N528AB

Substantial
None

bourque experimental KITFOX S/N: 528

Accident Details

Date
Sunday, June 19, 1994
NTSB Number
IAD94LA109
Location
CHESTER, CT
Event ID
20001206X01548
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fracture of the tailwheel assembly for undetermined reasons during the takeoff roll, and the subsequent loss of directional control and collision with a hangar.

Aircraft Information

Registration
N528AB
Make
BOURQUE EXPERIMENTAL
Serial Number
528
Engine Type
None
Model / ICAO
KITFOX FK9
No. of Engines
0

Registered Owner (Historical)

Name
BOURQUE ARCHILLE O
Address
139A BOSTON POST RD PO BOX 472
Status
Deregistered
City
OLD LYME
State / Zip Code
CT 06371
Country
United States

Analysis

History of Flight

On June 19, 1994 about 1055 eastern standard time, an experimental Kitfox II, N528AB collided with a hangar on takeoff at Chester Airport, Chester, Connecticut. The certificated private pilot was not injured and the airplane was substantially damaged. The personal flight was being operated by the pilot/owner. Visual meteorological conditions prevailed. There was no flight plan for the flight being conducted under 14 CFR Part 91.

In the NTSB Form 6120.1/2, the pilot stated,

I was conducting high speed taxi test on runway 35, when the tailwheel holding bracket broke, causing tailwheel to move abruptly to the right, and moving rudder to right, causing aircraft to leave runway, cross grass strip on the right, fly off a 10-foot high earth bank, and on to a hangar door, which stopped the airplane.

The pilot reported the failure of the tailwheel assembly occurred at the weld that attaches the tailwheel spring and fuselage.

The FAA Inspector stated in his report:

...The right main gear was ripped off, and the left main had collapsed. There was substantial damage to both wings...All this aircraft damage seemed consistent with impact. Additionally, I found the tailwheel spring shackle broken. It could not be determined if it was broken prior to impact or if it broke due to an overload when the main gear collapsed. The bottom of the rudder was wrinkled, as if the tailwheel assembly bounced up and struck it. I interviewed the pilot at the scene...[The pilot] stated that he had made the first flight in the aircraft the day before and was intending this, his second flight to be about 2 hours. It would be the first time he had flown the aircraft with full fuel tanks. He taxied out to runway 35 and performed the runup. He said everything appeared normal. He said the wind was down the runway at about 10 knots. After he applied power, he said he felt the tail raise off the runway and settle back down. He said when it came up the second time, he was about 500 [to] 600 feet down the runway. The aircraft veered to the right and ...the left wing came up. He stated it felt like a 45 degree bank to the right. He stated he felt the aircraft was airborne. His best recollection of the airspeed was about 20 knots... .

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD94LA109