Aviation Accident Summaries

Aviation Accident Summary SEA95LA061

FORKS, WA, USA

Aircraft #1

N4778A

PIPER PA-22-150

Analysis

THE PILOT STATED THAT ABOUT 30 MINUTES INTO A LOCAL FLIGHT HE HEARD A STRANGE POPPING NOISE AND STARTED LOSING RPMS. HE CHECKED THE MIXTURE CONTROL, SWITCHED FUEL TANKS, APPLIED CARBURETOR HEAT, AND ATTEMPTED OTHER CORRECTIVE ACTION. WHEN POWER WAS NOT REGAINED, THE PILOT ATTEMPTED A FORCED LANDING ON A GRAVEL BAR IN A RIVER. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE DURING ROLLOUT. THE ENGINE HAD 1000 RPM WHEN THE AIRCRAFT STOPPED. FAA INSPECTORS FOUND THE AIRCRAFT TO HAVE NOT HAD AN ANNUAL INSPECTION IN SEVERAL YEARS, AND FOUND MULTIPLE MECHANICAL DISCREPANCIES; NONE OF WHICH WOULD PRECLUDE THE ENGINE FROM OPERATING.

Factual Information

On March 5, 1995, approximately 1130 hours Pacific standard time (pst), a Piper PA-22-150, N4778A, registered to and being flown by a certificated private pilot, was substantially damaged when the nose gear collapsed during landing rollout following a partial loss of power while in cruise. The accident occurred near Forks, Washington, and the pilot sustained minor injuries. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was personal, was to have been operated under 14CFR91, and originated from Forks approximately 1100. The pilot reported that at 1500 feet MSL the engine popped several times and began losing power. Unable to maintain altitude, the pilot executed a forced landing to a sand bar in the Hoh River, during which the nose landing gear impacted a large rock and separated. The pilot, whose last medical was issued September 4, 1991, reported to the FAA that the aircraft had not had an annual inspection for several years and that he was utilizing auto gas at the time of the accident. Inspection of the aircraft by FAA inspectors revealed multiple mechanical discrepancies and maintenance deficiencies, however nothing obvious was found that could cause the loss of power described by the pilot. The carburetor heat control was in the on position.

Probable Cause and Findings

THE LOSS OF POWER FOR UNDETERMINED REASONS AND THE LACK OF SUITABLE TERRAIN FOR A SUCCESSFUL FORCED LANDING.

 

Source: NTSB Aviation Accident Database

Get all the details on your iPhone or iPad with:

Aviation Accidents App

In-Depth Access to Aviation Accident Reports