Basic Technical Data; Technical Description; Ull Aircraft Dimensions - Skyleader 200 Pilot Operating Handbook

20
2 333 371 B
1.5.

Basic technical data

1.5.1. Technical description

KP-2U (SKYLEADER 200) is a ULL category airplane, two-seater, all-metal, self-supported, low-wing ULL aircraft with
side-by-side seats. Supporting surfaces are with two spars. They are composed of a rectangular centre-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. A three-wheeled undercarriage with a controlled front wheel is retractable.
Maximum takeoff weight is 472,5 kg (1042 lb)

1.5.2. ULL aircraft dimensions

ULL aircraft
Wing span
Lenght
Height
Wing area
Depth of the mean aerodynamic chord
Dihedral of the wing
Dihedral of the centre section
Retractable landing gear
Dimensions of landing gear tyres
Landing gar gaude
Landing gear wheel base
Nose leg tyre pressure
Main leg tyre pressure
KP 2U POH 05/2022
9.9 m 32 ft 5.5 in
7.2 m 23 ft 7.5 in
2.6 m 7 ft 2.6 in
11.85 m2 127.5 sq ft
1.27 m 4 ft 2 in
6° 6°
0° 0°
300x85 mm 4"
1.78 m 5 ft 10.08 in
1.7 m 5 ft 6.93 in
250+/-10 kPa 37+/-1.5 psi
250+/-10 kPa 37+/-1.5 psi