Casualties unknown

2007-06-24: Cessna 177RG (N52103) — Wasilla, AK

Wasilla, AK, US

On June 24, 2007, a Cessna 177RG (registration N52103) was involved in an aviation accident near Wasilla, AK. Investigators recorded the probable cause as: The flight instructor's failure to adequately supervise the private pilot (dual student), and his delayed go-around during approach to land. Contributing to the accident was the dual student's misjudged distance/altitude. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

During commercial flight instruction, a private pilot and instructor collided with terrain during a go-around attempt. The aircraft impacted short of the runway, became airborne, then descended vertically. No preimpact mechanical anomalies were found.

Accident Overview

A flight instructor was providing commercial flight instruction to a private pilot preparing for a commercial flight test when the airplane collided with terrain at an unattended, public airport. The airplane's left wingtip and left main landing gear first impacted the ground on the north side of the runway, short of the threshold, as indicated by ground scars containing fragments of the left navigation light and parts from the left main landing gear.

Sequence of Events

After the initial impact, the airplane became airborne again for about 120 feet, leaving no ground scar, and then impacted terrain in a near-vertical descent, with enough forward motion to fold the engine under the fuselage. The airplane came to rest upright, with the engine intruding into the forward portion of the passenger cabin from underneath, significantly distorting the cabin area and decreasing survivable space.

Cockpit Configuration

Examination of the cockpit revealed that the landing light and fuel boost pump switches were in the on position, and the landing gear was extended, as in preparation for landing. However, the propeller, mixture, and throttle controls were forward, and the flap handle was up, as if initiating a go-around. The propeller showed signs of high power during impact.

Mechanical Examination

An examination of the engine and airframe disclosed no preimpact mechanical anomalies. The position of the airplane and ground scars, as well as the throttle and flap settings, are consistent with a low altitude, delayed attempt to reject the landing and go-around.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070709X00891. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.