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ACCIDENTS
A northeastern California VariEze pilot and passenger were
fatally injured when their VariEze crashed into trees on a ridge at 7000 feet. The
aircraft was traveling upslope towards the ridge when it struck the tree tops. The engine
was developing power at the time of impact. No control system failures or airframe
failures were found or suspected, The aircraft had been reported to be flying at extremely
low altitudes earlier.
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A Long-EZ crashed in central California. Both occupants
were fatally injured. The aircraft was observed flying low down a river. As it flew over a
bridge it struck unmarked power lines. The aircraft continued on for about a half mile
where it crashed into trees. No problems were found or suspected with the aircraft.
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A Long-EZ flying over the ocean in Southwestern Florida
crashed into the water. Both occupants were fatally injured. This aircraft was observed by
several eyewitnesses to be flying at cruise speed low across the water, estimates of from
one wingspan to 100 feet above the water. It hit the water and was heavily damaged. The
pilot was found to have a brain tumor and had been experiencing severe headaches. It is
not known however, it there is any connection.
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A VariEze in France took off from the Nice, France airport
with two people aboard. The airplane climbed straight ahead to about 150 AGL turned left,
started loosing altitude while continuing the left turn until it impacted the ground at a
point at about midfield on a heading 1800 opposite the take off heading. We have not had
much information on this, but there is reason to believe that the canopy may have been
unlatched.
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Shortly before this newsletter went to press we began investigating a fatal accident in which a Long-EZ apparently struck the ground in a flat attitude, possibly from a flat spin or deep stall. Of course the results of all testing shows that a Long-EZ is not capable of a flat spin or deep stall, when flown within the allowed limits. Preliminary information shows that the cg may have been behind the aft limit. Even though this aircraft was highly modified, we are concerned that it is possible that others operating near the aft limit and with contour tolerances that degrade flying qualities from the intended and tested configuration, may also be susceptible to spins. At least until this accident is totally investigated and understood we are recommending that the LongEl aft cg limit be moved forward one inch. Also, be sure you follow to the word all information on Pages 44 and 45 of the Owners Manual