ATL00LA030

NTSB accident investigation · Burak Stanley A XF4 · Brooksville, FL · February 29, 2000

Accident · Minor injuriesLimited investigationFinal report
Date
February 29, 2000, 15:45 local (20:45 UTC)
Place
Brooksville, FL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N9VYBurak Stanley A XF4
Weather
Visual (VMC) · Day
Status
Completed · report December 4, 2000
Report
Approved by Office Director
FAA report
20000229014359A
Case key
48694

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfCruise - normal
Propeller system/drive assembly - failure
Design stress limits of aircraft - exceededOwner/builderCause
Material inadequate,improperOwner/builderCause
In flight collision with terrain/waterEmergency descent/landing

Analysis

Approximately 35 minutes in to the flight, 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. The pilot said , 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. The examination of the wreckage revealed that the Rex Flex Coupling Assembly had failed and that three out of the six Rex Bolts had also failed. 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.

Factual narrative

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.

Aircraft

Registration
N9VY
Reported as
Burak Stanley A XF4
Category
Airplane, amateur-built
Serial number
1973-92
Airframe hours
9
Engine
Lycoming O-320, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Stanley A. Burak
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · September 15, 1999 · 2 hours before
Departed
BKV
Airport
BKV · Hernando County, runway 27, 7,001 × 150 ft, concrete

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Certificates
Airline transport, Flight engineer, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Flight hours
8,866 total · 9 in this make and model · 4,138 as pilot in command · 5 in the last 90 days · 3 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 55 °F
Altimeter
30.00 inHg
Observed at
PIE, 41 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.