N2364A

Substantial
Serious

Piper PA-38-112S/N: 38-78A0656

Accident Details

Date
Wednesday, June 30, 2004
NTSB Number
NYC04LA154
Location
Lawrenceburg, KY
Event ID
20040714X00970
Coordinates
38.049999, -84.933052
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The pilot's decision to perform a negative g maneuver, which resulted in a loss of engine power due to fuel starvation.

Aircraft Information

Registration
N2364A
Make
PIPER
Serial Number
38-78A0656
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
PA-38-112PA38
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BINGHAM RUSSELL E
Address
779 JANET ST
Status
Deregistered
City
VERSAILLES
State / Zip Code
KY 40383-1005
Country
United States

Analysis

On June 29, 2004, at 2020 eastern daylight time, a Piper PA-38-112, N2364A, was substantially damaged during a forced landing after experiencing a loss of engine power near Lawrenceburg, Kentucky. The certificated private pilot was not injured, and a passenger was seriously injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91.

According to the pilot, the flight departed from the Capitol City Airport, Frankfort, Kentucky, with about 20 gallons of fuel. After the airplane was leveled at 2,500 feet, the pilot demonstrated to the passenger, the effects of G forces. After the demonstration, the pilot reduced power, and a few moments later, the engine lost total power. The pilot unsuccessfully attempted to restart the engine, and performed a forced landing to a field, where the fuselage and wings of the airplane were substantially damaged.

According to the passenger, he informed the pilot that "he didn't want him to do anything that would scare him" during the flight. The pilot then placed a notepad between them, and performed a maneuver that made the notebook float into the air. The engine subsequently quit thereafter.

A Federal Aviation Administration (FAA) inspector test ran the engine after the accident. The engine operated with no abnormalities noted.

According to the PA-38-112 Information Manual, "The shape of the wing fuel tanks is such that in certain maneuvers the fuel may move away from the tank outlet. If the outlet is uncovered, the fuel flow will be interrupted and a temporary loss of power may result. Pilots can prevent inadvertent uncovering of the outlet by avoiding maneuvers which could result in uncovering the outlet."

The PA-38-112 had a maximum capacity of 30 gallons of usable fuel. The airplane did not have a negative load factor, and inverted maneuvers were not approved.

The pilot had accumulated 214 hours of total flight experience, with 3.5 hours in make and model.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC04LA154