N49309

Substantial
None

AEROTEK PITTS S-1TS/N: 1006

Accident Details

Date
Sunday, December 2, 2012
NTSB Number
WPR13LA063
Location
Billings, MT
Event ID
20121206X82018
Coordinates
45.807498, -108.542778
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 inability to maintain directional control during the landing roll because of the failure of the tailwheel support bracket.

Aircraft Information

Registration
Make
AEROTEK
Serial Number
1006
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
PITTS S-1TAB11
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
PITTS S-1T

Registered Owner (Current)

Name
NEWTON THOMAS L JR
Address
1702 FRANKLIN ST
City
FREDERICKSBURG
State / Zip Code
VA 22401-4508
Country
United States

Analysis

On December 2, 2012, at 1430 mountain standard time, an experimental exhibition AeroTek Pitts S-1T, N49309, experienced a flight control malfunction during the landing flare. The airplane landed hard on runway 28L, and departed the runway surface at the Billings Logan International Airport (BIL), Billings, Montana. After departing the runway surface, the airplane nosed over resulting in substantial damage to the tail section and the top wing. The pilot operated the airplane under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight; he was not injured. Visual meteorological conditions prevailed for the local area flight, and no flight plan had been filed.

The pilot stated that he had taken a 40-minute flight, with no problems encountered, and returned to land at his home airport. Upon touchdown, he was not able to maintain control of the airplane, and as it moved to the left edge of the runway, he added power to abort the landing. The airplane became airborne, and he was cleared to land again on runway 28L. The airplane touched down, and the pilot again was not able to gain control of the airplane. As the airplane moved to the right edge of the runway, the pilot realized he would not be able to abort the landing. The airplane departed the runway surface, something caught in the dirt, and the airplane nosed over. The pilot reported that the weld that attached the tail wheel tube to the fuselage had separated.

A Federal Aviation Administration (FAA) inspector responded to the accident site. During an inspection of the airplane, he noted a broken tail wheel support bracket, which allowed the tail wheel assembly to freely move left and right without corresponding rudder input. The pilot reported to him that the support bracket failure was found when the airplane was still inverted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR13LA063