ASN Wikibase Occurrence # 296329
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 22 December 2002 |
Time: | 17:00 LT |
Type: | Piper PA-28-235 |
Owner/operator: | Private |
Registration: | N8555W |
MSN: | 28-10069 |
Year of manufacture: | 1963 |
Engine model: | Lycoming O-540-B4B5 |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Carleton, Michigan -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | Pontiac-Oakland County International Airport, MI (PTK/KPTK) |
Destination airport: | Monroe, MI (KTFF) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The nose gear collapsed during an off airport forced landing following a loss of engine power. The pilot reported that while en route to his destination, the engine power dropped to 1,300 rpm. He stated he applied carburetor heat, turned on the auxiliary fuel pump, and switched fuel tanks to no avail. The pilot reported that the passenger checked the engine instruments and all indications were normal. The pilot contacted the Willow Run Air Traffic Control Tower and informed them of the situation, stating that he was going to land at their airport. After turning toward the airport, the pilot determined he was not going be able to reach the airport, so he pilot selected a plowed field in which to land. The nose gear collapsed during the landing and the airplane came to rest on the engine cowling and main landing gear. Examination of the engine revealed the #2 cylinder exhaust valve was broken off and a piece of the #2 cylinder was missing. Portions of the exhaust valve and valve stem were recovered from the engine. Visual examination revealed the fractured surfaces were deformed and obscured by impact damage to such a degree that the failure mode could not be determined.
Probable Cause: The #2 cylinder exhaust valve failed due to undetermined reasons. A factor associated with the accident was the soft terrain encountered during the forced landing.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI03LA043 |
Status: | Investigation completed |
Duration: | 6 months |
Download report: | Final report |
|
Sources:
NTSB CHI03LA043
Revision history:
Date/time | Contributor | Updates |
13-Oct-2022 19:16 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation