N8323N

Substantial
Serious

Beech V35A S/N: D-8736

Accident Details

Date
Sunday, March 10, 1996
NTSB Number
FTW96LA144
Location
CLINTON, LA
Event ID
20001208X05399
Coordinates
30.860448, -91.009391
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the pilot's improper positioning of the fuel selector which resulted in fuel starvation. Factors were the dark night light condition and the worn spark plugs.

Aircraft Information

Registration
N8323N
Make
BEECH
Serial Number
D-8736
Engine Type
Reciprocating
Model / ICAO
V35A BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
STEWART LINDA C
Address
604 CHEVELLE DRIVE SUITE C
Status
Deregistered
City
BATON ROUGE
State / Zip Code
LA 70806
Country
United States

Analysis

On March 9, 1996, approximately 2355 central standard time, a Beech V35A, N8323N, was substantially damaged during a forced landing near Clinton, Louisiana. The commercial pilot and the passenger sustained serious injuries. The airplane was registered to and operated by a private owner. The Title 14 CFR Part 91 personal flight originated at 2210 in Jackson, Tennessee, and the intended destination was Baton Rouge, Louisiana. Dark night visual meteorological conditions prevailed and an instrument flight plan was filed.

According to the pilot, the airplane was descending through 6,500 feet MSL, and the fuel selector was on the right tank, which was "indicating 1/4 tank," when the engine lost power. He switched to the left tank, which was "showing 1/3 tank," and attempted to restart the engine "several" times without success. A forced landing ensued to a "timbered field" and the airplane touched down with a "heavy vertical impact."

Examination of the airplane by the FAA inspector revealed that the fuel tank selector was in the right tank position. During recovery of the airplane, when the wings were removed from the airplane, the right wing tank was found to be "dry of fuel" and approximately 9 gallons of fuel was drained from the left wing tank.

On March 21, 1996, an engine tear down inspection was performed (report enclosed). All 12 of the Champion RHB32E spark plugs were found to have "excessive plug gap," and a test on 2 of the plugs performed with a spark plug testing machine revealed that the "plugs would not fire over 40 psi of pressure." According to the engine manufacturer, the recommended gap setting for these plugs is .016 to .018 inches and they should spark steadily when tested up to pressures of 115 to 135 psi.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA144