N930TG

Substantial
None

de Havilland DHC-2S/N: 1041

Accident Details

Date
Wednesday, June 25, 2003
NTSB Number
ANC03CA088
Location
Iliamna, AK
Event ID
20030912X01530
Coordinates
59.756389, -154.901672
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 incorrect selection of the fuel selector valve position during takeoff which resulted in fuel starvation. A factor associated with the accident was inadequate transition training provided to the pilot by the company/operator management.

Aircraft Information

Registration
N930TG
Make
DE HAVILLAND
Serial Number
1041
Engine Type
Turbo-shaft
Year Built
1957
Model / ICAO
DHC-2DH2T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RDM PILOT/GUIDE LTD
Address
4743 NORTH TONGASS HWY
Status
Deregistered
City
KETCHIKAN
State / Zip Code
AK 99901
Country
United States

Analysis

On June 25, 2003, about 1530 Alaska daylight time, a float-equipped de Havilland DHC-2 airplane, N930TG, sustained substantial damage when it collided with a gravel-covered road following a loss of engine power on takeoff from a lake located adjacent to the Iliaska Lodge, Iliamna, Alaska. The airplane was being operated by Iliaska Lodge as a visual flight rules (VFR) business flight under Title 14, CFR Part 91, when the accident occurred. The solo commercial certificated pilot was not injured. Visual meteorological conditions prevailed, and a VFR flight plan was in effect. The flight originated at the accident lake, about 1525.

During a telephone conversation with a National Transportation Safety Board investigator on August 4, the pilot reported that he was positioning the airplane in order to pick up a group of passengers who were clients of Iliaska Lodge. He said that this was the first time he had been assigned to fly the accident airplane, and that the airplane's main fuel valve was different than that of any other DHC-2 he had previously flown. The pilot stated that prior to takeoff, he placed the fuel selector valve in the "up" position, believing he had selected the center fuel tank. Just after takeoff, as the airplane climbed to about 30 feet above the water, the engine lost all power, and the airplane descended and struck a gravel-covered road at the departure end of the lake. The airplane sustained substantial damage to the fuselage.

The pilot noted that a postaccident inspection of the airplane revealed that when he placed the fuel valve in the "up" position, he inadvertently selected the "off" position. The pilot added that the operator did not inform him of the differences associated with the accident airplane's fuel valve.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC03CA088