Aviation Crash Map

C B Withun T-BIRD II N72145

29 October 1998 · New Haven, Michigan, United States · Fatal

Summary

On 29 October 1998 at about 19:00 local time, a C B Withun T-BIRD II registered N72145 was involved in an accident near New Haven, Michigan, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 19:00
Classification
Accident
Location
New Haven, Michigan, United States
Nearest airport
MacOmb Airport (57D)
Coordinates
42.7303, -82.7898
Aircraft
C B Withun T-BIRD II
Registration
N72145
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Unknown
Phase of flight
Not recorded
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
CHI99LA013

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

the improper installation of the propeller by the owner/pilot- mechanic and the pilot not maintaining the airplane's airspeed while approaching the trees along the airplane's flight path. A factor in this accident was the stall encountered by the pilot.

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

Read the full NTSB narrative

The pilot of the homebuilt experimental airplane advised air traffic that he was doing high speed taxi testing on runway 18. Shortly after making this announcement, a witness said he saw the airplane takeoff downwind on runway 36. Witnesses near the airport said they saw the airplane at a low altitude as it was climbing onto a downwind leg. One witness said the airplane was about 100 to 200-feet above the trees when it suddenly '...dropped nose down into the trees.' The on-scene investigation revealed the pusher propeller had a blade root angle set to 43-degrees at the hub. The propeller manufacturer said the blade angle for the propeller should normally be between seven and 14-degrees at its tip. With a 43-degree angle at the blade's root, the blade's tip angle would be about 20.5-degrees, according to the manufacturer's representative. No anomalies with the engine, airframe or flight control system were observed that would prevent flight.

Quoted verbatim from the NTSB record.

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