N8251K

Substantial
None

GRUMMAN ACFT ENG COR-SCHWEIZER G 164BS/N: 634B

Accident Details

Date
Wednesday, September 4, 2013
NTSB Number
CEN13LA551
Location
Clemville, TX
Event ID
20130916X70045
Coordinates
29.046112, -96.116668
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The uncommanded inflight application of parking brake due to a loose valve, which resulted in a noseover during landing.

Aircraft Information

Registration
N8251K
Make
GRUMMAN ACFT ENG COR-SCHWEIZER
Serial Number
634B
Engine Type
Turbo-shaft
Model / ICAO
G 164BG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KINGREY WILLIAM S III
Address
1127 PALMER PL
Status
Deregistered
City
RICHMOND
State / Zip Code
TX 77406-3659
Country
United States

Analysis

On September 4, 2013, about 1400 central daylight time, N8251K, a Grumman Aircraft Engineering Corporation-Schweizer, G-164B, single engine turboprop airplane, was substantially damaged during landing at Hlavinka Ag Strip, Clemville, Texas. The pilot was not injured. The airplane was registered to and operated by Fehmel Planes, Inc.; Bay City, Texas. Day visual meteorological conditions (VMC) prevailed at the time of the accident and a flight plan had not been filed for the 14 Code of Federal Regulations Part 137 agricultural aircraft application flight. The airplane had departed Hlavinka Ag Strip about 1330 for the local flight.

The pilot reported that for several previous several flights his left brake pedal had started to feel "spongy" and that he had to pump the brake pedal while still inflight in order to get adequate brake performance. While inbound for the last landing the pilot again stepped on the brake pedals and the "brakes felt really tight" so he quit applying pressure.

During the landing roll, immediately after touchdown, the tail-wheel equipped airplane slowed quickly, nosed over, impacted terrain and came to rest inverted. The impact resulted in substantial damage to the vertical fin, rudder, both upper wings, and the engine mount.

A postaccident examination of the parking brake valve revealed loose operation which allowed an uncommanded movement of the valve into the locked position.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA551