20051019032359A

Accident · Substantial damage

FAA accident report · Amtr GLASTAR · Summersville, WV · October 19, 2005

Date
October 19, 2005 · 14:30 local
Place
Summersville, WV
Airport
Summersville Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N722W
NTSB investigation
NTSBNYC06CA012
Reported as
Amtr Glastar
Reported engine
Lycoming O320*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
700 total44 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.

(-23) During cruise flight the engine quit suddenly and unexpectedly. The pilot applied carburetor heat, checked his fuel gauge, which showed 5 PSI and turned on the electric fuel pump and switched to another fuel tank. All had no effect. The pilot found the Summersville Airport on his GPS and changed direction towards that airport. The pilot was able to maintain 2000 RPM on the engine by pumping the primer handle in and out. The pilot landed the aircraft long and fast and was unable to stop the aircraft from traveling past the end of the runway and sliding down a hill where it flipped over and came to rest near the airport perimeter chain link fence. Fuel pressure was found to the carburetor inlet. The inlet screen was clear. The float bowl was full of fuel but there was a piece of black material in the float bowl. The accelerator pump functioned normally. When the carburetor was disassembled and the float actuated and released, the needle valve did not return to the open position. Air could not be forced through the carburetor after the needle valve stuck in the closed position. No debris, scoring or burrs were found on the needle or needle seat. After several actuations of the needle valve it would no longer get stuck.

As the FAA filed it

(-23) DURING CRUISE FLIGHT THE ENGINE QUIT SUDDENLY AND UNEXPECTEDLY. THE PILOT APPLIED CARBURETOR HEAT, CHECKED HIS FUEL GAUGE, WHICH SHOWED 5 PSI AND TURNED ON THE ELECTRIC FUEL PUMP AND SWITCHED TO ANOTHER FUEL TANK. ALL HAD NO EFFECT. THE PILOT FOUND THE SUMMERSVILLE AIRPORT ON HIS GPS AND CHANGED DIRECTION TOWARDS THAT AIRPORT. THE PILOT WAS ABLE TO MAINTAIN 2000 RPM ON THE ENGINE BY PUMPING THE PRIMER HANDLE IN AND OUT. THE PILOT LANDED THE AIRCRAFT LONG AND FAST AND WAS UNABLE TO STOP THE AIRCRAFT FROM TRAVELING PAST THE END OF THE RUNWAY AND SLIDING DOWN A HILL WHERE IT FLIPPED OVER AND CAME TO REST NEAR THE AIRPORT PERIMETER CHAIN LINK FENCE. FUEL PRESSURE WAS FOUND TO THE CARBURETOR INLET. THE INLET SCREEN WAS CLEAR. THE FLOAT BOWL WAS FULL OF FUEL BUT THERE WAS A PIECE OF BLACK MATERIAL IN THE FLOAT BOWL. THE ACCELERATOR PUMP FUNCTIONED NORMALLY. WHEN THE CARBURETOR WAS DISASSEMBLED AND THE FLOAT ACTUATED AND RELEASED, THE NEEDLE VALVE DID NOT RETURN TO THE OPEN POSITION. AIR COULD NOT BE FORCED THROUGH THE CARBURETOR AFTER THE NEEDLE VALVE STUCK IN THE CLOSED POSITION. NO DEBRIS, SCORING OR BURRS WERE FOUND ON THE NEEDLE OR NEEDLE SEAT. AFTER SEVERAL ACTUATIONS OF THE NEEDLE VALVE IT WOULD NO LONGER GET STUCK.

NTSB investigation

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