N4027Z

Substantial
None

Hiller UH-12E S/N: 5095

Accident Details

Date
Friday, February 13, 1998
NTSB Number
LAX98LA089
Location
CHICO, CA
Event ID
20001211X09571
Coordinates
39.740684, -121.829193
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Fuel exhaustion due to the pilot's failure to ensure that an adequate fuel supply was onboard. A contributing factor was related to the fuel quantity gage's erroneous indication of fuel.

Aircraft Information

Registration
N4027Z
Make
HILLER
Serial Number
5095
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
UH-12E UH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
MCBAIN CLAY E
Address
435 HELENE ST
Status
Deregistered
City
LEMOORE
State / Zip Code
CA 93245-9133
Country
United States

Analysis

On February 13, 1998, at 1130 hours Pacific standard time, a Hiller UH-12E, N4027Z, owned and operated by Chico Aerial Applicators, Chico, California, experienced a total loss of engine power during an aerial application flight. The pilot reported that he was too low to enter an autorotation, and the helicopter touched down hard in an open field a few miles from the Chico Airport. The helicopter was substantially damaged, and the commercial pilot was not injured. Visual meteorological conditions prevailed. The flight originated from Chico at 1100.

The pilot verbally stated that seconds prior to experiencing the loss of engine power he heard two loud "bang" sounds and then the engine failed. In the pilot's completed report, he reported that the engine lost power at 40 feet above ground level while he was spraying an orchard.

The pilot further reported that an examination of the helicopter revealed it was out of fuel. According to the pilot, prior to and following the mishap, the fuel quantity gage indicated 12 gallons remained in the tank and evidently the fuel float had become stuck in the tank.

According to the Federal Aviation Administration (FAA) coordinator, the fuel tank quantity gage and its associated erroneous reading was examined and the discrepancy that the pilot reportedly observed could not be duplicated during the postimpact examination. The FAA reported that, however, during the examination when the fuel quantity sender arm was manipulated the float could be induced to hang up vertically. Then, when lowered to the bottom of the tank, the fuel quantity would read 12 gallons.

All other system circuitry and component tests were negative. No specific mechanical defect was established.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX98LA089