N5932U

Substantial
None

PIPER PA-28-140 S/N: 28-7125143

Accident Details

Date
Sunday, March 31, 1996
NTSB Number
CHI96LA121
Location
THIEF RVR FALLS, MN
Event ID
20001208X05388
Coordinates
48.110870, -96.170951
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A ruptured oil line, which resulted in oil exhaustion and subsequent loss of engine power.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-7125143
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Name
ANDERSON THOMAS E DBA
Address
1071 CHESTNUT SPGS
City
BULVERDE
State / Zip Code
TX 78163-1701
Country
United States

Analysis

On March 31, 1996, at 1558 central standard time (cst), a Piper, PA-28-140, N5932U, operated by a private pilot, sustained substantial damage when during a forced landing, the airplane struck an electrical wire. The airplane subsequently impacted the terrain. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. No flight plan was on file. The pilot reported no injuries. The local flight originated at Thief River Falls, Minnesota, at 1545 cst.

In his written statement, the pilot said that as he was departing north from the airport, he "noticed a puff of smoke." He headed back to the airport. While en route to the airport, the engine began to run rough, then quit. The pilot elected to force land the airplane on a road. When he determined that he would not make the road, he turned so he could land the airplane in an adjacent field. On approach to the field, the airplane struck an electrical wire. The airplane subsequently impacted on the field and came to a stop.

The Federal Aviation Administration (FAA) inspector who examined the wreckage at the scene found the airplane resting upright in a snow-covered field. The airplane's forward fuselage, from the cowling aft to the crew compartment was bent. The airplane's nose wheel and firewall were bent up and aft into the underside of the engine cowling. The propeller exhibited bending. Both main landing gear were sheared off. Flight control continuity was confirmed. Fuel was noted in both wing tanks, and the smell of fuel was evident at the scene. No oil was found on the engine dipstick. The examination of all other airplane systems revealed no anomalies.

The engine was removed and examined at AIC Maintenance, Inc., Castleton, North Dakota, on April 17, 1996. The examination revealed that the oil line running from oil cooler to the engine case had ruptured near the back of the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA121