ASN Wikibase Occurrence # 297649
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Sunday 20 January 2002 |
Time: | 15:00 LT |
Type: | Piper PA-18 |
Owner/operator: | Private |
Registration: | N7113K |
MSN: | 18-332 |
Year of manufacture: | 1950 |
Engine model: | Lycoming O-290 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Clear Lake, Minnesota -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | CLEAR LAKE, MN (8Y6) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The airplane collided with two fences during a forced landing to a field following an engine failure while in the traffic pattern. The pilot said that he had performed three "run ups" and was going to perform "...some take-offs and landings after the annual." He said that after take-off, at about 400 feet agl, the engine lost power and quit. He said that he had just turned from the crosswind leg of the traffic pattern to the downwind leg. The pilot stated that he could not make it back to the airport, and could not land directly ahead due to obstructions. The pilot said that he attempted to land in a field but the field did not have enough room for the landing and he hit two fences before coming to rest. A postaccident examination of the airplane revealed no anomalies that could be associated with a pre-impact condition. The engine was subsequently test run on the airframe and no anomalies were found. The weather observing station located about 7 miles and 330 degrees from the accident recorded the temperature as -3 degrees Celsius and the dewpoint as -7 degrees Celsius at 1453. According to a Transport Canada carburetor icing probability chart, the temperature and dewpoint fall in the range for light icing at cruise or descent power.
Probable Cause: The loss of engine power for undetermined reasons and the unsuitable terrain for the forced landing. Factors were the low altitude and the fences.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI02LA065 |
Status: | Investigation completed |
Duration: | 7 months |
Download report: | Final report |
|
Sources:
NTSB CHI02LA065
Revision history:
Date/time | Contributor | Updates |
15-Oct-2022 06:51 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation