N57828

Substantial
Minor

Piper PA-36-300 S/N: 36-7760002

Accident Details

Date
Thursday, February 22, 1996
NTSB Number
FTW96LA126
Location
ANDREWS, TX
Event ID
20001208X05254
Coordinates
32.320068, -102.540565
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the mechanic's improper overhaul of the engine. Factors were: the pilot in command's inability to maintain visual lookout due to oil on the windscreen and unsuitable terrain for the forced landing.

Aircraft Information

Registration
N57828
Make
PIPER
Serial Number
36-7760002
Engine Type
Reciprocating
Model / ICAO
PA-36-300 PA36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WOOLIE ENTERPRISES
Address
401 LAKEVIEW DR
Status
Deregistered
City
OLDSMAR
State / Zip Code
FL 34677-4505
Country
United States

Analysis

On February 22, 1996, at 0915 central standard time, a Piper PA-36-300, N57828, owned and operated by a private owner, was substantially damaged during a forced landing near Andrews, Texas. The commercial pilot received minor injuries. The aircraft was being operated as a personal flight under Title 14 CFR Part 91. The flight originated in Andrews, Texas at 0915. Visual meteorological conditions prevailed for the local flight for which a flight plan was not filed.

The airplane was on its first flight after an engine overhaul. The pilot reported that moments after takeoff, oil "blew over my windshield," and he was unable to see out of the windshield. The pilot shut down the engine and turned back towards runway 30. Unable to make the runway, the airplane touched down in a "very rough pasture, bounced over a fence, and hit on the end of the [runway] overrun," damaging the landing gear and fuselage.

According to the FAA inspector, the crankshaft and crankcase thrust surfaces had failed. A field teardown of the engine, conducted by the FAA Inspector, revealed that the oil pressure loss was traced to the installation of the incorrect crankshaft oil seal. The oil seal had become dislodged during the flight. The crankshaft and crankcase thrust surface damage was determined to be the result of misalignment of the crankcase halves during a previous modification.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA126