No fatalities

22 Jul 2016: PIPER PA46 310P — Claremore, OK

Claremore, OK, United States

On 22 Jul 2016, a PIPER PA46 310P was involved in an aviation accident near Claremore, OK. No fatalities were reported. Investigators recorded the probable cause as: The pilot exceeded the critical angle of attack during the two initial climbs, and the airplane did not exit ground effect due to insufficient airspeed at rotation. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

During a takeoff from a closed runway's parallel taxiway, the airplane hit a dip, became airborne unintentionally, stalled, and veered into a ditch, resulting in substantial wing damage and landing gear collapse.

Accident Overview

A pilot reported an accident during takeoff from a taxiway at an airport where a NOTAM had closed the sole runway, permitting takeoffs and landings from the parallel taxiway. During the takeoff roll, the airplane struck a dip in the pavement and became airborne unintentionally. The pilot heard the stall warning horn and pitched the nose forward, but the airplane drifted left into a ditch, causing the nose and main landing gear to collapse. Both wings sustained substantial damage.

Pilot Actions and Conditions

The pilot indicated no mechanical malfunctions or failures that would have prevented normal operation. The takeoff weight was approximately 1 pound below the maximum allowable takeoff weight, and the pilot attempted a short-field takeoff technique. Density altitude at departure time was 3,168 feet, with a pressure altitude of 579 feet and a temperature of 93°F (34°C).

Video Evidence

Airport surveillance video showed the airplane's takeoff roll. About 2,050 feet into the roll, the airplane pitched up, lifting the nose and left main landing gear off the ground, but it did not climb. It touched back down and attempted to become airborne again approximately 300 feet later. The nose and main landing gear momentarily left the ground, but the airplane quickly settled back and moved out of camera view.

Performance Considerations

The Federal Aviation Administration provides guidance on how density altitude affects aircraft performance. According to the FAA Koch Chart, the airplane likely experienced a 35% increase in normal takeoff distance and a 25% decrease in normal climb rate. The FAA Airplane Flying Handbook notes that reduced drag in ground effect may allow an airplane to become airborne below recommended airspeed, but climbing out of ground effect with insufficient airspeed can result in marginal climb performance, especially under high-density altitude, high temperature, or maximum gross weight conditions.

Probable Cause

It is likely that the pilot exceeded the critical angle of attack during the two initial climbs, and the airplane did not exit ground effect due to insufficient airspeed at rotation.

Contributing factors

Causes

PilotDirectional control — Not attained/maintained

Other contributing factors

Capability exceededAirspeed — Not attained/maintainedEffect on operationContributed to outcome