N80859

Substantial
None

Cessna 172MS/N: 66776

Accident Details

Date
Tuesday, February 14, 2006
NTSB Number
LAX06CA115
Location
Murrieta, CA
Event ID
20060314X00299
Coordinates
33.574165, -117.128334
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

a partial loss of engine power resulting from the student pilot's mismanagement of the mixture control.

Aircraft Information

Registration
N80859
Make
CESSNA
Serial Number
66776
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
172MC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RTI AVIATION LLC
Address
2711 CENTERVILLE RD PMB 7073
Status
Deregistered
City
WILMINGTON
State / Zip Code
DE 19808-1660
Country
United States

Analysis

The airplane landed hard in a field adjacent to the airport during an attempted takeoff. The purpose of the solo flight was for the student pilot to perform practice touch-and-go takeoff and landings. After completing a normal takeoff, he continued around the traffic pattern and then preformed a normal landing. During the landing rollout he retracted the flaps, input full throttle, and pushed the mixture control partially forward, leaving it out about 7/8 inch. The airplane lifted off the runway surface and climbed to about 50 to 100 feet above ground level (agl), with an airspeed of about 60 knots. The airplane was not able to maintain the airspeed and the student pilot thought the engine was only producing partial power. He opted to perform a precautionary landing in an open field adjacent to the runway. The airplane landed hard and the left main landing gear broke off.

Damage to the airplane included the left main landing gear, firewall, and underside of right wing. Post accident examinations by both the operator and Federal Aviation Administration (FAA) inspector revealed no evidence of engine or airframe anomalies that would have precluded normal operation. The FAA inspector stated that the signatures on the spark plugs indicated a very lean condition. An engine run was conducted the day following accident and the FAA inspector attempted to power the engine to about 2,000 revolutions per minute (rpm); he did not want to apply full power due to the instability of the airplane from the damaged left main landing gear. The engine ran normally with no discrepancies noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX06CA115