20100823044079A

Accident · Substantial damage

FAA accident report · Cessna 182A · Ojai, CA · August 23, 2010

Date
August 23, 2010 · 17:12 local
Place
Ojai, CA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3850D
NTSB investigation
NTSBWPR10FA423
Reported as
Cessna 182A
Reported engine
Continental O-470 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
2,800 total500 in this make and model100 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The aircraft was in cruise flight at 7500 ft MSL. The aircraft experienced a complete and sudden engine failure. The pilot attempted to restart the engine by cycling throttle, mixture, and ignition controls. The pilot did not cycle the carburetor heat control. The pilot switched fuel valve from both to left and the right. The engine did not regain power. The pilot selected a golf course as the site to perform an emergency landing .during touchdown the aircraft's right wing collided with a tree/bush. The aircraft received substantial damage. The right wing was partially separated at the wing root and the empennage section had separated from the fuselage at the baggage door. The left main gear separated from the fuselage. The aircraft came to rest in an upright, left wing low attitude. The pilot received minor injuries. The following day, the aircraft retrieval crew drained approximately eight gallons of fuel from the left fuel tank. The right tank had only a residual amount of fuel. There was no evidence of a fuel spill at the accident site.

As the FAA filed it

THE AIRCRAFT WAS IN CRUISE FLIGHT AT 7500 FT MSL. THE AIRCRAFT EXPERIENCED A COMPLETE AND SUDDEN ENGINE FAILURE. THE PILOT ATTEMPTED TO RESTART THE ENGINE BY CYCLING THROTTLE, MIXTURE, AND IGNITION CONTROLS. THE PILOT DID NOT CYCLE THE CARBURETOR HEAT CONTROL. THE PILOT SWITCHED FUEL VALVE FROM BOTH TO LEFT AND THE RIGHT. THE ENGINE DID NOT REGAIN POWER. THE PILOT SELECTED A GOLF COURSE AS THE SITE TO PERFORM AN EMERGENCY LANDING .DURING TOUCHDOWN THE AIRCRAFT'S RIGHT WING COLLIDED WITH A TREE/BUSH. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE. THE RIGHT WING WAS PARTIALLY SEPARATED AT THE WING ROOT AND THE EMPENNAGE SECTION HAD SEPARATED FROM THE FUSELAGE AT THE BAGGAGE DOOR. THE LEFT MAIN GEAR SEPARATED FROM THE FUSELAGE. THE AIRCRAFT CAME TO REST IN AN UPRIGHT, LEFT WING LOW ATTITUDE. THE PILOT RECEIVED MINOR INJURIES. THE FOLLOWING DAY, THE AIRCRAFT RETRIEVAL CREW DRAINED APPROXIMATELY EIGHT GALLONS OF FUEL FROM THE LEFT FUEL TANK. THE RIGHT TANK HAD ONLY A RESIDUAL AMOUNT OF FUEL. THERE WAS NO EVIDENCE OF A FUEL SPILL AT THE ACCIDENT SITE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.