N9VY

Substantial
Minor

Burak Stanley A XF4 S/N: 1973-92

Accident Details

Date
Tuesday, February 29, 2000
NTSB Number
ATL00LA030
Location
BROOKSVILLE, FL
Event ID
20001212X20450
Coordinates
28.439104, -82.559631
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The owner/builder's failure to build the airplane within the design stress limits of the drive shaft assembly, that resulted in the failure of the Flex Coupling Retention Bolts.

Aircraft Information

Registration
N9VY
Make
BURAK STANLEY A
Serial Number
1973-92
Engine Type
Reciprocating
Model / ICAO
XF4 SA04
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BURAK STANLEY A
Address
9456 RUBY FALLS CT
Status
Deregistered
City
WEEKI WACHEE
State / Zip Code
FL 34613
Country
United States

Analysis

On February 29, 2000, at 1545 eastern standard time, a Burak XF4, experimental airplane, N9VY, collided with the ground following a loss of propeller thrust at the Brooksville Hernando County Airport in Brooksville, Florida. The personal flight was operated by the pilot under the provisions of Title 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The pilot received minor injuries and the airplane sustained substantial damage. The flight originated from Brooksville Airport, in Brooksville, Florida, at 1500.

According to the pilot, 35 minutes in to the flight, while circling Hernando County Airport, Brooksville, Florida, at 3000 feet, the pilot experienced a loss of propeller thrust. The pilot stated that he heard a loud "bang" from the engine compartment and experienced loss of thrust. The pilot said that the engine tachometer went to redline, and the propeller rpm decreased. According to the pilot, changing the engine rpm did not change the propeller rpm. The pilot declared an emergency and started an emergency descent for a landing on runway 27. As the pilot maneuvered the airplane on the final approach, he cleared a stand of trees on the final approach to runway 27. While on short final to land, the airplane initially collided with the ground short of the runway surface and subsequently came to rest on a taxiway.

According to the pilot, the examination of the wreckage revealed that the Rex Flex Coupling Assembly failed. The Rex Flex Coupling assembly connects the engine to the propeller drive shaft and pusher propeller. The pilot reported that three out of the six Rex Bolts (#16087) failed and one bolt was found with the head sheared off. According to the pilot, he cannot recall the torque applied to the flange assembly during installation nor did he recall the maximum required torque for this installation. The pilot stated that the Flexidyne Drive Shaft was designed for a 100 horse-power engine. The pilot/builder stated that he installed a 150 horse power engine on the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL00LA030