N85065

Substantial
None

AERONCA 7CCMS/N: 7AC-3792

Accident Details

Date
Saturday, August 14, 2010
NTSB Number
CEN10LA478
Location
Justin, TX
Event ID
20100814X55122
Coordinates
33.075000, -97.355278
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A loss of engine power due to fuel starvation as a result of the pilot's delay in transferring fuel from the gravity feed wing tanks to the main tank.

Aircraft Information

Registration
Make
AERONCA
Serial Number
7AC-3792
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
7CCMA270
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7CCM

Registered Owner (Current)

Name
WADE TIMOTHY K
Address
1008 DOUGLAS DR
City
ROANOKE
State / Zip Code
TX 76262-4430
Country
United States

Analysis

On August 14, 2010, approximately 1045 central daylight time, an Aeronca 7CCM, N85065, registered to and operated by the pilot, was substantially damaged when it impacted terrain during a forced landing following a loss of engine power near Justin, Texas. Visual meteorological conditions (VMC) prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 without a flight plan. The pilot and passenger on board the airplane were not injured. The local flight originated from Roanoke, Texas, at 1030, and was returning to that airport when the accident occurred.

According to the FAA inspector who went to the scene, the pilot said he had flown over to Prop Wash Airstrip (16X), Justin, where he made a full-stop landing. He taxied back and took off. During climb out, the engine "sputtered" and lost power. The pilot made a forced landing on a grass field near the airstrip. During the landing, the right main collapsed and the right wing and lift strut were bent. The pilot said in his written statement that accident could have been prevented if he had "Start[ed] fuel transfer from gravity feed wing tanks to [the] main tank earlier."

An examination of the airplane showed substantial damage to the right main landing gear, right lower fuselage, right outboard wing and lift strut, and fracture damage to the propeller. Flight control continuity was confirmed. An examination of the engine and other airplane systems revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10LA478