Pilot Operating Handbook KP-5 ASA
10
1.5 Basic technical data
1.5.1 Technical description
KP-5 is a two-seater, all-metal, self-contained, low-wing aircraft with
side-by-side seats. Supporting surfaces are with two spars. They are
composed of a rectangular center-section and a trapezoidal outer wing
with Fowler flap. The fuselage is of a semi-monocoque construction.
Tail units are self-contained, all metal with a forward HTU. The aircraft
is equiped with the fixed three-wheel undercarriage.
1.5.2 Dimensions of the aircraft
Wing span
Length
Height
Wing area
Depth of the mean aerodynamic chord
Dihedral of the wing
Dihedral of the center section
Dimensions of landing gear tire - nose
- main
Landing gear gauge
Landing gear wheel base
Nose leg tire pressure
Main leg tire pressure
32 ft 5,5 in
23 ft 7,3 in
7 ft 2,6 in
127,5 ft
2
4 ft 2 in
6
o
0
o
300x85 (4")
350x115 (6“)
6 ft 7,7 in
4 ft 11 in
36
±
1,5 psi
36
±
1,5 psi
