BELLANCA 17-31ATC

Roosevelt, UT — June 19, 2009

Event Information

DateJune 19, 2009
Event TypeACC
NTSB NumberWPR09LA297
Event ID20090619X54345
LocationRoosevelt, UT
CountryUSA
Coordinates40.27833, -110.05139
AirportRoosevelt Municipal
Highest InjuryNONE

Aircraft

MakeBELLANCA
Model17-31ATC
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDUSK
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None1
Total Injured0

Event Location

Probable Cause

The retraction of the left main landing gear due to the failure of the extension and retraction actuator arm attach bolt. Contributing to the accident was the failure of maintenance personnel to discover the extensive elongation of the actuator attach fitting bolt hole during past annual inspections.

Full Narrative

On June 18, 2009, about 2115 mountain daylight time, a Bellanca 17-31ATC, N14797, experienced a collapse of the left main landing gear during the landing roll at Roosevelt Municipal Airport, Roosevelt, Utah. The commercial pilot, who was the sole occupant, was not injured, but the airplane, which is owned and operated by the pilot, sustained substantial damage. The local 14 Code of Federal Regulations Part 91 personal pleasure flight, which departed Roosevelt Municipal Airport about 15 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed.

According to the pilot, this was a brief local flight to check the operation of the turbocharger, which had just come out of maintenance. After the flight around the local area, the pilot returned to the airport for a full stop landing. Reportedly, he made a normal flare and touchdown, and the first 1,000 feet of the landing roll was uneventful. The left main landing gear green DOWN light went out, and the red landing gear TRANSITION warning light came on, and the left main gear retracted. After the gear retracted, the airplane exited the left side of the runway, and collided with rough terrain. This sequence resulted in damage to the left wing, and bending of the fuselage structure.

A post- accident inspection of the left landing gear extension and retraction system by a Federal Aviation Administration (FAA) Airworthiness Inspector determined that the bolt connecting the hydraulic gear actuator rod to the gear leg support had failed. Further inspection revealed that over a period of time the bolt hole in the gear leg support had worn to a point where it had become elongated to about twice its original size (see photo in the public docket for this accident). According to the FAA inspector, the elongation of the hole, and the looseness it would have created, should have been detected during at least the last couple of annual inspections.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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