N6466G

Substantial
None

Cessna 150K S/N: 15071966

Accident Details

Date
Wednesday, April 17, 1996
NTSB Number
LAX96LA173
Location
MOJAVE, CA
Event ID
20001208X05617
Coordinates
35.070129, -118.180313
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's failure to clear the engine during an idle power descent, as required by the engine manual.

Aircraft Information

Registration
N6466G
Make
CESSNA
Serial Number
15071966
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
150K C150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ROBERTS SEAN
Address
HANGAR 61 MOJAVE ARPT
Status
Deregistered
City
MOJAVE
State / Zip Code
CA 93501
Country
United States

Analysis

On April 17, 1996, at 0915 hours Pacific daylight time, a Cessna 150K aircraft, N6466G, was substantially damaged during an off-airport landing 1 mile east of the Mojave, California, airport. The airline transport pilot and one passenger were not injured. Visual meteorological conditions prevailed for the instructional flight.

The second pilot, who holds a commercial pilot license, told an inspector from the FAA Van Nuys, California, Flight Standards District Office that the flight was part of the training syllabus of a private test pilot school. After descent from 7,000 feet (4,200 feet AGL) with the engine idled, carburetor heat on and mixture rich, the engine failed to produce power when the throttle was advanced during landing approach to runway 25. The first pilot took control of the aircraft at this point; however, because of 20- to 30-knot surface winds, he was not able to glide to the runway. An off-airport landing was made in the desert and the aircraft nosed over. The second pilot stated that they had not "cleared" the engine during descent.

The Teledyne Continental Motors Operator's Manual for the O-200 engine, dated January 1975, states on page 19: "If a long glide is made, apply power at short intervals to clear the cylinders and retain engine temperatures in the event that instant power is required." Inspection of the engine by the FSDO inspector revealed heavy carbon buildup under the intake and exhaust valves and low compression. After staking the valves compression returned to normal. The fuel supply was clear and the magnetos and spark plugs sparked normally.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX96LA173