Hi Denis,
Just thought I would touch bases with you to see if
you had gone ahead with that engine. We had one show up yesterday from Washington, jogged our memory about yours. Any
news??
<Marv>
Posted for "Conkey, Denis" <dconkey@roadrunner.com>:
I've had a
couple of inquires about why this airplane flamed out and some of the particulars of the accident. I won't provide names, but this
is what I know, albeit second hand. About December of last year, the airplane was being test flown by
an accomplished Lancair IV Turbine pilot out of Camarillo, CA. The aircraft was beginning its fourth flight and it had
flown well up to this point. This flight was going to be up to 25,000 feet to check the pressurization. Just after takeoff, the
tower called out some traffic and the pilot pitched the airplane up and to the right in the climb out. The engine then
quite (flamed out) at about 800 ft. The pilot turned back toward the runway and S-turned to lose altitude as
he was now landing opposite direction to takeoff. The pilot touched down at Bravo which I think is about 1,500 ft from
the end of the runway and I'm sure he had some knots on the airplane. Camarillo has about 3,000 ft of overrun, but it is
commonly blocked off for police training and other activity that is conducted in the overrun area (subject of a long discussion that
I won't get into here). The pilot did not think he could get the airplane stopped before the barriers and chose to leave
some speed on the aircraft and hopped the barriers and landed in the overrun. Unfortunately this maneuver chewed up some
overrun distance and there is a Convair CV-240 (guessing at type) parked at the end of the overrun near the fence. The pilot had
stomped on the breaks as evidenced by one of the tires being flat sided, but decided he would not get it fully stopped before
reaching the Convair so he maneuvered to the left and this is when the left gear dug into some soft dirt on the side of the overrun
and the airplane flipped on its back. Estimates of speed when this happened were 30-40 kts. As I said, this is
not firsthand knowledge and there may be some inaccuracies in the story, but I think it's close. As for the reason for the
flameout, here is what I know of the system design. Fuel is put into the wings and it then flows into the belly tank. Fuel from
the engine is fed from the belly tank through an accumulator that was located in the baggage compartment. Obviously, we will
redesign the fuel system. Most of the data I've picked up so far points to having the fuel come from the wings to an
accumulator/tank that is near the engine. This seems to make sense to me. Comments
welcome. Denis 805-402-6197 N102M/N750PJ -- For archives and unsub
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