Aviation Crash Map

Debus/Mountain/Bowes DEBUS-CASST-SNOSHOO N102MB

29 May 2005 · Oklahoma City, Oklahoma, United States · Serious injuries

Summary

On 29 May 2005 at about 17:15 local time, a Debus/Mountain/Bowes DEBUS-CASST-SNOSHOO registered N102MB, operated by Steven L Mountain, was involved in an accident near Oklahoma City, Oklahoma, United States. One person was on board and one was seriously 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 17:15
Classification
Accident
Location
Oklahoma City, Oklahoma, United States
Nearest airport
Clarence E Page Muni (F29)
Coordinates
35.4881, -97.8233
Aircraft
Debus/Mountain/Bowes DEBUS-CASST-SNOSHOO
Registration
N102MB
Category
Airplane
Engines
1
Operator
Steven L Mountain
Operating rule
Part 91: General Aviation
Purpose of flight
Air Race/Show
Phase of flight
Not recorded
Route
Oklahoma City → Oklahoma City
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
DFW05LA140

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

The pilot's failure to maintain airspeed which resulted in an inadvertent stall. A contributing factor was the loss of engine power as result of the fracture of the number two piston to crankshaft connecting rod.

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

Read the full NTSB narrative

On the third lap of an International Formula One Air Race the pilot aborted the race and turned south toward the center of the airport after experiencing a complete loss of engine power. The private pilot performed an emergency descent with an intended landing on runway 35R (a 3,502-foot-long and 75-foot wide asphalt/concrete runway). Near the approach end of runway 35R and approximately 50 feet above ground level (agl), the airplane stalled and started to spin to the left. Subsequently, the airplane impacted the edge of runway 35R in a near vertical nose-down attitude before coming to rest in an inverted position. An examination of the modified four-cylinder engine revealed the loss of engine power was due to a fracture of the number two piston to crankshaft connecting rod.

Quoted verbatim from the NTSB record.

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