N84538

Substantial
None

Aeronca 7AC S/N: 7AC-3241

Accident Details

Date
Tuesday, June 25, 1996
NTSB Number
MIA96LA163
Location
CALLAHAN, FL
Event ID
20001208X06069
Coordinates
30.559043, -81.829109
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 premature decision to reduce power, following application of carburetor heat, when engine operation became rougher after experiencing roughness due to carburetor icing. The weather (carburetor icing) conditions and carburetor ice were related factors.

Aircraft Information

Registration
Make
AERONCA
Serial Number
7AC-3241
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
7AC CH7A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
7AC

Registered Owner (Current)

Name
RASER GARY D
Address
36 FLEISHMAN DR
City
BIRDSBORO
State / Zip Code
PA 19508-8407
Country
United States

Analysis

On June 25, 1996, about 1700 eastern daylight time, a Aeronca 7AC, N84538, registered to a private owner, sustained damage when the right main gear collapsed during a forced landing in a field near Callahan, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the commercial-rated pilot was not injured. The flight originated from Jacksonville, Florida, the same day about 1630.

The pilot stated that while in cruise flight at 1,200 feet, the engine began to run rough. The engine oil pressure and oil temperature were normal. He applied carburetor heat and the engine roughness got worse. He immediately selected a field and began his approach to the field for a forced landing. While approaching the field he observed fence posts in his path and extended the approach to avoid them. After touchdown he turned the aircraft to the left in an attempt to spin the aircraft around and stop. The right main landing gear hit something, collapsed, and folded under the aircraft. The aircraft slid to a stop.

After the accident the engine was started in the presence of an FAA inspector and operated to full power with no evidence of failure or malfunction. The carburetor heat operated normally.

Carburetor icing probability curves indicate the aircraft was operating in conditions conducive to visible icing at glide and cruise power at the time of the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA163