N333HT

Substantial
None

Bellanca 8GCBC S/N: 333-80

Accident Details

Date
Friday, April 18, 1997
NTSB Number
ANC97LA057
Location
PALMER, AK
Event ID
20001208X07647
Coordinates
61.619369, -148.980087
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the pilot's inadequate preflight, and a foreign object (can) that became jammed under the rudder pedal, which resulted in an inadvertent activation of the right brake.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
333-80
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
8GCBC BL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
8GCBC

Registered Owner (Current)

Name
TIERNAN BARTON M
Address
611 TIMBERLANE CIR
City
ANCHORAGE
State / Zip Code
AK 99515-3391
Country
United States

Analysis

On April 17, 1997, about 1940 Alaska daylight time, a tundra tire equipped Bellanca 8GCBC, N333HT, crashed during landing in a remote area, about 22 miles southeast of Palmer, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight when the accident occurred. The airplane, registered to and operated by the pilot, sustained substantial damage. The certificated private pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. The flight originated at the Merrill Field Airport, Anchorage, Alaska, about 1855.

On April 21, 1997, at 0840, the pilot reported in a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), that he was landing on a 900 foot long gravel area, located near Lake George, Alaska, and the Knick Glacier. He had landed at that location numerous times, and at the time of the accident, the wind conditions were calm. The pilot landed toward the south and just after touchdown, he applied right rudder pressure. The airplane began to skid on the gravel surface, and then nosed over. The airplane received damage to the right wing tip, the left wing lift strut, the vertical stabilizer, and the rudder. After the airplane was turned back over onto its landing gear, a can of spray wax was observed lodged under the right rudder pedal. The pilot indicated that when he applied right rudder pressure, the wedged spray can allowed the rudder pedal to pivot forward, and activate the right toe brake.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC97LA057