BRINKERHUFF GERALD G Q200 near Holland, MI — 2011-10-06
- Date
- 2011-10-06
- Location
- Holland, MI, USA
- Airport
- BIV
- Aircraft
- BRINKERHUFF GERALD G Q200
- Registration
- N2935R
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Approach
Probable cause
The pilot failed to maintain sufficient altitude during the landing approach, which resulted in the airplane contacting an approach light. Contributing to the accident was the setting sun, which most likely obscured the pilot’s vision.
Contributing factors
Contributing to the accident was the setting sun, which most likely obscured the pilot’s vision.
NTSB narrative
The pilot was landing the airplane when it contacted a 14-foot 8-inch tall approach light stanchion that was located about 460 feet from the approach end of the runway. The airplane crashed and came to rest inverted. Witnesses reported that the airplane appeared to be operating normally as the pilot performed touch-and-go landings before the accident. Another witness reported the airplane was low as it approached the runway on the final approach. The pilot had about 2 hours of flight time in the newly built tandem wing airplane. A postaccident examination of the airplane and engine did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation. The examination found the throttle in the retarded position and noted that its location required the pilot to reach his left hand across his body to control it while his right hand was on the control stick. According to sun and moon data for the day of the accident, the landing approach would have been in the direction of the setting sun, which likely would have obscured the pilot’s vision as he approached the runway, making it difficult to judge the airplane’s height above the ground and clearance from the approach lights.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have aborted landing due to low approach before colliding with the light stanchion.
NTSB coding
Evidence available
- Photos
- 24 docket documents
Docket documents24
- Evidence Control Formform
- Informational Statementsform
- Record Shipment Informationform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Airframe and Engine Log Booksother
- Fuel Logother
- Quickie Instrument and Pitot-Static Installationother
- Sun and Moon Dataother
- Photo 01. Approach Light System.photos
- Photo 02. Approach Light Contacted by N2935R.photos
- Photo 03. View of N2935R.photos
- Photo 04. View of N2935R.photos
- Photo 05. View of N2935R.photos
- Photo 06. Left Forward Wing and Main Gear Covering.photos
- Photo 07. Slash Mark.photos
- Photo 08. Left Forward Wing.photos
- Photo 09. Shoulder Harness Belts.photos
- Photo 10. Throttle and Control Stick.photos
- Photo 11. Propeller.photos
- Photo 12. Elevator Control Rods.photos
- Photo 13. Elevator Torque Rod Lever Arm.photos
- Holland Public Safety - Police Reportreport
- Toxicological Reportreport
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