N9407W

Substantial
None

Piper PA-28-235 S/N: 28-11114

Accident Details

Date
Thursday, June 8, 2000
NTSB Number
FTW00LA202
Location
SUGAR LAND, TX
Event ID
20001212X21241
Coordinates
29.610416, -95.609260
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 improper fuel tank selection, which resulted in fuel starvation. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-11114
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-235 P28B
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-235

Registered Owner (Current)

Name
LOZES JAY P
Address
77065 HIGHWAY 21
City
COVINGTON
State / Zip Code
LA 70435-4009
Country
United States

Analysis

On June 8, 2000, at 1720 central daylight time, a Piper PA-28-235 airplane, N9407W, was substantially damaged when it impacted terrain during a forced landing following a loss of engine power near Sugar Land, Texas. The airplane was registered to a private individual and operated by the pilot. The instrument rated private pilot, who was the sole occupant, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight originated from the Sugar Land Municipal Airport approximately 10 minutes prior to the accident, and was destined for the West Houston Airport, Houston, Texas.

During a telephone interview conducted by the NTSB investigator-in-charge, the pilot reported that he departed the Sugar Land Municipal Airport and the airplane was climbing through 1,500 feet, when the engine "spooled down." The pilot stated that he pushed the engine controls forward and turned on the auxiliary fuel pump; however, he did not detect a change in engine power. The pilot elected to make a forced landing in a field approximately 2 miles from the departure airport. During the landing roll, the left main landing gear impacted an ant hill resulting in the separation of the left main landing gear.

The FAA inspector, who responded to the accident site, stated that he found the fuel selector in the off position. The inspector stated that he found the left auxiliary fuel tank "completely empty," the left and right main fuel tanks full, and the right auxiliary fuel tank containing 3.5 gallons of fuel. The airplane was taken to an aircraft maintenance facility in Houston. The FAA inspector stated that the mechanics test ran the engine on the airplane. The mechanics reported that the engine would not start and run with the left auxiliary fuel tank selected; however, the engine started and ran approximately 15 minutes on each of the remaining fuel tanks. The mechanics also reported that the left wing spar was structurally damaged.

The FAA inspector stated that the pilot indicated that he thought he had taken off with the left main fuel tank selected. The pilot reported that he had a total of 9 flight hours in the accident airplane and 767 total flight hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA202