Beech A45 accident near Montgomery, TX

On November 19, 2003, a Beech A45 (airplane) was involved in an accident near Montgomery, TX. 2 people died. Damage to the aircraft: destroyed.

Date
November 19, 2003
Place
Montgomery, TX
Aircraft
Beech A45 · Airplane
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
30.455°N, 95.663°W
NTSB ID
20031203X01988

NTSB summary

HISTORY OF FLIGHT On November 19, 2003, at 1016 central standard time, a Beech A45 single-engine airplane, N44KK, registered to PRVNY PLUK, LLC, of Houston, Texas, and operated by Texas Air Aces of Spring, Texas, was destroyed when it impacted terrain following a loss of control after an in-flight breakup while maneuvering near Montgomery, Texas. The commercial pilot and pilot-rated passenger were fatally injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 training flight. The local flight originated from the David Wayne Hooks Memorial Airport (DWH), near Spring, Texas, approximately 0930, in the flight lead position of a flight of two airplanes. The pilot-rated passenger attended Texas Air Aces for a two-day advanced maneuvering program (AMP), which included ground school and in-flight training that focused on unusual attitude recognition and "upset" recovery. On the morning of the accident, a pre-flight briefing was conducted by the pilot in command of the accident airplane. According to the pilot-rated passenger of the second airplane in the formation (N141SW): "The briefing included the pertinent radio and formation information for a flight of two, to and from the practice area. Loss of radio was covered. We discussed completing the AMP training from the day before. The pre-flight brief did not include air combat maneuvers, as I remember it." According to a statement provided by the pilot of N141SW, the flight of two airplanes flew to a practice area located near Lake Conroe, approximately 1

Probable cause

The non-compliance with applicable Airworthiness Directives which required wing spar inspections, and the continued operation of the aircraft beyond the compliance time extension granted as per the approved alternate means of compliance (AMOC). Also causal was the operation of the aircraft outside of its flight "G" load limitations. Contributing factors were the misunderstanding between the Federa

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