ASN Wikibase Occurrence # 297223
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: | Friday 31 May 2002 |
Time: | 16:30 LT |
Type: | Piper PA-24-250 |
Owner/operator: | Private |
Registration: | N5360P |
MSN: | 24-409 |
Year of manufacture: | 1958 |
Total airframe hrs: | 2720 hours |
Engine model: | Lycoming O-540-AID5 |
Fatalities: | Fatalities: 0 / Occupants: 4 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Sparta, Illinois -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | Sparta Community Airport, IL (SAR/KSAR) |
Destination airport: | Eldon, MO (H79) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The airplane was substantially damaged when the gear collapsed during a forced landing due to a total loss of engine power. The airplane was directly over the Festus Memorial Airport (FES), Festus, Missouri when the engine started to run rough. The pilot decided to return to the Sparta Community-Hunter Field Airport (SAR), Sparta, Illinois, approximately 35 nautical miles (nm) from FES. The engine experienced a total loss of engine power approximately eight nm from SAR and the pilot executed an emergency landing on a wheat field. The number five cylinder was found to have separated from the engine. The last major overhaul on the engine was conducted on November 1, 1988 and the engine had accumulated 526 hours since the overhaul. The engine manufacturer recommends the engine be overhauled every 12 years even if the engine does not meet the time between overhaul hours.
Probable Cause: The total loss of engine power due to a separated cylinder and the failure of the pilot to perform a precautionary landing at the nearest suitable airport when the engine had a partial loss of engine power. The failure of the aircraft owners to perform an engine overhaul and the unsuitable terrain encountered during the emergency landing were contributing factors.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI02LA150 |
Status: | Investigation completed |
Duration: | 10 months |
Download report: | Final report |
|
Sources:
NTSB CHI02LA150
Revision history:
Date/time | Contributor | Updates |
14-Oct-2022 15:57 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation