N50765

Substantial
None

CESSNA 150 S/N: 15069538

Accident Details

Date
Sunday, February 27, 1994
NTSB Number
SEA94LA067
Location
CLARKSTON, WA
Event ID
20001206X00822
Coordinates
46.360401, -117.220870
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE PILOT IN COMMAND'S INADEQUATE USE OF CARBURETOR HEAT. FACTOR(S) WERE: CARBURETOR ICING WEATHER CONDITIONS AND ROUGH TERRAIN.

Aircraft Information

Registration
N50765
Make
CESSNA
Serial Number
15069538
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
150 C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HEDRICK HAL E
Address
318 ELM
Status
Deregistered
City
CLARKSTON
State / Zip Code
WA 99403
Country
United States

Analysis

On February 27, 1994, at approximately 1427 hours Pacific standard time (PST), a Cessna 150, N50765, registered to and being flown by Harold E. Hedrick, a commercially certificated pilot, sustained substantial damage when the aircraft nosed over during a forced landing following a power loss near Clarkston, Washington. The pilot and passenger were uninjured. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was personal in nature, was to have been operated in accordance with the requirements set forth in 14CFR91, and originated from Lewiston, Idaho, at approximately 1345 hours.

The pilot reported that after several touch and go landings, he departed the pattern westbound. Shortly thereafter the engine began "sputtering" and he was unable to maintain altitude. He executed a forced landing to a plowed field landing approximately 60 degrees to the furrows (refer to photograph 01). During the rollout the nose wheel collapsed and the aircraft nosed over. The elevation of the accident site was approximately 450 feet above sea level (refer to CHART I).

The pilot report that the aircraft had a total of 20 gallons of automotive fuel aboard when it took off from the Lewiston Airport.

The pilot was interviewed by telephone by the Investigator in Charge and reported that he applied carburetor heat, observed no change in engine performance, and returned the carburetor heat to the cold position.

The aircraft was transported to the facilities of Gustin Aviation at the Lewiston Airport, Lewiston, Idaho, following the accident. Mr. Ron Gustin examined the engine at that time and found no evidence of any mechanical malfunction.

Selected meteorological observing system (AMOS) reports taken at the Lewiston airport (elevation: 1,438 feet above sea level) on the afternoon of the accident were recorded as follows:

1349 hours: ceiling measured 1,100' broken; 2,100' overcast 10 miles visibility in light drizzle; temperature 40 deg F., dew point 34 deg. F.; winds 140 deg. (true) at 5 knots; altimeter 30.07 inches of Hg.

1409 hours: sky condition 1,000' scattered, ceiling measured 1,700' broken, 5,000' overcast; 10 miles visibility; temperature 40 deg F., dew point 33 deg. F.; winds 160 deg. (true) at 5 knots; altimeter 30.07 inches of Hg. remarks: drizzle ended at 1405 hours

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA067