19980629015249A

Accident · Destroyed

FAA accident report · Amtr Mustangmidgt · Tracy, CA · June 29, 1998

Date
June 29, 1998 · 20:00 local
Place
Tracy, CA
Airport
Tracy Municipal Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N76JF
NTSB investigation
NTSBLAX98FA208
Reported as
Amtr Mustangmidgt
Reported engine
Lycoming O320A3B
People aboard
1
Fatal injuries
1
Pilot’s flight hours
660 total

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. Crashed. Plastic lodged in fuel line. (.4)the experimental airplane was on climbout following a touch-and-go landing. During the climb, the engine began sputtering and lost power. The airplane leveled off momentarily and then began a steep left turn back toward the runway. During the turn, the airplane descended and collided with a power line. The engine had lost power in flight on several prior occasions. The airplane was not equipped with a fuel boost pump or an engine-driven fuel pump. The fuel tank was mounted in the fuselage, immediately forward of the instrument panel with no accumulator tank. The headspace between the fuel tank and the carburetor was reduced whenever the airplane's pitch attitude increased. A minimum of 0.5 pounds of fuel pressure at the carburetor inlet is required for operation of the engine. The minimum flow volume required for engine operation is not specified. The tank had a single, under wing vent line. Dirt and a piece of plastic were found lodged in the 90-degree elbow of the fuel tank vent line at the point where the line enters the tank. The dirt had formed a ball and was located on the tank side of the piece of plastic. The fuel tank was also equipped with a vented fuel cap that was found in place; however, the vent hole in the cap had been covered with gray silicon sealant. (-23) no narrative.

As the FAA filed it

LOST POWER. CRASHED. PLASTIC LODGED IN FUEL LINE. (.4)THE EXPERIMENTAL AIRPLANE WAS ON CLIMBOUT FOLLOWING A TOUCH-AND-GO LANDING. DURING THE CLIMB, THE ENGINE BEGAN SPUTTERING AND LOST POWER. THE AIRPLANE LEVELED OFF MOMENTARILY AND THEN BEGAN A STEEP LEFT TURN BACK TOWARD THE RUNWAY. DURING THE TURN, THE AIRPLANE DESCENDED AND COLLIDED WITH A POWER LINE. THE ENGINE HAD LOST POWER IN FLIGHT ON SEVERAL PRIOR OCCASIONS. THE AIRPLANE WAS NOT EQUIPPED WITH A FUEL BOOST PUMP OR AN ENGINE-DRIVEN FUEL PUMP. THE FUEL TANK WAS MOUNTED IN THE FUSELAGE, IMMEDIATELY FORWARD OF THE INSTRUMENT PANEL WITH NO ACCUMULATOR TANK. THE HEADSPACE BETWEEN THE FUEL TANK AND THE CARBURETOR WAS REDUCED WHENEVER THE AIRPLANE'S PITCH ATTITUDE INCREASED. A MINIMUM OF 0.5 POUNDS OF FUEL PRESSURE AT THE CARBURETOR INLET IS REQUIRED FOR OPERATION OF THE ENGINE. THE MINIMUM FLOW VOLUME REQUIRED FOR ENGINE OPERATION IS NOT SPECIFIED. THE TANK HAD A SINGLE, UNDER WING VENT LINE. DIRT AND A PIECE OF PLASTIC WERE FOUND LODGED IN THE 90-DEGREE ELBOW OF THE FUEL TANK VENT LINE AT THE POINT WHERE THE LINE ENTERS THE TANK. THE DIRT HAD FORMED A BALL AND WAS LOCATED ON THE TANK SIDE OF THE PIECE OF PLASTIC. THE FUEL TANK WAS ALSO EQUIPPED WITH A VENTED FUEL CAP THAT WAS FOUND IN PLACE; HOWEVER, THE VENT HOLE IN THE CAP HAD BEEN COVERED WITH GRAY SILICON SEALANT. (-23) NO NARRATIVE.

NTSB investigation

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