Runway excursion Accident Cessna A185F N4492,
ASN logo
ASN Wikibase Occurrence # 288212
 
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:Wednesday 11 August 2010
Time:10:50 LT
Type:Silhouette image of generic C185 model; specific model in this crash may look slightly different    
Cessna A185F
Owner/operator:Private
Registration: N4492
MSN: 18502971
Year of manufacture:1976
Total airframe hrs:2371 hours
Engine model:Continental IO-520-D
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Farmington, New Mexico -   United States of America
Phase: Landing
Nature:Private
Departure airport:San Antonio-Stinson Municipal Airport, TX (SSF/KSSF)
Destination airport:Farmington Municipal Airport, NM (FMN/KFMN)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot said that very little crosswind correction was required as he landed on runway 25. After rolling a few hundred feet, the airplane "swerved very strongly to the right." Opposite brake and rudder had no effect and the airplane departed the runway and impacted terrain. The left landing gear collapsed and the left wing and elevator sustained leading edge damage. Federal Aviation Administration inspectors found that the through-bolt that attached the inboard end of the gear leg to the airframe hard-point had pre-existing damage. Further examination found that threads from the failed nut remained stuck in the threads of the bolt, indicating that the nut failed and stripped off the bolt, leaving the inboard end of the gear leg loose and free to move up and down. This allowed the gear leg to move forward and aft. The chaffing on the longeron, inboard of the gear leg attach point, was indicative that the bolt-nut combination had been loose for some time. There were indications of looseness on the right gear leg attach bolt after the leg was removed for transport.

Probable Cause: Pre-existing damage of the through-bolt that attached the inboard end of the gear leg to the airframe hard-point, likely caused during maintenance on the gear.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN10LA474
Status: Investigation completed
Duration: 4 months
Download report: Final report

Sources:

NTSB CEN10LA474

Location

Revision history:

Date/timeContributorUpdates
04-Oct-2022 19:40 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org