Comment:
The HP-14 was developed from the HP-13 which was
essentially a HP-11 fuselage with the Wortmann
airfoil used on the HP-12, with extended span.
That wing was later mated to an improved
fuselage to become the HP-14. The ヨ14 used lower
wing loading and reduced aspect ratio in an
attempt to maximize performance in weak
conditions. More than 40 of all versions were
built in the U.S. and by Slingsby in Great
Britain. The ship has appeared with all three
tail styles : the original had the Schreder V-
tail, Slingsby produced the ヨ14C version with 18
m. wing and conventional tail, and the ヨ14T
version used the C wing tieh a T-tail. The
Slingsby HP-14Cメs are ATCメd. The type features a
90 degree landing flap for approach control,
originally operated by a rack and pinion
mechanism. The ヨ14C adopted a rechargeable
pneumatic system to ease aerodynamic operating
loads at high speed. Specifications in
parenthesis are for the HP-14T. As with many
homebuilts, a number of builders have made
design changes to their ships. In some cases
these have been substantial. Andre Krutchkoff
built his SHP-1 with his own design of fuselage
with T-tail. Paul Bikle produced a modified ヨ14
(the T-6) with a 17.37 m./ 57 ft. span wing and
control system modifications. Otto Zauner
constructed an 18 m. model (called the Zauner OZ-
4) which has been modified substantially to have
tip extensions with winglets to give a span of
19.2 m. / 63 ft, and a gross weight of 386 kg./
850 lb.
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