N843CW
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, 2003-12-08 – 2008-05-29.
Part: CONTROL VALVE — MALFUNCTIONED (BRAKE ASSY) · airframe 6,912 hrs · 4,513 cycles
AFTER LANDING THE CREW REPORTED THE BRAKES WERE MUSHY AND COULD ONLY ACHIEVE 200-300 PSI WITH BRAKES FULLY DEPRESSED. THE CREW WAS ABLE TO PUMP THE BRAKES UP AFTER ENGINE SHUT DOWN. MAINTENANCE GAINED ACCESS TO THE BRAKE CONTROL VALVE AND BLED THE PILOT AND COPILOT MASTER CYLINDERS. MX DID FIND AIR IN THE SYSTEM. THEY PERFORMED A GOOD OPS AND TAXI CHECK.
Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 5,828 hrs · 3,754 cycles
WHILE TROUBLESHOOTING A NOSE STEERING PROBLEM, MAINTENANCE FOUND THE LT NOSE GEAR DOOR FRAME CRACKED BEYOND THE LIMITS ACCEPTABLE IAW THE SRM. THE CRACK WAS APPROXIMATELY .5 INCHES IN LENGTH. MAINTENANCE PERFOMRED A REPAIR FROM ENGINEERING IAW EO 4731-187607 REV NC AS APPROVED ON 8110-3 DATE 29 JAN 2007.
Part: FLOOR SKIN — DAMAGED (COCKPIT) · airframe 5,319 hrs · 3,415 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING B, C AND D LEVEL INSPECTIONS A CRACK WAS DISCOVERED IN THE STRUCTURAL WEB BENEATH THE CO-PILOTS SEAT. THE DAMAGED WEB WAS REPAIRED IAW RAYTHEON FIELD REPAIR FR-HK-02956 REVISION 1 BY INSTALLING A REPAIR ANGLE TO THE OUTBOARD SEAT RAIL WEB.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 5,319 hrs · 3,415 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING B, C, AND D INSPECTIONS A CRACK WAS DISCOVERED IN THE CAPTAINS OUTBOARD SEAT TRACK. THE PILOTS OUTBOARD SEAT TRACK WAS REPLACED IN ACCORDANCE WITH THE HAWKER 800XP STRUCTURAL REPAIR MANUAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: STARTER GEN — FAILED (NR 2 ENGINE) · airframe 2,509 hrs · 1,600 cycles
AIRCRAFT DESCENDING THROUGH 11,000 FT, VIBRATION WAS NOTED. ENGINE NR 2 WAS SHUT DOWN AND VIBRATION WENT AWAY. AIRCRAFT LANDED AND IT WAS FOUND THAT THE STARTER GENERATOR BEARINGS HAD FAILED.
Part: BEARING — FAILED (STARTER GEN) · airframe 2,509 hrs · 1,600 cycles
AIRCRAFT DESCENDING THROUGH 11,000 FT, VIBRATION WAS NOTED. ENGINE NR 2 WAS SHUT DOWN AND VIBRATION WENT AWAY. AIRCRAFT LANDED AND IT WAS FOUND THAT THE STARTER GENERATOR BEARINGS HAD FAILED.