Runway excursion Accident Ayres S-2R-T Turbo Thrush N32LF,
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ASN Wikibase Occurrence # 239275
 
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Date:Wednesday 16 August 2017
Time:18:00
Type:Silhouette image of generic SS2T model; specific model in this crash may look slightly different    
Ayres S-2R-T Turbo Thrush
Owner/operator:Glenn Air, Inc.
Registration: N32LF
MSN: 5089R
Year of manufacture:1977
Total airframe hrs:10527 hours
Engine model:Honeywell Aersopace TPE331-6-252M
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Talkeetna, AK -   United States of America
Phase: Landing
Nature:Executive
Departure airport:Willow, AK (UUO)
Destination airport:Talkeetna, AK (AK61)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot was transporting bulk fuel to a remote lodge. During the landing to the dirt and gravel runway, the tail of the airplane came down, and the pilot heard a loud bang. He reported the empennage “went clear” to the ground and that he had no rudder authority. The pilot attempted to control the airplane, but the airplane departed the runway and impacted a ditch, which resulted in substantial damage to the left wing, fuselage, and empennage.
The tailwheel spring assembly and a fractured attachment bolt were recovered from the airplane. An examination revealed that the deformation of the bolt and appearance of the fracture surface were consistent with bending overstress. The spring and a portion of the bolt exhibited corrosion and pitting; signs of fatigue were not noted.
The airplane flight manual states to lower the tail smoothly during the landing roll. Because the deformation of the bolt and the fracture surface were the result of overstress, it is likely that the pilot allowed an excessive landing load on the tailwheel when it touched down, which resulted in a loss of control and a subsequent runway excursion and impact with terrain.




Probable Cause: The pilot's improper landing in the tailwheel-equipped airplane, which allowed an excessive load on the tailwheel and resulted in the subsequent component fracture, loss of control, runway excursion, and impact with terrain.



Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ANC17LA046
Status: Investigation completed
Duration: 2 years and 11 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
09-Aug-2020 07:24 ASN Update Bot Added

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