N389VV

Substantial
Serious

Hopkins Rutan VariViggenS/N: 389

Accident Details

Date
Wednesday, November 16, 2005
NTSB Number
LAX06CA037
Location
Aguila, AZ
Event ID
20051227X02013
Coordinates
33.919445, -113.167221
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the pilot's failure to maintain an adequate airspeed during landing approach, which resulted in an inadvertent stall. A contributing factor was the pilot's lack of experience in the accident airplane.

Aircraft Information

Registration
N389VV
Make
HOPKINS
Serial Number
389
Engine Type
Reciprocating
Year Built
2004
Model / ICAO
Rutan VariViggenSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HOPKINS MICHAEL P
Address
PO BOX 670
Status
Deregistered
City
AGUILA
State / Zip Code
AZ 85320-0670
Country
United States

Analysis

On November 16, 2005, at 1210 mountain standard time, an amateur-built, experimental Hopkins Rutan VariViggen airplane, N389VV, impacted terrain during landing at the Eagle Roost Airpark in Aguila, Arizona. The private pilot, who was the sole occupant, sustained serious injuries, and the airplane incurred substantial damage. The pilot/owner was operating the airplane under the provisions of 14 CFR Part 91 as an initial test flight. Visual meteorological conditions prevailed, and a flight plan was not filed for the local area flight, which departed the airpark about 25 minutes prior to the accident.

According to the pilot's written account of the event, he was conducting his first test flight in the aircraft after building the canard-wing, pusher-propeller airplane. He considered the winds to be light and variable. He took off, departed the traffic pattern, and conducted the test flight. Upon returning, he set up for landing on runway 35. On the first approach, he believed he was too high and the airplane encountered a "strong gust of wind" from the tail, ballooning the airplane up 40 to 50 feet. He aborted the approach and went around for a second attempt. During the second approach, he extended his downwind leg, and established the airplane on a 9-degree approach angle at 80 miles per hour. He did not make any additional adjustments to the throttle, and "allowed his airspeed to decay to the point that the canard stalled." The right wing dropped and the tip scraped the ground resulting in a cartwheel with the nose of the airplane impacting the ground shortly thereafter.

The airplane sustained substantial damage to the cockpit/cabin area, the canard wing, and the left vertical stabilizer and wing.

The pilot accumulated a total of 83 hours of flight experience, none of which were in the same make and model as the accident airplane. He did not have a current biennial flight review endorsement nor did he have a current medical certificate. He reported that he might have been able to prevent the accident had he hired an experienced test pilot to conduct the flight tests required by the Federal Aviation Administration.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX06CA037