N637KM

Substantial
None

Hampson VELOCITY S/N: DMO-63

Accident Details

Date
Tuesday, August 6, 1996
NTSB Number
MIA96LA205
Location
DUBLIN, GA
Event ID
20001208X06575
Coordinates
32.530178, -82.919563
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

the failure of the exhaust of the cylinder Nos. 2 and 4 at each exhaust flange for undetermined reasons. The unsuitable terrain encountered during the forced landing was a factor.

Aircraft Information

Registration
Make
HAMPSON
Serial Number
DMO-63
Engine Type
Reciprocating
Year Built
1993
Model / ICAO
VELOCITY FEST
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
VELOCITY

Registered Owner (Current)

Name
APPLING JUSTIN
Address
127 HYMAN ST
City
AMARILLO
State / Zip Code
TX 79108
Country
United States

Analysis

On August 6, 1996, about 1820 eastern daylight time, a homebuilt Velocity, N637KM, registered to a private individual, nosed over during a precautionary landing in a field near Dublin, Georgia. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was substantially damaged and the commercial-rated pilot, and two passengers were not injured. The flight originated about 1700 from the Cobb County-McCollum Field Airport, Marietta, Georgia.

The pilot stated to an FAA inspector that en route he first heard engine roughness then observed high oil temperature and experienced momentary binding of the aileron flight controls. The engine began to run rough and the oil temperature reached maximum red line. He initiated a forced landing in a cotton field and after touchdown, the nose gear and a section of the left wing separated. The airplane then nosed over and came to rest inverted.

Examination of the engine by the FAA inspector revealed that the exhaust for the Nos. 2 and 4 cylinders were separated at the flange at each cylinder. The exhaust was manufactured by Velocity using 16 gauge 304 stainless steel purchased by the owner/pilot and was installed about 96 hours earlier. No determination was made as to the reason for the failure of the exhaust.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA205