N245FX

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

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.

3 reports on file, 2004-03-31 – 2005-07-15.

FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2005-07-15 Matched by certificate designator
ATA 2916

Part: CHECK VALVE — LEAKING (HYD RESERVOIR) · airframe 4,891 hrs · 3,488 cycles

AFTER TAKEOFF CREW NOTED VISIBLE FUMES AND A HYDRAULIC SMELL IN THE COCKPIT. RETURNED AIRCRAFT TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE FOUND HYDRAULIC FLUID IN A PNUEMATIC DUCT AND DEBRIS UNDER THE SEAT OF THE HYDRAULIC RESERVOIR CHECK VALVE. CLEANED VALVE AND ALL ASSOCIATED DUCTS. OPS CHECK PERFORMED WITH NO DEFECTS NOTED.

Source: SDR 6018207152005
WARNING INDICATION; FLUID LOSS; AFFECT SYSTEMS · 2004-10-25 Matched by certificate designator
ATA 3231

Part: WASHER — CRUSHED (SHUTTLE VALVE) · airframe 4,179 hrs · 3,010 cycles

"LOW HYD PRESS" WARNING MSG ILLUMINATED IN FLIGHT JUST AFTER TAKEOFF (FROM DEN) FOR BOTH 1/2 SYSTEMS. CREW DIVERTED TO ICT FOR RUNWAY LENGTH AND MX AVAILABILITY. EMERGENCY DECLARED AND PROCEDURES FOLLOWED FOR EMERGENCY GEAR EXTENSION AND BRAKE ACTIVATION. ON ROLLOUT, NR 1 AND NR 2 MAIN TIRES BLEW OUT. SUBSEQUENTLY FOUND NR 3 MAIN DEFLATED. A CRUSH WASHER P/N: AN901-4A ON THE LEFT HAND MAIN LANDING GEAR INBOARD DOOR ACTUATOR SHUTTLE VALVE WAS DISCOVERED TO BE BLOWN OUT. PICTURES OF THE WASHER HAVE BEEN REQUESTED. NO SIGNS OF METAL CONTAMINATION ARE PRESENT IN THE HYDRAULIC FLUID. TWO PUMPS HAVE BEEN PLACED ON ORDER, ALONG WITH NEW FILTERS. NO EVIDENCE OF METAL CONTAMINATION IN THE FILTERS.

Source: SDR 60182102504
WARNING INDICATION · 2004-03-31 Matched by certificate designator
ATA 3241

Part: CONTROL BOX — FAILED (ANTI SKID SYS) · airframe 3,630 hrs · 2,609 cycles

ON TAKE-OFF ROLL, ALL 4 ANTI-SKID LIGHTS ILLUMINATED. TAKE-OFF WAS ABORTED. AS AIRCRAFT SLOWED, LIGHTS EXTINGUISHED ONE BY ONE. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE

Source: SDR 6018203312004