Casualties unknown

1997-08-19: Beech B24R (N2521W) — Abilene Aero — Albany, TX

Albany, TX, US

On August 19, 1997, a Beech B24R (registration N2521W) operated by Abilene Aero was involved in an aviation accident near Albany, TX. Investigators recorded the probable cause as: The flight instructor's failure to maintain aircraft control during the takeoff/initial climb. A factor was the flight instructor's lack of experience in the make and model of aircraft. 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 a night training flight, a steep climb initiated after takeoff resulted in a near-vertical descent and impact with trees and terrain. The aircraft was destroyed by post-impact fire and explosion.

Accident Overview

A night instructional flight ended when, after initiating a steep climb following takeoff, the aircraft descended in a near-vertical attitude and impacted trees and terrain. A post-impact fire and explosion ensued.

Witness Observations

Witnesses reported that the airplane lifted off the runway, accelerated while remaining in ground effect, and near the departure end of the runway climbed in a vertical attitude, banked, and then descended. Local authorities and the flight instructor's students had previously observed the flight instructor perform this same maneuver in single-engine high-wing aircraft.

Pilot and Aircraft Information

The flight instructor had accumulated 17.1 hours in the low wing single-engine aircraft involved, which included one night flight of 1.5 hours consisting of takeoffs and landings.

Physical Evidence

Examination of the accident site revealed that the airplane impacted the ground in a nose-low attitude with a left bank. The landing gear and flaps were in the retracted configuration. No evidence of any pre-impact mechanical anomalies was found. Flight control continuity was established; however, the stabilator up cable was found severed due to arcing and tensile overload.

Investigation Findings

The investigation did not identify any mechanical malfunctions or anomalies that would have contributed to the accident. The aircraft's flight controls were functional up to the point of impact, except for the severed stabilator cable, which resulted from the accident sequence.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X08611. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.