Accident Piper PA-28-235 N8540W,
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ASN Wikibase Occurrence # 44383
 
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Date:Monday 8 August 2005
Time:12:58
Type:Silhouette image of generic P28B model; specific model in this crash may look slightly different    
Piper PA-28-235
Owner/operator:Private
Registration: N8540W
MSN: 28-10041
Year of manufacture:1963
Total airframe hrs:3177 hours
Engine model:Lycoming O-540-B2B5
Fatalities:Fatalities: 2 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:Big Bear City, CA -   United States of America
Phase: Landing
Nature:Private
Departure airport:Las Vegas, NV (KHND)
Destination airport:Big Bear City, CA (KL35)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The airplane made a sudden steep turn to the right, rolled inverted, and impacted the ground just after the landing flare. Witnesses observed the airplane make a normal landing approach to runway 08 and flare. The engine suddenly went to full power, the nose pitched up, and the plane abruptly turned to the right. It then continued to roll right and impacted the ground inverted at the south edge of the airport boundary. The airplane's sudden turn and right roll is consistent with the result of a cross-control stall to the right, as described by the Airplane Flying Handbook. Two witnesses stated that they saw an airplane takeoff from runway 26 (in the opposite direction) moments after the crash. Approximately 5 minutes after the accident radar data identified a contact 2 miles east of the airport, traveling at 85 knots, departing the vicinity. Four minutes would be the approximate amount of time required for an airplane traveling at 85 knots to perform a downwind departure from the airport and appear on radar 2 miles to the east, if it followed the approximate 5.5-mile downwind departure route. Radar coverage to pattern altitude was not possible due to the mountainous terrain in which the airport is located. Examination of the airplane revealed no evidence of a preimpact malfunction or failure of the control system or power plant.
Probable Cause: The pilot's failure to maintain aircraft control and adequate airspeed while executing an evasive maneuver during an aborted landing, which resulted in a cross-controlled accelerated stall and impact with terrain. Contributing to the accident was the probable presence of another aircraft on the runway traveling in the opposite direction.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX05FA262
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20050817X01265&key=1

Location

Revision history:

Date/timeContributorUpdates
28-Oct-2008 00:45 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
06-Dec-2017 10:50 ASN Update Bot Updated [Source, Narrative]

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