No fatalities

2008-01-16: Cessna 207 Skywagon/Stationair (N1701U) — Inland Aviation Services — Aniak, United States of America

Aniak, United States of AmericaLanding (descent or approach)

On January 16, 2008, a Cessna 207 Skywagon/Stationair (registration N1701U) operated by Inland Aviation Services was involved in an aviation accident near Aniak, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: A partial loss of engine power for an undetermined reason. Contributing to the accident were the pilot's inadvertent encounter with IMC conditions, and a whiteout during his attempted go around from an emergency landing approach. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197669Data APIEditorial standards

A commercial pilot experienced engine fuel pressure fluctuations and power loss after receiving SVFR clearance, switched fuel tanks, regained full power, but collided with a river surface while preventing excessive climb; aircraft sustained structural damage.

Flight Details

The commercial certificated pilot was returning from a remote village after completing a round robin flight of approximately 130 miles over a frozen and snow-covered river. During cruise flight at about 500 feet above ground level (AGL), the pilot circled while holding between 6 and 7 miles east of the destination airport, awaiting a special VFR (SVFR) clearance.

Weather Conditions

At the holding location, weather conditions were reported as about 1 mile visibility with a ceiling of approximately 1,000 feet AGL. The pilot later described near white-out conditions, though he could see the bank of the river. At the time of the accident, the airport reported a ceiling of 600 feet obscured and visibility of 1/2 mile in snow.

Engine Anomaly and Forced Landing

After receiving SVFR clearance, the pilot proceeded toward the airport. Shortly thereafter, the engine fuel pressure began fluctuating, followed by a decrease in engine rpm and a loss of altitude. The pilot switched fuel tanks, selected full flaps, and prepared for a forced landing.

Accident Sequence

Upon switching the fuel tank selector from the left to the right tank, the engine power suddenly returned to full power. The pilot applied forward flight control pressure to prevent the airplane from climbing too rapidly. Despite this action, the airplane collided with the surface of the river. The collision resulted in structural damage to both the wings and the fuselage.

Aftermath

Neither the fuel status of the accident airplane nor the mechanical condition of the engine was verified by the National Transportation Safety Board or the Federal Aviation Administration.

Probable cause

A partial loss of engine power for an undetermined reason. Contributing to the accident were the pilot's inadvertent encounter with IMC conditions, and a whiteout during his attempted go around from an emergency landing approach.