Beech 65-A80 N6AQ accident near Midland, Texas

Jul 17, 2008 · NTSB number DFW08CA194 · Final report

Probable cause

The failure of the landing gear retraction/extension mechanism due to it being jammed by displaced sound proofing material.

NTSB analysis

The pilot elected to return to the airport following the display of an unsafe landing gear light. Following a flyby and visual check by the airport's control tower, the pilot proceeded to land. During touchdown the main landing gear collapsed and the airplane's belly sustained structural damage. An examination of the landing gear revealed that the failure was due to sound proofing material being caught in the landing gear retraction/extension mechanism.

Text from the NTSB. Open the NTSB docket for DFW08CA194 for the full record.

Event

Date
Jul 17, 2008
Type
Accident
Place
Midland, Texas
Nearest airport
Midland International (MAF)
Highest injury
None
Weather
Visual (VMC)
Light
Day

Beech 65-A80

N-number
N6AQ
Category
Airplane
Damage
Substantial
Operating rule
Part 135 (charter and commuter)

From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.