No fatalities

3 Sep 2011: STINSON V77 (N9112H) — Tillamook Air Tours — Tillamook, OR

Tillamook, OR, United States

On 3 Sep 2011, a STINSON V77 (registration N9112H) operated by Tillamook Air Tours was involved in an aviation accident near Tillamook, OR. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s loss of directional control while taxiing in a gusting tailwind. This summary draws on records from NTSB; 2 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

A Stinson V77, N9112H, sustained substantial damage when its right main landing gear collapsed after a loss of control during taxi at Tillamook Airport, Oregon, on September 3, 2011. The pilot and two passengers were uninjured.

Accident

On September 3, 2011, about 1140 Pacific daylight time, a Stinson V77, registration N9112H, sustained substantial damage during taxi for takeoff at Tillamook Airport (TMK), Tillamook, Oregon. The airline transport pilot and two passengers were not injured. The aircraft was operated by Tillamook Air Tours under 14 Code of Federal Regulations Part 91 as a local sightseeing flight. Visual meteorological conditions prevailed, and a company flight plan was on file.

Pilot Statement

The pilot reported that he was taxiing on runway 19 with the intention of turning around to take off on runway 01. The wind was a left quartering tailwind, and the first 800 to 1,000 feet of taxi were uneventful. Suddenly, the airplane rotated over 90 degrees to the left. The right main landing gear collapsed, and the airplane dropped onto its right wing and horizontal stabilizer. The pilot believed the loss of control was due to a strong gust of wind.

Post-Accident Examination

A Federal Aviation Administration inspector examined the airplane after the accident. The right wing and horizontal stabilizer were bent, and the fuselage was wrinkled and bent on the left aft lower side and on the right side where the main landing gear joined the fuselage. The right main landing gear pivot bushing, made of steel tubing, had cracked longitudinally and split in half, allowing the landing gear leg to separate from the airplane. Some areas of corrosion were present on the bushing.

Metallurgical Analysis

Pieces of the fractured pivot bushing were examined at the National Transportation Safety Board's Materials Laboratory. The fracture features were consistent with overstress fracture. No evidence of preexisting fatigue cracking was found.

Weather

At 1135, the reported wind at TMK was from 050 degrees at 13 knots. At 1155, the reported wind was from 050 degrees at 13 knots with gusts to 18 knots.

Contributing factors

Causes

Directional control — Not attained/maintainedPilot

Other contributing factors

Effect on operation