19970926029159A

Accident · Substantial damage

FAA accident report · Cessna P210N · Creswell, OR · September 26, 1997

Date
September 26, 1997 · 12:45 local
Place
Creswell, OR
Airport
Hobby Field Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6394W
NTSB investigation
NTSBSEA97LA216
Reported as
Cessna P210N
Reported engine
Continental TSIO520AF
Fatal injuries
0
Pilot’s flight hours
894 total92 in this make and model39 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.

Lost power enroute. Flipped over landing fuel selector on empty tank. Fuel in other. (.4)the pilot reported that shortly after takeoff he moved the fuel selector from 'both' to 'right' and did not subsequently reposition it from 'right', resulting in fuel starvation as the aircraft cruised at 16,000 feet about 3 hours after takeoff. The pilot declared an emergency with air traffic control (ATC) and was directed to a nearby airport where he attempted a forced landing; however, he was not successful in reaching the airport runway. In the ensuing forced landing, the airplane struck a ditch and flipped over, coming to rest in a field near the runway. Post-accident examination found 35 gallons of fuel in the left tank, no fuel in the right tank, and the fuel selector positioned to 'right.' Pilot's operating handbook (POH) data indicate the airplane takes approximately 15 minutes to descend from 16,000 feet to the emergency airport elevation (535 feet above mean sea level) in a descent at best glide speed (approximately 85 knots indicated airspeed) with propeller windmilling and flaps and gear up. The POH 'engine failur e in flight' procedure directs the pilot to check fuel quantity and place the fuel selector on the fulledt tank.

As the FAA filed it

LOST POWER ENROUTE. FLIPPED OVER LANDING FUEL SELECTOR ON EMPTY TANK. FUEL IN OTHER. (.4)THE PILOT REPORTED THAT SHORTLY AFTER TAKEOFF HE MOVED THE FUEL SELECTOR FROM 'BOTH' TO 'RIGHT' AND DID NOT SUBSEQUENTLY REPOSITION IT FROM 'RIGHT', RESULTING IN FUEL STARVATION AS THE AIRCRAFT CRUISED AT 16,000 FEET ABOUT 3 HOURS AFTER TAKEOFF. THE PILOT DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL (ATC) AND WAS DIRECTED TO A NEARBY AIRPORT WHERE HE ATTEMPTED A FORCED LANDING; HOWEVER, HE WAS NOT SUCCESSFUL IN REACHING THE AIRPORT RUNWAY. IN THE ENSUING FORCED LANDING, THE AIRPLANE STRUCK A DITCH AND FLIPPED OVER, COMING TO REST IN A FIELD NEAR THE RUNWAY. POST-ACCIDENT EXAMINATION FOUND 35 GALLONS OF FUEL IN THE LEFT TANK, NO FUEL IN THE RIGHT TANK, AND THE FUEL SELECTOR POSITIONED TO 'RIGHT.' PILOT'S OPERATING HANDBOOK (POH) DATA INDICATE THE AIRPLANE TAKES APPROXIMATELY 15 MINUTES TO DESCEND FROM 16,000 FEET TO THE EMERGENCY AIRPORT ELEVATION (535 FEET ABOVE MEAN SEA LEVEL) IN A DESCENT AT BEST GLIDE SPEED (APPROXIMATELY 85 KNOTS INDICATED AIRSPEED) WITH PROPELLER WINDMILLING AND FLAPS AND GEAR UP. THE POH 'ENGINE FAILUR E IN FLIGHT' PROCEDURE DIRECTS THE PILOT TO CHECK FUEL QUANTITY AND PLACE THE FUEL SELECTOR ON THE FULLEDT TANK.

NTSB investigation

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