N524FX
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, 2006-12-28 – 2019-02-22.
Part: DCPC — MALFUNCTIONED (ELECTRICAL SYS) · airframe 12,714 hrs · 7,757 cycles
DIVERTED DUE TO MULTIPLE OCCURRENCE'S OF "L BAT FAIL, L GEN FAIL" AND/OR "R BAT FAIL, R GEN FAIL" CAS MESSAGES. AIRCRAFT LANDED WITHOUT INCIDENT. R&R LT DCPC WITH A REPAIRED UNIT.
Part: BRACKET — CRACKED (APU FIREWALL) · airframe 12,146 hrs · 7,402 cycles
APU FIREWALL LOWER AND LEFT BRACKETS CRACKED. R & R THE BRACKETS.
Part: CONTROL VALVE — FAILED (BRAKE SYS) · airframe 11,803 hrs · 7,188 cycles
LEFT SIDE BRAKES WOULD ENGAGE ON LANDING BUT THEN STOPPED WORKING FOR 1-2 SECONDS AROUND 60 KTS AND 15-20 KTS. R & R BRAKE CONTROL VALVE. LEAK CHECKED GOOD BUT LH BRAKES STILL FAILED DURING TAXI CHECK. R&R BRAKE CONTROL UNIT WITH MODIFIED UNIT. LEAK CHECKED GOOD. OPS/TAXI CHECKS GOOD.
Part: SAFETY VALVE — MALFUNCTIONED (CABIN PRESSURE)
EXPERIENCED RAPID CABIN DEPRESSURIZATION AT FL430 CABIN ALTITUDE INCREASED AT 10,000+ FEET PER MINUTE. EXECUTED EMERGENCY DESCENT TO 15,000 FT IN LESS THAN 4 MINUTES. AFTER LEVELING AT 15,000 FT CABIN PRESSURE SYSTEM APPEARED TO RETURN TO NORMAL OPERATION AND ALTITUDE SCHEDULE. REPLACED LT AND RT SAFETY VALVES AND SWAPPED IASC NR 1 AND NR 2. OPS CHECK GOOD FOR IASC SWAP AND FOR THE OUTFLOW VALVE.
Part: ELEMENT — OUT OF POSITION (RT BLEED SYSTEM)
RIGHT BLEED LEAK RED CAS POSTED AFTER TAKEOFF. ACFT DIVERTED. REPOSITIONED SENSING ELEMENT AND CLAMPS.
Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 475 hrs · 299 cycles
BIRD STRIKE HIT LT HORZ STAB AND VERTICAL STAB, LEADING EDGE FOR THE LT STAB, LEADING EDGE ACCESS PANEL, UPPER AND LOWER HORSE COLLAR DAMAGED. NO DAMAGE FOUND TO STAB ACTUATOR. FOUND BIRD PARTS INSIDE PANELS.