N8226P
We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.
Safety history
- November 28, 1988Accident
WHILE IN CRUISE FLT NEAR AN ARPT, THE PROP SEPARATED. PLT WAS GIVEN VECTORS TO ARPT & ENTERED PATTERN FOR LNDG. DOWNWIND LEG WAS EXTENDED DUE TO STRONG TAILWIND. STRONG HEADWIND ON FINAL CAUSED ACFT TO LAND SHORT. DURING LANDING ROLL ACFT COLLIDED WITH TWO FENCES. EXAMINATION OF ACFT REVEALED 6 PROP MOUNT BOLTS FAILED DUE TO FATIGUE AS A RESULT OF IMPROPER PLACEMENT OF PROP MOUNTING SHIM BETWEEN ENGINE CRANKSHAFT FLANGE AND STARTER GEAR FLANGE. ACFT MANUAL STATED PROP MOUNT BOLTS MAY FAIL DUE TO
- June 16, 1988Accident
UPON RETURN FROM A LOCAL AERIAL PHOTOGRAPHY FLIGHT, THE PILOT FAILED TO ENSURE THAT THE AIRCRAFT LANDING GEAR WAS EXTENDED, DOWN AND LOCKED. WHEN THE AIRCRAFT TOUCHED DOWN, THE GEAR WAS ONLY EXTENDED APPROXIMATELY 10%; IT COLLAPSED FULLY WHEN IT CONTACTED THE GROUND AND THE AIRCRAFT SLID TO A STOP ON ITS BELLY. THE PAX STATED THAT HE THOUGHT THE GEAR WAS STILL IN THE UP POSITION ON SHORT FINAL AND THE PILOT LOWERED THE GEAR HANDLE ONLY WHEN THE PAX QUERIED HIM. POST-ACCIDENT GEAR ACTUATION REVE
- March 2, 1969Accident
Improper Maintenance (Owner Personnel); Braking System (Normal System); Pressure,None