20070528013819A

Accident · Destroyed

FAA accident report · Cessna A185F · Wilbur, WA · May 28, 2007

Date
May 28, 2007 · 15:15 local
Place
Wilbur, WA
Airport
Gollehon
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9434N
NTSB investigation
NTSBSEA07FA134
Reported as
Cessna A185F
Reported engine
Continental IO520D
People aboard
1
Fatal injuries
1
Pilot’s flight hours
16,400 total0 in this make and model8 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.

(-23) Airman departed to the east from personal airstrip, according to his spouse, between 1500 and 1530. Aircraft is subsequently discovered 1/4 mile north of the departure end of the runway. The left wing struck the ground first, with the aircraft then cartwheeling into the nose section, and then coming to rest laying on the right side. Aircraft came to rest approximately 45 feet from initial wing strike. Wheat at the crash site was between 2 and 3 feet high. No wheat was disturbed on either side of the left wing entry path--suggest bank angle of at least 80 degrees. Flaps were found in the 3rd notch position, and witness marks on the fuselage confirm this selection. Throttle, prop, and mixture were all found full forward. No appreciable fuel was found in either wing tank. Fuel odor was noted in soil below right tank. Fuel selector found in "both" position. Ultimate fuel kill area measured approximately 3' by 6'. Fueling records compared with flight records indicate that the aircraft experienced only 1.7 flight hours against full fuel tanks prior to the accident. Amended narrative likely to follow. (-23 amendment) airman is believed to have been under additional stress prior to the flight.

As the FAA filed it

(-23) AIRMAN DEPARTED TO THE EAST FROM PERSONAL AIRSTRIP, ACCORDING TO HIS SPOUSE, BETWEEN 1500 AND 1530. AIRCRAFT IS SUBSEQUENTLY DISCOVERED 1/4 MILE NORTH OF THE DEPARTURE END OF THE RUNWAY. THE LEFT WING STRUCK THE GROUND FIRST, WITH THE AIRCRAFT THEN CARTWHEELING INTO THE NOSE SECTION, AND THEN COMING TO REST LAYING ON THE RIGHT SIDE. AIRCRAFT CAME TO REST APPROXIMATELY 45 FEET FROM INITIAL WING STRIKE. WHEAT AT THE CRASH SITE WAS BETWEEN 2 AND 3 FEET HIGH. NO WHEAT WAS DISTURBED ON EITHER SIDE OF THE LEFT WING ENTRY PATH--SUGGEST BANK ANGLE OF AT LEAST 80 DEGREES. FLAPS WERE FOUND IN THE 3RD NOTCH POSITION, AND WITNESS MARKS ON THE FUSELAGE CONFIRM THIS SELECTION. THROTTLE, PROP, AND MIXTURE WERE ALL FOUND FULL FORWARD. NO APPRECIABLE FUEL WAS FOUND IN EITHER WING TANK. FUEL ODOR WAS NOTED IN SOIL BELOW RIGHT TANK. FUEL SELECTOR FOUND IN "BOTH" POSITION. ULTIMATE FUEL KILL AREA MEASURED APPROXIMATELY 3' BY 6'. FUELING RECORDS COMPARED WITH FLIGHT RECORDS INDICATE THAT THE AIRCRAFT EXPERIENCED ONLY 1.7 FLIGHT HOURS AGAINST FULL FUEL TANKS PRIOR TO THE ACCIDENT. AMENDED NARRATIVE LIKELY TO FOLLOW. (-23 AMENDMENT) AIRMAN IS BELIEVED TO HAVE BEEN UNDER ADDITIONAL STRESS PRIOR TO THE FLIGHT.

NTSB investigation

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

Other reports on N9434N · 1

Matched to the same aircraft by N-number and date.