N42760

Substantial
None

Piper J3C-65 S/N: 15069

Accident Details

Date
Saturday, July 4, 1998
NTSB Number
ATL98LA091
Location
ZELLWOOD, FL
Event ID
20001211X10469
Coordinates
28.730579, -81.598999
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power for undetermined reasons which led to a forced landing and nose over. A factor affecting the severity of the damage was the soft terrain.

Aircraft Information

Registration
Make
PIPER
Serial Number
15069
Engine Type
Reciprocating
Year Built
1945
Model / ICAO
J3C-65 J3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
J3C-65

Registered Owner (Current)

Name
BROWN DAVID K
Address
18227 KILLINTON CT
City
ESTERO
State / Zip Code
FL 33928-9648
Country
United States

Analysis

On July 4, 1998, about 1135 eastern daylight time, a Piper J3C-65, N42760, nosed over during a forced landing near Zellwood, Florida. The airplane was operated by the registered owner under the provisions of Title 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the local, personal flight. There were no injuries to the private pilot, and the airplane was substantially damaged. Origination of the flight was the Bob White Field Airport, Zellwood, Florida, about 1000 on the same day.

According to the pilot, he was conducting touch and go landings at the Bob White Field. Just prior to turning crosswind on the fourth departure, the engine lost power. The pilot applied carburetor heat and full throttle, but the engine continued to lose power until it quit. A forced landing was made in a farm field. The wheels sank into the soft ground, and the airplane nosed over.

After the accident, the engine and fuel were tested. The engine started, ran at a low revolutions per minute (RPM), and was able to produce maximum RPM. The magnetos were checked while the engine was operating, with no discrepancies noted. According to the FAA inspector, there was no problem with the operation of the engine during the test run. There was fuel in the airplane, approximately 3/4 of a tank. It was drained and examined, with no water or sediment found.

The Carburetor Icing Probability Curve was reviewed, and the conditions were on the outside edge of the visible icing curve.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL98LA091