TECHNICAL DESCRIPTION, OPERATING, MAINTENANCE AND REPAIR MANUAL
1.5.3 Basic dimensions
Wing
Wing span..…………...………………………………...
9,000 m
Wing area…............................................……………….
10,300 m
2
Wing aspect ratio.........................................……………
7,82
Aerodynamic mean chord ( MAC )……...……………..
1,185 m
Aileron
Aileron span………………………………….…………
1,250 m
Aileron area...………………………………………….. 0,273 m
2
Wing flap
Flap span..………………………………………………
2,280 m
Flap area.………………………………………………..
0,750 m
2
Fuselage
Length..…………………………………………………
6,400 m
Width..…………………………………………………. 1,180 m
Height…...……………………………………………... 2,000 m
Horizontal tail unit
Horizontal tail span…...………………………………...
2,400 m
Horizontal tail area…………………………………….. 1,680 m
2
Elevator area……………...…………………………….
0,500 m
2
Vertical tail unit
Height.…………...………………………………….…. 1,022 m
Vertical tail area ………………………………………..
1,020 m
2
Rudder area………………..……………………………
0,360 m
2
Landing gear
Wheel spacing……………………...…………………...
2,270 m
Wheel base.……………………………………………..
1,490 m
Main wheel diameter ………………………………….. 0,350 m
Nose wheel diameter ………………………………….. 0,320 m
1.5.4 Weights
Empty weight
( with rescue system and standard instrument equipment )
( Model Club/Tow…………………………………..
279/298 kg
( Model Speed………………………………………
299 kg
Maximum take-off weight ……..………………………………………
472,5 kg
Maximum landing weight ……..………………………………………
472,5 kg
Fuel weight ( 75 litres / optional 100,5 / 126 litres …..……… 54/72,3/91kg
Maximum weight in Baggage Compartment………………… 10 kg
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