19980213001239A

Accident · Substantial damage

FAA accident report · Hiller UH-12E · Chino, CA · February 13, 1998

Date
February 13, 1998 · 11:30 local
Place
Chino, CA
Phase of flight
Low Level Operations
Operating rules
Agricultural (Part 137)
Operator
NHFG
Damage
Substantial damage
Aircraft
N4027Z
NTSB investigation
NTSBLAX98LA089
Reported as
Hiller UH12E
People aboard
1
Fatal injuries
0
Pilot’s flight hours
27,000 total900 in this make and model50 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Lost power on spray run. Landed hard. Engine made 2 loud bangs prior stopping. (.4)during an aerial application flight over an orchard at 40 feet above ground level, the pilot experienced a total loss of engine power. Unable to enter an autorotation due to the low altitude, the pilot landed hard in an open field, and the helicopter was substantially damaged. An examination of the helicopter revealed it was out of fuel. According to the pilot, prior to the mishap the fuel quantity gage had indicated 12 gallons remained in the tank, and evidently the fuel float had become stuck in the tank. The FAA coordinator reported that the conditions which may have produced the discrepancy could not be duplicated during the postimpact testing. 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. (-23)the helicopter was returning to it's tanker truck to refill when the engine lost power. The helicopter was at too low of an altitude to autorotate, so it landed quite hard. There were no reported injuries to the pilot. The helicopter was substantially damaged. No fuel was observed in the fuel tank and there was no leakage on site.

As the FAA filed it

LOST POWER ON SPRAY RUN. LANDED HARD. ENGINE MADE 2 LOUD BANGS PRIOR STOPPING. (.4)DURING AN AERIAL APPLICATION FLIGHT OVER AN ORCHARD AT 40 FEET ABOVE GROUND LEVEL, THE PILOT EXPERIENCED A TOTAL LOSS OF ENGINE POWER. UNABLE TO ENTER AN AUTOROTATION DUE TO THE LOW ALTITUDE, THE PILOT LANDED HARD IN AN OPEN FIELD, AND THE HELICOPTER WAS SUBSTANTIALLY DAMAGED. AN EXAMINATION OF THE HELICOPTER REVEALED IT WAS OUT OF FUEL. ACCORDING TO THE PILOT, PRIOR TO THE MISHAP THE FUEL QUANTITY GAGE HAD INDICATED 12 GALLONS REMAINED IN THE TANK, AND EVIDENTLY THE FUEL FLOAT HAD BECOME STUCK IN THE TANK. THE FAA COORDINATOR REPORTED THAT THE CONDITIONS WHICH MAY HAVE PRODUCED THE DISCREPANCY COULD NOT BE DUPLICATED DURING THE POSTIMPACT TESTING. 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. (-23)THE HELICOPTER WAS RETURNING TO IT'S TANKER TRUCK TO REFILL WHEN THE ENGINE LOST POWER. THE HELICOPTER WAS AT TOO LOW OF AN ALTITUDE TO AUTOROTATE, SO IT LANDED QUITE HARD. THERE WERE NO REPORTED INJURIES TO THE PILOT. THE HELICOPTER WAS SUBSTANTIALLY DAMAGED. NO FUEL WAS OBSERVED IN THE FUEL TANK AND THERE WAS NO LEAKAGE ON SITE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.