N904FX
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.
6 reports on file, 2006-10-04 – 2007-03-22.
Part: GOVERNOR — INTERMITTENT (NR 2 ENGINE) · airframe 22,378 hrs · 28,658 cycles
NR 2 ENGINE SURGE DURING CLIMB.
Part: JAM-NUT — LOOSE (HYDRAULIC SYS) · airframe 22,327 hrs · 24,614 cycles
ON DEPARTURE FROM MEM THE GREEN SYSTEM HYD LOW LEVEL LIGHT ILLUMINATED. THE PIC DECLARED AN EMERGENCY AND RETURNED TO MEM. A JAM NUT FOR THE O-RING ON A TEE FITTING COMING OUT OF THE MAIN HYD SYSTEM ACCUMULATOR WAS TIGHTENED AND LEAK CHECKED WITH NO LEAKS FOUND AND THE A/C RETURNED TO SERVICE.
Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 22,323 hrs · 28,610 cycles
DURING DEPARTURE, THE GREEN HYDRAULIC SYSTEM LIGHT ILLUMINATED.
Part: WIRE — OUT OF POSITION (FEATHER SOLENOID) · airframe 22,294 hrs · 28,587 cycles
DURING DESCENT INTO DHN THE NR 2 ENGINE BEGAN SURGEING (PROP CHANGEING PITCH). WIRE NR 101 WAS FOUND NEARLY SEPARATED FROM IT'S PIN IN THE CONNECTOR TO THE RIGHT FEATHER SOLENOID.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,265 hrs · 28,563 cycles
CORROSION FOUND ON FRAME 13 AT STRINGER 17 RT BEYOND SRM ALLOWABLE LIMITS.
Part: SEAL — DETERIORATED (NR 2 ENGINE) · airframe 22,163 hrs · 28,475 cycles
CCAS ENGINE 2 OIL AND LOW ENGINE OIL PRESSURE DETECTED ON NR 2 ENGINE.