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Specifications
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Specifications

 

 

Maximum suggested take off weight(aerobatic category)                  1350 lbf/612 Kgf

Maximum  suggested take off weight(normal category)                    1600 lbf/725 Kgf

Baggage load                                                                                   80 lbf/36 Kgf

Recommended powerplant                                                               150 to 200 hp

Used  engine power                                                                                  180 hp

Maximum continuous power                                                                      180 hp

Maximum take off / climb power                                                                210 hp

Wing loading @ 1600 lb / 725 kg                                 16,47 lbf/ft 2 /80,36 Kgf/m 2

Aspect ratio                                                                                                 6.1

Power loading (180 hp)                                                8,89 lbf/hp  /   4,03 kgf/hp

 Fuel Tanks (3)                                                                         61 the Gal/231 l

 

Wing span         24' 4" ft / 7,42 m                 Height                      5' 5" ft / 1,75 m

Length              19' 6"  ft / 5,94 m                 Cockpit width            40" in / 1,02 m

Propeller diameter              74 in                  Wheel tread              6' 10" / 2,06 m

 

Wing area         97.1ft 2 /9,02 m 2                                    Fin area        4,25 ft 2 /0,39 m 2

Flap area             8 ft 2 /0,74 m 2                            Elevator area 6,85 ft 2 /0,64 m 2

Aileron area       4,8 ft 2 /0,45 m 2                           Rudder area  3,72 ft 2 /0,35 m 2

Stabilizer area    10 ft 2 /0,93 m 2

Elevator Compensator area          0,30 ft 2 /0,03 m 2

 

Flap deflection: 40 degrees down

Ailerons deflection: 20 degrees up/15 degrees down

Elevator deflection:  20 degrees up/20 degrees down

Compensator deflection: 20 degrees up/40 degrees down

Rudder deflection: 20 degrees to right/20 degrees to left

 Wing angle of incidence:                               +1,0

Stabilizer angle of incidence:                           -1,5

 Wings wash out:                                           +2,5

Wings dihedral  (external panels):                    +5,0

Airfoil (Modified):                           NACA      64a212(root), 64a210 (tip)

Reference line above  fuselage center line          1  1/4" /  3,175 cm

C. G. limits                                                  16% to  28% of MAC

 

Never exceed speed(V ne , calm air)                             200 kt/370 km/h (IAS)

maximum cruising structural speed (V in )                     170 kt/314 km/h (IAS)

Maximum maneuver speed(VA)                                     130 kt/241 km/h (IAS)

Maximum flap extended speed (V fe )                             87 kt/161 km/h (IAS)

Stall speed / no flap @ 1600 lbf / 725 kgf  (V s )               54 kt/100 km/h (IAS)

Stall speed / full flap@ 1600 lbf / 725 kgf (Vso)                 50 kt/92 km/h (IAS)

 

Maximum structural load factors         +/- 6 g's service        +/- 9 g's ultimate