Accident de Havilland Canada DHC-2 Beaver N105RL,
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ASN Wikibase Occurrence # 178411
 
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Date:Saturday 12 June 2004
Time:18:30
Type:Silhouette image of generic DHC2 model; specific model in this crash may look slightly different    
de Havilland Canada DHC-2 Beaver
Owner/operator:private
Registration: N105RL
MSN: 720
Year of manufacture:1957
Total airframe hrs:7864 hours
Engine model:Pratt & Whitney R985-AN-14B
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Gattis Strip Airport, ca 3 mi NE of Wasilla, AK -   United States of America
Phase: Landing
Nature:Executive
Departure airport:Northway, AK (PAOR)
Destination airport:Wasilla, AK (16AK)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The second pilot, who was seated in the right seat, was landing a tailwheel-equipped airplane on runway 04 at a private airport. Runway 04 is 1,200 feet long, and has an asphalt surface. The second pilot indicated that runway 04 sloped uphill, and he was landing with a slight tailwind. He said that the right pilot position did not have any brake pedals, and that he did not have a tailwheel endorsement. He relied on the first pilot, seated in the left seat, to apply the brakes after touchdown. The second pilot said that during the landing roll, as the first pilot applied the brakes, the airplane veered sharply to the right and departed the runway. The right main landing gear wheel struck a log, the right wing contacted several small trees, and the airplane momentarily nosed down. The airplane received structural damage at the right main landing gear attach point, damage to the propeller, the aft fuselage adjacent to the tailwheel attach point, and the left main landing gear strut. The closest official weather observation station, located 3 nautical miles southwest of the accident site, was reporting, in part: Wind, 240 degrees (true) at 7 knots.
Probable Cause: The pilot's failure to maintain directional control of the airplane during the landing roll, which resulted in a collision with a log. Factors contributing to the accident were a tailwind, a lack of brake pedals at the second pilot station, and the second pilot's lack of a tailwheel endorsement.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ANC04LA064
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20040617X00829&key=1

Location

Revision history:

Date/timeContributorUpdates
08-Aug-2015 12:45 Noro Added
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Dec-2017 18:03 ASN Update Bot Updated [Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative]
04-Jan-2018 10:03 harro Updated [Aircraft type]
14-Mar-2021 16:11 TB Updated [Operator, Location]

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