N664CW
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, 2005-06-19 – 2009-01-27.
Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 13,706 hrs · 8,227 cycles
DURING CRUISE, CREW NOTED WHISTILING SOUNDS FROM THE LT WINDSCREEN. AFTER A BRIEF INSP, CREW NOTED (2) VERTICAL CRACKS SPANNING THE WINDSCREEN. AS THE ACFT BEGAN THE INITIAL DESCENT, THE CREW WITNESSED THE OUTER PLY OF THE WINDSCREEN DEPART THE ACFT. THE CREW REPORTED THAT THERE WAS NO INDICATION THAT THE DEBRIS CONTACTED THE ACFT OR POWERPLANT. ACFT LANDED SAFELY AT ITS DESTINATION. MX CONFIRMED THE MISSING OUTER PLY OF THE WINDSCREEN. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.
Part: HEAT TAPE — BURNED · airframe 13,635 hrs · 8,175 cycles
WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. OPEN (A)
Part: UNKNOWN — SMOKE (COCKPIT)
WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. (SDR WILL BE COMPLETED AFTER MAINTENANCE/ INSPECTION IS COMPLETE). (K)
Part: ADG — BURNED (GENERATOR) · airframe 13,262 hrs · 7,941 cycles
DURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL BLACKOUT. ENGINE DRIVEN SYSTEM WAS BROUGHT BACK ON-LINE AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND ADG FAILED INTERNALLY. THE ADG WAS REPLACED.
Part: BULKHEAD — CRACKED (BS 409) · airframe 12,473 hrs · 7,451 cycles
DURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AIRWORTHINESS DIRECTIVE 97-24-02, SERVICE BULLETIN 601-0501. THE CRACK IS LOCATED AT THE CORNER OF THE KEEL BEAM LINK CUTOUT ANGLE, EXTENDING UP TO THE LEFT SIDE CORNER OF THE CUTOUT.
Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 11,981 hrs · 7,164 cycles
THE CREW REPORTED THAT DURING A NORMAL GEAR EXTENSION, THE NOSE WHEEL WOULD NOT EXTEND. THE LANDING GEAR WAS CYCLED TWICE, AND THE NOSE GEAR REMAINED RETRACTED. A MANUAL EXTENSION WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS WERE GOOD. EXTENSION AND RETRACTION CHECKS WERE PERFORMED WITH NO NOTED DEFECTS. THE AIRCRAFT WAS RETURNED TO SERVICE.