NTSB investigations · 1
Matched to this aircraft by N6604C and the event date: up to this one’s cancellation.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N6604C and the event date: up to this one’s cancellation.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX2682Flux Detector · shortedGYRO CIRCUIT BREAKER TRIPPED 6 MINUTES INTO FLIGHT. CIRCUIT BRAKER WOULD NOT RESET. DISCOVERED THE FLUX DETECTOR P/N FDO103011 HAD SHORTED INTERNALLY CAUSING THE GYRO CIRCUIT BREAKER TO TRIP. FLUX DETECTOR WAS REPLACED. AIRPLANE RETURNED TO SERVICE.SDR 97ZZZX4580Manifold Assy · defectivePILOT REPORTED THE 'HYDRAULIC PRESSURE' LIGHT WOULD NOT EXTINGUISH WHEN THE LANDING GEAR WAS RETRACTED. RED TRANSIT LIGHT EXTINGUISHED. GEAR CYCLED 5 TIMES IN THE AIR WITH NO CHANGE. AIRCRAFT RETURNED TO STATION. AIRCRAFT PLACED ON JACKS. GEAR CYCLED 5 TISDR 97ZZZX1188Elbow · tornPILOT REPORTED THAT THE RIGHT ENGINE WOULD NOT MAINTAIN POWER. MANIFOLD PRESSURE DECREASED DURING FLIGHT. TAKEOFF POWER OKAY ON BOTH ENGINES. DURING CLIMB, THE RIGHT ENGINE ONLY DEVELOPED 27 IN HG. IT WAS DISCOVERED THAT THE INBOARD INDUCTION ELBOW RAM P/NSDR 96ZZZX5443Switch · looseLANDING GEAR FAILED TO RETRACT. AIRCRAFT LANDED WITHOUT INCIDENT. IT WAS DISCOVERED THE WIRING HARNESS HAD TORN LOOSE FROM THE MICROSWITCH. HYD ACTUATOR WAS REPLACED. OPERATIONAL CHECK PERFORMED AND IS OKAY.SDR 96ZZZX2401Connector Plug · pins strippedLEFT ENGINE TACHOMETER FAILED ON TAKEOFF ROLL. PRE-INSPECTION, CONNECTOR PLUG SECURED AND SAFETIED. IT WAS DISCOVERED THE LEFT TACHOMETER GENERATOR ELECTRICAL CONNECTOR PLUG ELECTRICAL PINS HAD STRIPPED. CONNECTOR PLUG REPLACED. AIRCRAFT RETURNED TO SERVICSDR 96ZZZX697Hose · rupturedHOSE ASSEMBLY P/N AE1005816G0166 LOCATED BETWEEN THE RT HYDRAULIC PUMP P/N 9910137-2 AND HYDRAULIC FILTER ASSEMBLY P/N AN6234-2 RUPTURED APPROXIMATELY 3 INCHES FROM THE HYDRAULIC PUMP. IT APPEARED THE TOP ENGINE COWLING HAD CHAFED THROUGH THE FIRE SHIELD AND SDR 95ZZZX3467Shim · deformedNOSE STRUT ASSY FAILED TO EXTEND. STUCK WITH APPROXIMATELY 6 INCHES OF PISTON AREA SHOWING. STRUT ASSY WAS DISASSEMBLED AND INSPECTED FOR DAMAGE. SHIM WAS FOUND DEFORMED. IT IS BELIEVED THE SHIM BECAME WEDGED BETWEEN THE CHROME AREA OF THE PISTON AND BEARI