N466CW
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.
5 reports on file, 2006-08-02 – 2008-10-07.
Part: MOTOR — INOPERATIVE (COMPRESSOR)
DURING FLIGHT, AIR CONDITIONING CIRCUIT BREAKER POPPED; CREW NOTED A BURNING ODOR. AIRCRAFT LANDED SAFELY. MX FOUND THE COMPRESSOR MOTOR FIALED. THE MOTOR WAS REPLACED.
Part: RIB — CRACKED (HORIZONTAL STAB)
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIB ASSEMBLIES WITH IMPROVED ASSEMBILES.
Part: GPU — SMOKE · airframe 2,656 hrs · 2,367 cycles
CREW REPORTS THAT THE GPU- (GROUND POWER UNIT) CAUSED ELECTRICAL SMOKE INSIDE TAIL CONE. ONCE GPU WAS DISCONNECTED SMOKE DISSIPATED. NO EVIDENCE OF FIRE HAS BEEN DISCOVERED.
Part: RIB — CRACKED (HORIZ STAB) · airframe 2,524 hrs · 2,254 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RIGHT INBOARD HORIZONTAL STABILIZER NOSE RIB STRUCTURE (PART NUMBER 45A21085-004) WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. THE HORIZONTAL STABILIZER WAS REMOVED TO ACCESS THE RIB. THE FORWARD RIB ASSEMBLY ON THE RIGHT HORIZONTAL STABILIZER WAS REPLACED IN ACCORDANCE WITH THE HAWKER 400XP STRUCTURAL REPAIR MANUAL, AND THE HORIZONTAL STABILIZER WAS REINSTALLED. OPERATIONAL CHECKS OF THE HORIZONTAL STABILIZER WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: WIRE HARNESS — FALSE ACTIVATION (RT ENGINE) · airframe 2,417 hrs · 2,153 cycles
KAPA - KAPA, WHILE IN CRUISE FLIGHT AT 34,000 FT THE RT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. AFTER THE CREW PUSHED THE EMERGENCY STOW BUTTON, THE LIGHT REMAINED ILLUMINATED. WHILE DESCENDING FROM 29,000 FT TO RETURN TO KAPA, A "POP" SOUND WAS HEARD AND WAS FELT IN THE POWER LEVERS. THE THRUST REVERSER DEPLOY LIGHT EXTINGUISHED AND AN UNEVENTFUL LANDING WAS MADE IN KAPA. MAINTENANCE REPLACED THE WIRING HARNESS ON BOTH LEFT AND RIGHT THRUST REVERSERS IN ACCORDANCE WITH NORDAM GROUP SERVICE BULLETIN BJ400 78-3. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.