N5366M

Substantial
None

CESSNA 152 S/N: 15284566

Accident Details

Date
Tuesday, December 12, 1995
NTSB Number
SEA96LA028
Location
CHIMACUM, WA
Event ID
20001207X05081
Coordinates
47.970218, -122.779693
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 delayed application of carburetor heat which resulted in a power loss due to carburetor ice. Carburetor icing conditions, a short takeoff area, and a ditch at the end of the airstrip were factors.

Aircraft Information

Registration
Make
CESSNA
Serial Number
15284566
Engine Type
4-cycle
Year Built
1980
Model / ICAO
152 C152
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
152

Registered Owner (Current)

Name
HILLSBORO AERO ACADEMY LLC
Address
3565 NE CORNELL
City
HILLSBORO
State / Zip Code
OR 97124
Country
United States

Analysis

On December 11, 1995, approximately 1900 Pacific standard time, a Cessna 152, N5366M, operated by Galvin Flying Service of Seattle, Washington, a 14 CFR 141 flight training school certificate holder, experienced a loss of engine power on takeoff from a private airstrip near Chimacum, Washington. The pilot in command, a certificated flight instructor, landed the airplane straight ahead on the airstrip, but the airplane struck a ditch at the end of the strip and nosed over. The airplane was substantially damaged but neither the pilot nor a student pilot-rated passenger were injured. The pilot stated that visual meteorological conditions existed at the airstrip. The pilot filed, but did not activate, a visual flight rules (VFR) flight plan for the 14 CFR 91 flight, which was to have proceeded to Boeing Field in Seattle.

The pilot stated on his accident report that the takeoff area was a 1,200-foot-long wet grass surface. He stated that prior to the takeoff attempt, he taxied along the strip several times to check conditions. He stated that the engine stopped once while taxiing but then restarted. The pilot stated that the takeoff proceeded normally until the airplane became airborne in ground effect. He reported that at this point, the engine lost "at least" 300 to 400 RPM. He stated that he then cycled carburetor heat, at which point the engine stopped completely. He landed straight ahead but was unable to stop in the remaining distance. The airplane then struck the ditch and nosed over. In an initial telephone interview conducted by the NTSB investigator-in-charge on the day after the accident, the pilot stated that he took off with carburetor heat off.

The pilot reported on the initial telephone interview that the outside air temperature on the aircraft gauge read 40 degrees F. At 1846, Port Angeles, 30 nautical miles west of Chimacum, reported fog, calm winds, and temperature and dewpoint of 45 degrees F. A Transport Canada carburetor icing hazard chart used by the investigator indicated that at the temperature and dewpoint reported in the Port Angeles observation, there was a potential for "serious icing - any power."

A test run of the accident aircraft's engine was conducted by Galvin Flying Service personnel under supervision of the NTSB and FAA at Boeing Field, Seattle, on December 20, 1995. The engine was successfully started and run.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA96LA028