Accident Piper PA-28R-200 N55676,
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ASN Wikibase Occurrence # 39821
 
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Date:Saturday 10 May 1997
Time:14:40 LT
Type:Silhouette image of generic P28R model; specific model in this crash may look slightly different    
Piper PA-28R-200
Owner/operator:Riverside Executives, Inc.
Registration: N55676
MSN: 28R-7335269
Year of manufacture:1973
Engine model:Lycoming IO-360-C1C
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Destroyed
Category:Accident
Location:Tigard, OR -   United States of America
Phase: Approach
Nature:Private
Departure airport:Mulino, OR (4S9)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot flew to a local airport for lunch with the passenger. The airplane was full of fuel, and no problems had previously been reported with it. After lunch, the airplane returned to the departure airstrip. During approach, about 1/2-mile from the runway, the engine began to run rough as the airplane was about 200 feet above wooded terrain. The pilot reversed course and attempted a landing in an open field. The airplane struck trees and terrain as the engine began to regain power. The wreckage was subjected to a post-crash fire. Examination of the engine/airframe did not reveal any evidence of preimpact mechanical malfunction. Defoliated trees near the impact site of the left wing indicated the left fuel tank had a significant quantity of fuel at the time of impact. The lack of fuel, fire damage and hydraulic deformation of the right wing, which was found near an area of intense fire, indicated that the right fuel tank was almost empty. The fuel selector valve was found in the RIGHT or OFF position, and it does not have a BOTH selection. The airplane would have consumed more than the max usable capacity of either wing if used exclusively.

Probable Cause: The pilot's failure to properly manage the aircraft fuel supply, which led to fuel exhaustion of the right tank and subsequent fuel starvation/power loss of the engine during the final approach. Factors contributing to the accident were the lack of sufficient altitude to effect a recovery, and the lack of suitable terrain for a successful forced landing.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: SEA97FA106
Status: Investigation completed
Duration: 2 years and 9 months
Download report: Final report

Sources:

NTSB SEA97FA106

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:23 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
08-Apr-2024 15:31 ASN Update Bot Updated [Time, Operator, Other fatalities, Source, Narrative, Category, Accident report]

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