EV-97 Eurostar SL Microlight Maintenance Manual GEN/EUR/04 Issue 4
6
2.3
Basic dimensions
Wing span ............................................... 26.57 ft.
8.1m
Wing area ............................................. 105.92 sq. ft. 9.84m
2
MAC ......................................................... 4.10 ft.
1.25m
Wing loading (MTOW, 1030 lb, 472.5 kg) 9.72 lb./sq. ft. 48 kg/m
2
Aileron area .............................................. 2.26 sq. ft. 0.21m
2
Flap area ............................................... 5.60 sq. ft. 0.52m
2
Fuselage length ...................................... 19.62 ft.
5.98m
Fuselage width ......................................... 3.41 ft.
1.04m
Fuselage height ........................................ 7.68 ft.
2.34m
Horizontal Tail Unit (HTU)
Span ......................................................... 8.20 ft.
2.5m
HTU area ................................................ 20.99 sq. ft. 1.95m
2
Elevator area ............................................ 8.61 sq. ft.
0.8m
2
Vertical Tail Unit (VTU)
Height ....................................................... 4.21 ft.
1.28m
VTU area ................................................ 10.93 sq. ft.
1.02m
2
Rudder area .............................................. 4.67 sq. ft.
0.43m
2
Landing gear
Wheel track ............................................... 5.25 ft.
1.6m
Wheel base ............................................... 4.42 ft.
1.35m
Main wheel diameter ................................. 14
in
350mm
Nosewheel diameter ................................. 14
in
350mm
2.4
Weight
Empty weight will vary with selection of options and small manufacturing variations. However there
is a maximum limit to the aircraft’s dry empty weight, as shown below.
Empty weight max.(standard equipment)
290.5kg + 0, - 3%
Maximum Take-off weight
472.5kg
Maximum Landing weight
472.5kg
Max. fuel weight, (standard 65 l fuel tank)
47kg
Maximum weight in Baggage Compartment
15kg
NOTE
Actual empty weight is stated on the placard “LOAD LIMITS,“
located on the instrument panel. Empty weight includes 2.9 litres of unusable
fuel.
2.5
Centre of Gravity
Empty weight CG (standard equipment)
18 ±2% Mean Aerodynamic Chord (MAC)
200 – 250mm AoD
Operating CG
20-34% MAC
250 – 410mm AoD
