Commander Aircraft Company 114-B near Adrian, MI — 2009-10-23
- Date
- 2009-10-23
- Location
- Adrian, MI, USA
- Airport
- KADG
- Aircraft
- Commander Aircraft Company 114-B
- Registration
- N6025U
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Approach
Probable cause
The pilot did not maintain control of the airplane due to spatial disorientation while on an instrument approach in instrument meteorological conditions.
NTSB narrative
The air traffic controller cleared the flight for a non-precision instrument approach and provided vectors to an intermediate fix located on the inbound course for the airport, which was reporting a ceiling of 700 feet above ground level. Radar track data revealed that, as the airplane proceeded on the inbound approach segment from the intermediate fix toward the final approach fix, there were significant heading changes and large altitude fluctuations, including rapid ascents and descents. As the airplane neared the final approach fix, instead of proceeding straight on the inbound course as called for by the approach procedure, it entered a left descending turn during which the rate of descent increased to 3,600 feet per minute. A witness reported hearing an airplane circle above his residence at a low altitude, but was unable to see the airplane due to a low cloud ceiling and limited ground visibility. He subsequently saw the airplane in a descent, about 200 to 300 feet above the ground, when the left wing separated from the fuselage. Another witness reported seeing the airplane rolling clockwise in a 45-degree nose-low descent before the left wing separated from the airplane. Neither witness reported seeing any smoke or fire until after the airplane collided with terrain. The postaccident examination did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. Additionally, the left wing main spar exhibited upward deformation consistent with an overload separation during flight. Pilots are vulnerable to spatial disorientation if they do not properly rely on cockpit instrumentation to maintain basic orientation while operating in instrument meteorological conditions. Because the airplane was in an overcast cloud layer throughout the instrument approach, the pilot lacked a discernible horizon; therefore, he would likely have been susceptible to spatial disorientation. The radar flight path and witness observations were consistent with the pilot becoming spatially disorientated and losing control of the airplane.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot did not request weather briefing before departure.
NTSB coding
Evidence available
- ADS-B / radar
- Photos
- 38 docket documents
Docket documents38
- FAA Air Traffic Control Flight Summaryatc
- FAA Air Traffic Controller Statementatc
- Airplane Information, N6025Uform
- Pilot Information, Eric Beaudryform
- Retention / Release of Wreckage Formform
- Weather Information (KADG)form
- Weather Information (KARB)form
- FAA Inspector Statement, Larry Wardinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- GPS Runway 23 Instrument Approach Procedure (KADG)other
- Weather Briefing and Flight Plan Documentationother
- Photo 01 - Accident Site, Left Wingphotos
- Photo 02 - Accident Site, Wreckage Debris Pathphotos
- Photo 03 - Accident Site, Impact Craterphotos
- Photo 04 - Accident Site, Main Wreckagephotos
- Photo 05 - Accident Site, Main Wreckagephotos
- Photo 06 - Wreckage Layout, Main Cabin and Propellerphotos
- Photo 07 - Wreckage Layout, Left Wingphotos
- Photo 08 - Wreckage Layout, Left Wingphotos
- Photo 09 - Wreckage Layout, Left Main Wing Sparphotos
- Photo 10 - Wreckage Layout, Left Main Wing Sparphotos
- Photo 11 - Wreckage Layout, Empennagephotos
- Photo 12 - Wreckage Layout, Empennagephotos
- Photo 13 - Wreckage Layout, Right Wingphotos
- Photo 14 - Wreckage Layout, Right Wingphotos
- Photo 15 - Recovered Cockpit Instruments and Avionicsphotos
- Photo 16 - Disassembled Electrically-Powered Remote Directional Gyrophotos
- Photo 17 - Disassembled Vacuum-Powered Attitude Indicatorphotos
- Photo 18 - Enginephotos
- Photo 19 - Enginephotos
- Photo 20 - Enginephotos
- Photo 21 - Propeller Bladesphotos
- Radar Data Plotsradar
- Radar Data, Detroit Approach Controlradar
- Radar Data, Toledo Approach Controlradar
- Toxicological Report, Eric Beaudryreport
- Transcript of Voice Transmissions, Toledo Approach Controltranscript
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