOVED AND REPLACED PITCH TRIM ACTUATOR ON 467500-1003. REMOVED SN 0141 AND INSTALLED SN 0058. ACCOMPLISHED HORIZONTAL STABILIZER ELECTRICAL STOP-FUNCTIONAL CHECK, CHECKS GOOD.