N353FX
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.
12 reports on file, 2017-11-13 – 2024-09-24.
Part: FCE — UNSERVICEABLE (ZONE 100) · airframe 10,934 hrs · 7,314 cycles
CREW RECEIVED GND SPOILER FAIL CAS MESSAGE IN FLIGHT. REPLACED FAULTY FCE #2 IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD, NO FURTHER FAULTS NOTED.
Part: GENERATOR — FAILED (RIGHT) · airframe 10,552 hrs · 7,015 cycles
ON DESCENT INTO KPHX AT AROUND 10,000FT, CREW NOTICED A LIGHT WHINING NOISE & FELT VIBRATION IN FLOOR & RUDDER PEDALS. RECEIVED E2 FIRE DET FAIL CAS, BEGAN RUNNING QRH, & 10-15 SECONDS LATER E2 FAIL ILLUMINATED & RT ENGINE FAILED. AN EMERGENCY WAS DECLARED, ENGINE 2 THRUST LEVER WAS SET TO IDLE, & ENGINE 1 USED TO MAINTAIN SPEED. CREW BEGAN THE ENGINE INFLIGHT START PROCEDURE & ADVISED THAT, WHILE THERE WAS FUEL FLOW TO ENGINE, N2 ROTATION TOPPED AT 19.5 WHILE N1 REMAINED CONSTANT THROUGHOUT ENTIRE PROCESS. AT 5,000FT, CREW ABORTED RESTART PROCESS, & SHORTLY RECEIVED ELECTRICAL EMERGENCY CAS. AUTOPILOT DISENGAGED & CONTACT WITH ATC WAS BRIEFLY LOST DUE TO ELECTRICAL ISSUE. CREW BEGAN ELECTRICAL EMERGENCY CHECKLIST & ABLE TO BRING POWER BACK ONLINE. CREW EXITED ELECTRICAL EMERGENCY CHECKLIST 1 MILE FROM RUNWAY & LANDED WITHOUT INCIDENT. FIRE DEPARTMENT CIRCLED AIRCRAFT & STATED THAT FLUID, WHICH WAS LATER IDENTIFIED AS FUEL 7-8 GALLONS OF FUEL, WAS LEAKING FROM ENGINE #2. A SMELL WAS DETECTED COMING FROM ACFT, & CREW RAN EMERGENCY EVACUATION CHECKLIST. ONCE PASSENGERS EVACUATED, CREW TAXIED BACK TO FBO. REPLACED RT ENGINE STARTER GENERATOR IAW AMM 24-31-01. REPLACED STARTER GENERATOR PAD SEAL IAW EMM 72-60-01. REPLACED ALL 3 RT ENGINE ACC DRIVE GEAR SHAFT SEALS IAW EMM 72-60-01. REPLACED RT ENGINE FLOW METER FUEL TUBES IAW EMM 73-10-01. REPLACED #2 ENGINE FMU DUE TO CRACKED & LEAKING FUEL LINE IAW EMM 73-20-01. PERFORMED VISUAL INSPECTION OF RT ENGINE IGNITION EXCITER IAW EMM 74-10-01, NO DEFECTS NOTED. REPLACED SEVERED #2 ENGINE FIRE DETECTION LOOP IAW AMM 26-11-01. OPS & LEAK CHECKED GOOD.
Part: ELECTRONIC UNIT — UNSERVICEABLE (ZONE 100) · airframe 10,153 hrs · 6,746 cycles
WHILE IN CRUISE FLIGHT PTRIM NML FAIL CAS. MESSAGE STAYED ON UNTIL POWER DOWN. REPLACED #2 FCE. COMPLIED W/ RIGGING AND OPS CHECKS, NO DEFECTS NOTED. WORK COMPLETED IAW EMB 505 AMM 27-03-01.
Part: ELEVATOR — FAULT MESSAGE · airframe 9,019 hrs · 5,907 cycles
REPLACED #2 FCE DUE TO REPEAT PITCH TRIM AND SPOILER FAULT CAS MESSAGES IAW PHENOM 300 27-03-01.
Part: SPOILER — FAULT MESSAGE · airframe 8,954 hrs · 5,869 cycles
REPLACED FCE #2 DUE TO GND SPLR FAIL AND SPOILER FAULT ON LANDING. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.
Part: FCU — FAULT MESSAGE · airframe 8,952 hrs · 5,867 cycles
REPLACED #2 FCE DUE TO SWPS FAULT, GND SPL FAIL, PTRIM NML FAIL, SPOILER FAULT AND RED X'S ON SPOILER INDICATOR AND PITCH INDICATOR WHILE TAXING INTO POSITION FOR TAKEOFF AT KMDW. WORK COMPLETED IAW PHENOM 300 AMM 27-30-01.
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 7,523 hrs · 5,072 cycles
DISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND INSTALLED FWD AND AFT EMERGENCY LIGHT POWER SUPPLIES WITH SERVICEABLE, IAW AMM 33-52-01. FUNCTIONAL CHECK GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 6,682 hrs · 4,621 cycles
NOSE LANDING GEAR DISAGREE ON GEAR EXTENTION. RECEIVED THREE GREEN INDICATIONS AFTER RECYCLING THE GEAR AS PER EMERGENCY PROCEDURE. VISUALLY INSPECTED THE NOSE GEAR FOR CONDITION AND SECURITY, NO DEFECTS OR LEAKS NOTED. PERFORMED LUBRICATION OF THE NOSE LANDING GEAR IAW PHENOM 300 AMM 12-21-00. PERFORMED EXTENSION AND RETRACTION FUNCTIONAL CHECK IAW PHENOM 300 MM 32-31-00. OPS CHECK GOOD.
Part: AUTOPILOT SYS — FAILED · airframe 6,595 hrs · 4,561 cycles
PTRIM NML FAIL CAS MESSAGE ILLUMINATED AT CRUISE. AUTOPILOT THEN FAILED - NO CAS SWAPPED FCE 1 AND FCE 2 FOR TROUBLESHOOTING PURPOSES. REPLACED FCE 1 WITH REPAIRED UNIT. ALL WORK PERFORMED IAW EMB 505 AMM 27-03-01 PN 462900-1017 S/N 1038 PN 462900-1017 S/N 0398 (SMN)
Part: ELECTRONIC UNIT — FAILED (NR 1) · airframe 6,481 hrs · 4,482 cycles
#1 FCE FAILED PTRIM BACK UP OPS TEST. REMOVED AND REPLACED #1 FCE, OPERATIONAL CHECK SATISFACTORY.
Part: MODULATING VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 5,644 hrs · 3,857 cycles
ON DESCENT PASSING 1200 (H STAB AND ENGINE HEATS ON) IMC, "DUCT 2 OVERTEMP" CAS MESSAGE ILLUMINATED. AIR CONDITION TO MANUAL - NO EFFECT, ECS KNOB - 1 NO EFFECT, ECS KNOB OFF - VENT CAS MESSAGE WENT OUT. LANDING UNEVENTFUL AFTER SHUT DOWN STRONG BURNING SMELL WAS NOTICEABLE. REMOVED AND REPLACED TEMP MODULATING VALVE NR 2 AND DUCT TEMP SENSOR NR 2 PERFORMED OPS CHKS. OPS CHKS GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION
DUCT NR 2 OVERTEMP CAS MESSAGE DURING CLIMB OUT. DECLARED EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. RESET THE CIRCUIT BREAKER AND COMPLIED WITH AN ELECTRICAL CHECK. NO FAULTS FOUND..