N187ES

Substantial
None

GANSHEIMER EVANS VP2 S/N: VP-2-187

Accident Details

Date
Thursday, February 10, 1994
NTSB Number
LAX94LA118
Location
TUCSON, AZ
Event ID
20001206X00764
Coordinates
32.329223, -111.049980
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the pilot's failure to attain and maintain sufficient flying speed during the first flight test of his experimental homebuilt. A factor in the accident was the pilot's selection of a propeller inadequate for the airframe and engine combination.

Aircraft Information

Registration
N187ES
Make
GANSHEIMER
Serial Number
VP-2-187
Model / ICAO
EVANS VP2

Registered Owner (Historical)

Name
GANSHEIMER EDGAR L
Address
6740 N STARSHINE
Status
Deregistered
City
TUCSON
State / Zip Code
AZ 85741
Country
United States

Analysis

On February 10, 1994, at 1113 mountain standard time, a homebuilt experimental Gansheimer Evans VP2 airplane, N187ES, experienced a thrust deficiency in the takeoff initial climb from runway 6L at Ryan Field, Tucson, Arizona. The aircraft subsequently stalled and mushed into the ground about 300 feet beyond the departure end of the runway. The aircraft was on the first test flight following construction completion and Federal Aviation Administration (FAA) certification in the experimental category. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft incurred substantial damage. The certificated private pilot, the sole occupant, was not injured. The flight was originating at the time of the mishap as a local area test flight.

The pilot reported that the takeoff seemed fine until the aircraft got out of ground effect. The aircraft began oscillating in roll and did not want to climb. The pilot noted that the engine was producing full power throughout the sequence. According to the pilot, the aircraft "mushed back to the ground at 500 feet per minute" and impacted the ground in a slight nose- high attitude about 300 feet off the end of the runway.

The pilot said he believes the roll oscillation was caused by an impending stall buffet and the lack of thrust was due to the propeller being of insufficient size.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX94LA118