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Randy,
Interesting.
In the pattern, level, lo pwr and dirty, 1.3 x 61=79 KIAS.
A 30 degree banked turn raises the stall speed about 4 kts. Not much of a
margin if operating at or below 85 KIAS.
Engine failure on take off after flaps and gear cleaned up - level flight -
1.3 x 72 = 93 and a 30 degree turn raises that to 98 KIAS. I think that's
why I liked to climb out at an excess of 130 KIAS.
Scott
In a message dated 10/21/2013 11:34:57 A.M. Central Daylight Time,
marv@lancair.net writes:
Posted for "Randy Hartman"
<randy@aoaircrafters.com>:
>Fellow 360 drivers, >
> > > I have over 500 hours on my Lancair 360 (N360DE)
now and just recently did > my first stalls. (I know, I know, I should
have done them a long time ago, > but...) > > >
> Here are the numbers: > > > > Altitude =
8,500, OAT = 65 DF > > > > Clean >
> Power
OFF 72
Kts (right wing > drooping, left wing fall off) >
> Power ON (13"
MAP)
69.5 Kts (slight break/buffet) > > > > Dirty (full
flaps, gear down) >
> Power
OFF 67.8
Kts (slight > break/buffet) >
> Power ON (13"
MAP)
60.8 Kts (slight break/buffet) > > > > Because of
my own personal respect for, and healthy fear of, the airplane > and the
unknown results of stalls in this airplane, I approached the stall >
speeds very slowly and deliberately, taking care to keep the ball
centered. > The numbers taken were at the first, slightest feel of a
stall. I have it > all on video. > > >
> I am wondering what others have experienced. Are these
numbers unusual? > High, low, etc.? > > > >
Points of interest regarding N360DE: > >
. The tail is neither "large"
or "small". It is a one-off > modification that is a little
larger than the original. (Designed and built > by Chuck
Brenner prior to my ownership.) > >
. The flaps are non-standard
for the 360. They are hinged below the > bottom surface of
the wing on three pivot points about 1.25" below. (Also > designed and
built by Chuck Brenner prior to my ownership.) > >
. Cowling has no lower bulge
for the RSA. The RSA is mounted on the > front of the oil
pan. (Cowlings by Chuck Brenner.) > >
. I have 10" stall strips
installed on the leading edge of the wings > about 12" from the side of
the fuselage. > >
. When trimmed up, she flies
extraordinarily stable, the faster the > more stable > >
. Very responsive in pitch,
which I believe is normal for the 360 - > but I have not flown in any
other 360/320/235 > > > > Randy
Hartman > > Alpha Omega Aircrafters > > (319)
360-9775 > > >
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