CFKEZ

Substantial
None

BAMBRICK CORBEN ACE S/N: 0988

Accident Details

Date
Monday, July 11, 1994
NTSB Number
SEA94LA176
Location
ARLINGTON, WA
Event ID
20001206X01875
Coordinates
48.180507, -121.670471
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

FUEL STARVATION DUE TO THE BUILDERS' INADEQUATE DESIGN OF THE FUEL SYSTEM. FACTORS INCLUDE HIGH AMBIENT TEMPERATURES DURING THE CLIMB, AND A FENCE IN THE FIELD WHERE THE FORCED LANDING TOOK PLACE.

Aircraft Information

Registration
CFKEZ
Make
BAMBRICK
Serial Number
0988
Engine Type
None
Model / ICAO
CORBEN ACE FK9
No. of Engines
0

Analysis

On July 10, 1994, about 1835 Pacific daylight time (PDT), a Canadian registered experimental Bambrick Corben Ace, CFKEZ, collided with a fence during a forced landing near Arlington, Washington. The private pilot, who was the sole occupant of the aircraft, was not injured, but the aircraft sustained substantial damage. The personal pleasure flight, which departed Arlington Municipal Airport, Arlington, Washington, about 10 minutes before the accident, was being operated in visual meteorological conditions. The aircraft was on a VFR flight plan en route to Abbotsford, British Columbia, and there was no report of an ELT activation.

According to the pilot, after starting the engine, he taxied his aircraft to the active runway in 95 plus degree heat. He then sat at the end of the runway for at least five minutes waiting for other aircraft to depart from the fly-in he was attending. After his takeoff, the pilot climbed at full power for about eight to ten minutes. While still climbing, the aircraft experienced a loss of power four separate times. The first three times the engine restarted on its own, but after the fourth loss of power, the engine didn't restart.

After the loss of power, the pilot attempted a forced landing in a nearby field. His touchdown was successful, but the field was too small to stop the aircraft prior to impacting a perimeter fence.

According to both the owner/builder and the FAA inspector who responded to the accident, the fuel line in the engine compartment was routed near the exhaust stack, allowing it to absorb excessive heat. They both felt that absorption of this heat, combined with the high ambient air temperature, resulted in vaporization of fuel in the line. The pilot said that he planned to reroute the line to minimize this problem in the future.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA176