N53819

Substantial
None

BELLANCA 8GCBC S/N: 201-76

Accident Details

Date
Thursday, June 2, 1994
NTSB Number
ATL94LA112
Location
SUMMERDALE, AL
Event ID
20001206X01427
Coordinates
30.479986, -87.699836
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 FAILURE TO MAINTAIN AIRSPEED DURING TAKEOFF.

Aircraft Information

Registration
Make
BELLANCA
Serial Number
201-76
Engine Type
Reciprocating
Model / ICAO
8GCBC BL8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
3
FAA Model
8GCBC

Registered Owner (Current)

Name
SEEKINS RALPH DBA
Address
1625 SEEKINS FORD DR
City
FAIRBANKS
State / Zip Code
AK 99701-3170
Country
United States

Analysis

On June 2, 1994, at 1715 central daylight time, a Bellanca 8GCBC, N53819, collided with trees and a fence on the departure end of the south runway, during an aborted takeoff attempt from a private airstrip near Summerdale, Alabama. The flight operated under 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage and the pilot was not injured. The accident occurred during the initial takeoff attempt.

During an attempted takeoff, the pilot felt a jerk in the flight controls and elected to abort the takeoff procedure after the airplane was airborne. According to the pilot, the airplane was controllable until the airplane entered a left turn at 40 mph. The airplane collided with a small stand of trees and a fence off the departure end of the runway. Examination of the airplane failed to disclose a mechanical problem. The pilot report that the left aileron push rod was broken and appeared to have jammed the flight controls. The metallurgist factual report of the left aileron push rod assembly stated that the examination of the assembly revealed features typical of a bending overstress, and there was no evidence of preexisting defects (see attached metallurgist's factual report). According to the operator's handbook, the airplane will stall between 51 and 52 mph with normal takeoff flaps and takeoff power; stall airspeed information in a turn was not determined, but typically the stall airspeed in a turn would be higher than 52 mph.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA112