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Aviation safety reports, made easier to study

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NTSB Report

June 30, 1999 · Hiller UH-12ET · N7173F

Williams, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 30, 1999
Injury Outcomes
No injuries (1 uninjured)
Location
Williams, CA
Aircraft
Hiller UH-12ET
Tail Number
N7173F
Operator
Pacific Valley Aviation
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX99LA237

While spraying a rice field the engine suddenly quit. The pilot force landed in the field severing the tail boom. The pilot reported the turbine powered helicopter had been fueled the day before the accident, however, he did not visually confirm it. The aircraft had only flown 0.5 hours during this flight. Examination of the fuel system revealed a broken wire in the fuel quantity indicating system. According to the maintenance manual for this helicopter, the open circuit caused by the wire breakage will cause a fuel quantity indication of 34 gallons when the tank is empty.

NTSB Probable Cause

The pilot's inadequate preflight planning and verification that fuel was available for the intended flight. A factor was the fuel quantity false indication.

Full Narrative

On June 30, 1999, about 0700 hours Pacific daylight time, a Hiller UH-12ET, N7173F, was substantially damaged during a forced landing in a rice field at Williams, California. The commercial pilot was not injured. The helicopter was being operated by Pacific Valley Aviation of Colusa, California, under the provisions of 14 CFR Part 137. A company visual flight plan was filed. Visual meteorological conditions prevailed for the local area agricultural flight, which originated near the field to be sprayed about 0630. The pilot stated that the engine abruptly quit while spraying the rice field and the forced landing resulted in the severing of the tail boom. He reported the turbine powered helicopter had been fueled the day before the accident, however, he did not visually confirm it. He had only flown 0.5 hours during this flight. Subsequent examination of the fuel system revealed a broken wire at the aft liquidometer. According to the UH-12E maintenance manual, an open circuit between pin A of the fuel gauge and pin C of the aft tank liquidometer would cause the gauge to indicate 34 gallons when the tank is empty. The pilot/operator failed to file a Safety Board Pilot Operator Accident Report, form 6120.1/2.

Flight

Event TypeAccident
Event Time07:00 PDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12ET
Tail NumberN7173F
Aircraft CategoryHeli
DamageSubstantial
OperatorPacific Valley Aviation
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 305
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 52 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data