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Specifications and Performances

SPECIFICATIONSCH601-UL-DRAWING-WEB.jpg

WING SPAN                               8.2 m.

WING AREA                              12 m.sq.

WING AIRFOIL               NACA 65018 mod.

WING CHORD                          124.5 cm.

WING ASPECT RATIO            5.58

HORIZ. TAIL SPAN                  228 cm.

RUDDER TIP HEIGHT (tri)     208 cm.

CABIN TOP HEIGHT              168 cm.

LENGTH                                   580 cm.

CABIN WIDTH                         112 cm

EMPTY WEIGHT                    267 kg.

GROSS WEIGHT                   450 kg.

DESIGN LOAD FACTOR     +/- 6 "G" +/- 6 "G"

FUEL CAPACITY (std)          60.5 litres – (with Optional Wing Tanks 113litres)

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PERFORMANCE                      @ 385 kg          @ 476 kg

TOP SPEED                     205 km/h      205 km/h

CRUISE                           180 km/h     180 km/h

Never exceed speed(Vne)  240 km/h     240 km/h

STALL SPEED                   58 km/h       63 km/h

RATE OF CLIMB                7 m/s          6 m/s

TAKE-OFF ROLL                95 m           115 m

LANDING DISTANCE          120 m         150 m

SERVICE CEILING             3600+ m     3600+ m

RANGE (std.)                   720 km        720 km

RANGE (with wing tanks)   1350 km      1350 km

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25 Years of Quality and Performance!

Roomy cabin. Unmatched visibility.Extended baggage room.

 
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