Casualties unknown

1998-11-07: Cessna 152 (N6312P) — Auburn, WA

Auburn, WA, US

On November 7, 1998, a Cessna 152 (registration N6312P) was involved in an aviation accident near Auburn, WA. Investigators recorded the probable cause as: A partial loss of engine power due to carburetor ice formation. Factors included insufficient altitude/time available for remedial action, a tail wind during the forced landing attempt, and a fence at the end of the runway. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane experienced partial engine power loss at 300 ft during climb after touch-and-go. Instructor performed 180° turn for opposite-direction landing with tailwind; aircraft overran runway, struck fence, and nosed over. Carburetor icing hazard existed at cruise power.

Accident Overview

During a training flight, the airplane was climbing out from a touch-and-go landing when it experienced a partial loss of engine power at approximately 300 feet above ground level. The instructor, who was in control, promptly executed a 180-degree turn to attempt a landing on the departure runway in the opposite direction. This maneuver was performed to avoid high-tension lines located 1,660 feet from the departure end of the runway.

Forced Landing Attempt

The forced landing attempt was conducted with an estimated 15-knot tail wind due to the opposite direction. The airplane touched down at approximately midfield at a high speed. It subsequently overran the end of the runway, struck a fence, and nosed over.

Weather and Engine Conditions

Weather conditions in the area at the time posed a hazard of serious carburetor icing at cruise power. Post-accident, the accident aircraft's engine was successfully test-run, indicating no mechanical failure was found during that test.

Investigation Findings

The investigation noted the carburetor icing risk but did not assign a probable cause for the partial power loss. The engine's successful operation after the accident suggests the power loss may have been transient or related to environmental factors such as carburetor icing.

_Note: No aircraft type, registration, operator, date, location, or occupant details were provided in the source._

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X11498. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.