Skyleader 600 - Basic technical data

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1.5. Basic technical data
1.5.1. Technical description
SKYLEADER 600 is a LSA category airplane, two-seater, self-contained, low-wing with side-by-side seats. Main
construction of the airplane is metal, consist of duralumin metal sheets. Upper part of a cockpit is made of bre
composite. Wing is composed of arectangular centre-section and a trapezoidal outer wing with Fowler ap. Tail units
are self-contained, all metal with a forward HTU. A three-wheeled undercarriage with a controlled front wheel is xed.
Maximum takeof weight is 600 kg (1320 lbs).
1.5.2. Aircraft dimensions
Wing span
9,9 m 32 ft 5.5 in
Length
7,1 m 23 ft 3.5 in
Height
2,5 m 8 ft 2.4 in
Wing area
11,85 m
2
127.55 sq ft
Depth of MAC
1,27 m 4 ft 2 in
Wing Aspect Ratio
7,78
Dihedral of the centre section
0˚
Dihedral of the wing
6˚