N50XP

Substantial
None

Cessna 150MS/N: 15077981

Accident Details

Date
Friday, May 17, 2002
NTSB Number
FTW02LA153
Location
Godley, TX
Event ID
20020521X00709
Coordinates
32.354167, -97.062774
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the loss of engine power for undetermined reasons. A contributing factor was the pilot's failure to maintain clearance with the transmission wire during the precautionary landing.

Aircraft Information

Registration
N50XP
Make
CESSNA
Serial Number
15077981
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
150MC150
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
1500 HOUSTON ST
Status
Deregistered
City
FORT WORTH
State / Zip Code
TX 76102-6524
Country
United States

Analysis

On May 16, 2002, approximately 1900 central daylight time, a Cessna 150M single-engine airplane, N50XP, sustained substantial damage when it impacted a transmission wire during a precautionary landing to a field following a loss of engine power while in cruise flight near Godley, Texas. The private pilot, sole occupant of the airplane, was not injured. The airplane was registered to Delta Aeronautics Inc., Fort Worth, Texas, and operated by Delta Qualiflight, Fort Worth. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 instructional flight. The local flight departed the Fort Worth Mecham International Airport, Fort Worth, approximately 1800.

The pilot reported that prior to departure from Fort Worth, he performed an engine run-up with no anomalies noted. Approximately 1.8 hours into the flight, the airplane "experienced engine roughness." During a precautionary landing to a field, the airplane impacted a transmission wire.

An FAA inspector, who responded to the accident site, reported that the airplane came to rest upright in the field with the nose landing gear separated, and the aft wing spars bent. The fuel selector was found in the OFF position, the right fuel tank was approximately 1/2 full of fuel, and the left fuel tank was approximately 2/3 full of fuel. The FAA inspector rotated the engine crankshaft by hand; the engine crankshaft was free to rotate, and the engine accessories drive shafts were observed to rotate. The reason for the loss of engine power was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA153