19990411035869A

Accident · Destroyed

FAA accident report · Amtr VARI-EZE · Eufaula, AL · April 11, 1999

Date
April 11, 1999 · 14:14 local
Place
Eufaula, AL
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N250GH
NTSB investigation
NTSBMIA99LA122
Reported as
Amtr Varieze
Reported engine
Lycoming O290D2
Fatal injuries
0
Pilot’s flight hours
880 total630 in this make and model6 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) Engine started to sputter and lost power approx. 9 miles from eufala, AL, pilot attempted emergency landing on county road 79. Right wing tip hit power line causing loss of control. Pilot attempted to correct, aircraft hit down on road and abruptly veered to the right. Aircraft continued moving along the shoulder of the road contacting several small trees and brush. Nose and main gears separated from the aircraft along with the right wing. There was also damage to the fuselage and left wing. (.4) while descending to land at the destination airport, the engine lost power. The pilot was able to maintain some engine power by moving the throttle in and out. While attempting a forced landing on a road, the flight encountered a truck and had to pull up. The right wing collided with power lines, the airplane crashed onto the road, slid off the road, and collided with trees. The pilot estimated there was 10 gallons of fuel remaining after the accident. Examination of the carburetor after the accident showed the inlet fuel screen was blocked about 50 percent with fiberglass debris, however there was no evidence of precrash mechanical failure or malfunction of the carburetor. The engine was operated to full power after the accident using the accident carburetor and with the carburetor fuel inlet screen blocked 50 percent. There was no evidence of failure or malfunction of the engine.

As the FAA filed it

(-23) ENGINE STARTED TO SPUTTER AND LOST POWER APPROX. 9 MILES FROM EUFALA, AL, PILOT ATTEMPTED EMERGENCY LANDING ON COUNTY ROAD 79. RIGHT WING TIP HIT POWER LINE CAUSING LOSS OF CONTROL. PILOT ATTEMPTED TO CORRECT, AIRCRAFT HIT DOWN ON ROAD AND ABRUPTLY VEERED TO THE RIGHT. AIRCRAFT CONTINUED MOVING ALONG THE SHOULDER OF THE ROAD CONTACTING SEVERAL SMALL TREES AND BRUSH. NOSE AND MAIN GEARS SEPARATED FROM THE AIRCRAFT ALONG WITH THE RIGHT WING. THERE WAS ALSO DAMAGE TO THE FUSELAGE AND LEFT WING. (.4) WHILE DESCENDING TO LAND AT THE DESTINATION AIRPORT, THE ENGINE LOST POWER. THE PILOT WAS ABLE TO MAINTAIN SOME ENGINE POWER BY MOVING THE THROTTLE IN AND OUT. WHILE ATTEMPTING A FORCED LANDING ON A ROAD, THE FLIGHT ENCOUNTERED A TRUCK AND HAD TO PULL UP. THE RIGHT WING COLLIDED WITH POWER LINES, THE AIRPLANE CRASHED ONTO THE ROAD, SLID OFF THE ROAD, AND COLLIDED WITH TREES. THE PILOT ESTIMATED THERE WAS 10 GALLONS OF FUEL REMAINING AFTER THE ACCIDENT. EXAMINATION OF THE CARBURETOR AFTER THE ACCIDENT SHOWED THE INLET FUEL SCREEN WAS BLOCKED ABOUT 50 PERCENT WITH FIBERGLASS DEBRIS, HOWEVER THERE WAS NO EVIDENCE OF PRECRASH MECHANICAL FAILURE OR MALFUNCTION OF THE CARBURETOR. THE ENGINE WAS OPERATED TO FULL POWER AFTER THE ACCIDENT USING THE ACCIDENT CARBURETOR AND WITH THE CARBURETOR FUEL INLET SCREEN BLOCKED 50 PERCENT. THERE WAS NO EVIDENCE OF FAILURE OR MALFUNCTION OF THE ENGINE.

NTSB investigation

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