Casualties unknown

2003-05-23: Piper PA-32-260 (N3921W) — James A. Caldwell — Fort Meade, FL

Fort Meade, FL, US

On May 23, 2003, a Piper PA-32-260 (registration N3921W) operated by James A. Caldwell was involved in an aviation accident near Fort Meade, FL. Investigators recorded the probable cause as: Thew failure of the pilot to abort the takeoff after travelling past the estimated point of liftoff, and failure of the pilot to maintain airspeed during the initial climb resulting in inadvertent stall and uncontrolled descent with subsequent impact onto the… 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

A pilot reported that during a short/soft field takeoff from a 3,000-foot grass strip, the airplane stalled at 20 feet AGL and struck fences.

Incident Overview

A pilot reported an accident during a takeoff attempt from a 3,000-foot grass strip with approximately 4-inch tall grass. The pilot stated that he performed weight and balance calculations before the flight by asking passengers their weights and estimating the weights of their bags. He calculated that the airplane was within center of gravity and weight limits.

Preflight and Takeoff

A preflight inspection of the airplane revealed no discrepancies. Before takeoff, the pilot performed an engine run-up with no discrepancies noted. He lowered the flaps to 10 degrees and initiated a short/soft field takeoff, applying full power while rolling onto the runway. The engine responded, and the pilot estimated that the airplane became airborne approximately three-quarters of the way down the runway.

Stall and Impact

While airborne at 20 feet above ground level, the airplane "stalled came back down and began sliding." The airplane traveled through three fences before coming to rest. The pilot stated that he expected the airplane should have become airborne about halfway down the runway and that there was no mechanical failure or malfunction.

Post-Accident Engine Run

The airplane was recovered, and no repairs to the engine or its systems were performed. With FAA oversight, the engine was started and operated to 2,000 rpm. Safety concerns prevented operation to a higher rpm, but no discrepancies were noted during the engine run. The engine was operated with the fuel selector positioned to the right main fuel tank, which had been selected for takeoff.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030603X00757. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.