N90469

Substantial
Minor

HILLER UH-12E S/N: 2358

Accident Details

Date
Wednesday, May 4, 1994
NTSB Number
FTW94LA144
Location
OSAGE, AR
Event ID
20001206X01278
Coordinates
36.290790, -93.290176
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

FUEL EXHAUSTION DUE TO THE PILOT'S FAILURE TO REFUEL AND THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING.

Aircraft Information

Registration
N90469
Make
HILLER
Serial Number
2358
Engine Type
Reciprocating
Model / ICAO
UH-12E UH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
EVERGREEN EQUITY INC
Address
3850 THREE MILE LANE
Status
Deregistered
City
MCMINNVILLE
State / Zip Code
OR 97128
Country
United States

Analysis

On May 4, 1994, at 1830 central daylight time, a Hiller UH-12E helicopter, N90469, was substantially damaged following a loss of engine power near Osage, Arkansas. The airline transport rated pilot sustained minor injuries. Visual meteorological conditions prevailed for the aerial application flight.

According to the operator, the turbine powered helicopter was supporting a gypsy moth eradication program within the Ozark National Forest. The pilot stated that the helicopter was serviced with 100 gallons pesticides and 30 gallons of Jet A fuel for the ninth sortie of the day.

Approximately 45 minutes later, while en route back to the load site, the engine lost power. The pilot stated that he entered autorotation, and the engine auto reignite restarted the engine. The pilot added that he turned towards an open field to make a precautionary landing, and approximately 5 to 8 seconds later, the engine lost power for the second time.

The pilot reentered an autorotation to the heavily wooded area ahead and was able stop all forward motion above the tree tops, settling through the trees. After falling 40 to 50 feet, the helicopter came to rest in the upright position lodged between the tree trunks.

According to the operator, the fuel cell and the fuel lines were not compromised during the crash sequence. No fuel was found in the fuel cell, and there was no evidence of a fuel spill on the ground. According to the engine manufacturer, the average fuel burn rate is 25 to 26 gallons per hour. A successful engine run was accomplished in a test cell, and no anomalies were found with either the fuel control or associated fuel system components.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA144