N3014V

Substantial
None

BEECH 35S/N: D-416

Accident Details

Date
Sunday, September 9, 2012
NTSB Number
CEN12CA625
Location
Geary, OK
Event ID
20120912X50304
Coordinates
35.619445, -98.522499
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The student pilot failed to maintain control of the airplane during a forced landing attempt which resulted in an aerodynamic stall. Contributing to the accident was the instructor pilot's delay in taking control of the airplane and the loss of engine power for undetermined reasons.

Aircraft Information

Registration
N3014V
Make
BEECH
Serial Number
D-416
Engine Type
Reciprocating
Year Built
1947
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HAYNES ROWDY
Address
929 N ELM ST
Status
Deregistered
City
WEATHERFORD
State / Zip Code
OK 73096-5815
Country
United States

Analysis

After an uneventful local instructional flight, the student pilot and instructor pilot were practicing emergency landing procedures. After a missed approach to the private ranch airport, the student attempted a go-around. During the go-around, there was a loss of engine power during the climb and the student pilot tried to set up for an actual emergency landing. While maneuvering the airplane to land, both the instructor pilot and student attempted to trouble shoot and regain engine power by switching fuel tanks attempting a restart. About 20 feet above the runway, the airplane stalled, impacted the runway, and came to a stop in a grassy area to the left of the runway. Both wings sustained substantial damage. After the accident, the student pilot, who owned the airplane, stated that he may have moved the fuel selector lever to the left tank position while he and the instructor were trying to trouble shoot the loss of engine power. The instructor pilot occupied the right seat and would not have been able to see the fuel selector lever position. Postaccident examination of the airplane and engine revealed that both the right main fuel tank and auxiliary fuel tank had usable fuel. The left main fuel tank was empty and was not compromised. The fuel selector lever was found in the left tank position. No evidence of mechanical malfunction or any other preimpact abnormalities were found. Although the loss of engine power could be linked to possible fuel starvation, the cause for the loss of engine power could not be substantiated.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12CA625