Aviation Crash Map

Brinker / Garner BI-PLANE N375CB

17 April 2009 · Caldwell, Idaho, United States · No injuries

Summary

On 17 April 2009 at about 18:40 local time, a Brinker / Garner BI-PLANE registered N375CB, operated by Kurt G Becker, was involved in an accident near Caldwell, Idaho, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:40
Classification
Accident
Location
Caldwell, Idaho, United States
Nearest airport
Caldwell Industrial Airport (EUL)
Coordinates
43.6417, -116.6356
Aircraft
Brinker / Garner BI-PLANE
Registration
N375CB
Category
Airplane
Engines
1
Operator
Kurt G Becker
Operating rule
Part 91: General Aviation
Purpose of flight
Flight Test
Phase of flight
Not recorded
Route
Marsing → Caldwell
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR09LA201

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

Loss of control during the landing roll for undetermined reasons.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot reported that during a routine test flight, he felt an abnormal vibration and decided to divert to a nearby airport. After noting the wind conditions, the pilot entered the airport traffic pattern and proceeded to execute a wheel landing in the tailwheel-equipped airplane. As the tailwheel settled onto the runway, the airplane immediately veered to the right. Despite the pilot's control and brake inputs, the airplane continued to veer to the right and exited the runway. Subsequently, the airplane came to rest in a nose-low attitude adjacent to the runway surface. Examination of the airplane by a Federal Aviation Administration inspector revealed that the left and right top and bottom wing assemblies and fuselage were structurally damaged. Flight control continuity was established throughout the airplane to all flight controls. Movement of the tailwheel by hand revealed that it locked into its normal turning radius and subsequently broke free with little pressure. No anomalies could be found with the airframe; however, examination of the runway revealed a black rubber transfer mark with a width corresponding to the width of the airplane's tailwheel. The mark was not linear, but had a zigzag shape consistent with the tailwheel shimmying.

Quoted verbatim from the NTSB record.

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