19990717035079A

Accident · Substantial damage

FAA accident report · Bell 47G-3B-1 · Sour Lake, TX · July 17, 1999

Date
July 17, 1999 · 16:30 local
Place
Sour Lake, TX
Phase of flight
Forced/Precautionary Landing
Operating rules
Agricultural (Part 137)
Operator
ZIOG
Damage
Substantial damage
Aircraft
N4002G
NTSB investigation
NTSBFTW99TA194
Reported as
Bell 47G3B1
Reported engine
Allison T63A700
People aboard
1
Fatal injuries
0
Pilot’s flight hours
11,549 total500 in this make and model170 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.

(.4) The helicopter lost engine power during takeoff due to contaminated fuel. The commercial helicopter pilot stated that the night before the accident flight, the fueling truck, which contained three tanks (one each for water, chemicals, and fuel), was checked. The pilot stated that the fuel appeared `normal' that night. The following day, prior to the accident flight, the helicopter was `refueled without sumping the tanks.' The pilot added that during takeoff, the engine lost power about 50 feet above the ground, at 30 miles per hour. He executed an autorotation to the ground where the main rotor blades impacted the tail boom and the tail rotor blades contacted the ground. The pilot stated that he found 20 gallons of water in the helicopter's fuel tank after the accident. He added that he discovered the fuel truck had a crack in between the water and fuel tanks. Approximately 80 gallons of water had leaked into the truck's fuel tank. The fuel truck was `supposed to have an aqua stop filter installed that will not pump if water is present but the wrong filter was installed.'

As the FAA filed it

(.4) THE HELICOPTER LOST ENGINE POWER DURING TAKEOFF DUE TO CONTAMINATED FUEL. THE COMMERCIAL HELICOPTER PILOT STATED THAT THE NIGHT BEFORE THE ACCIDENT FLIGHT, THE FUELING TRUCK, WHICH CONTAINED THREE TANKS (ONE EACH FOR WATER, CHEMICALS, AND FUEL), WAS CHECKED. THE PILOT STATED THAT THE FUEL APPEARED `NORMAL' THAT NIGHT. THE FOLLOWING DAY, PRIOR TO THE ACCIDENT FLIGHT, THE HELICOPTER WAS `REFUELED WITHOUT SUMPING THE TANKS.' THE PILOT ADDED THAT DURING TAKEOFF, THE ENGINE LOST POWER ABOUT 50 FEET ABOVE THE GROUND, AT 30 MILES PER HOUR. HE EXECUTED AN AUTOROTATION TO THE GROUND WHERE THE MAIN ROTOR BLADES IMPACTED THE TAIL BOOM AND THE TAIL ROTOR BLADES CONTACTED THE GROUND. THE PILOT STATED THAT HE FOUND 20 GALLONS OF WATER IN THE HELICOPTER'S FUEL TANK AFTER THE ACCIDENT. HE ADDED THAT HE DISCOVERED THE FUEL TRUCK HAD A CRACK IN BETWEEN THE WATER AND FUEL TANKS. APPROXIMATELY 80 GALLONS OF WATER HAD LEAKED INTO THE TRUCK'S FUEL TANK. THE FUEL TRUCK WAS `SUPPOSED TO HAVE AN AQUA STOP FILTER INSTALLED THAT WILL NOT PUMP IF WATER IS PRESENT BUT THE WRONG FILTER WAS INSTALLED.'

NTSB investigation

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

Other reports on N4002G · 3

Matched to the same aircraft by N-number and date.