DOVA AIRCRAFT DV-1 SKYLARK, Руководство по обслуживанию

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Fuselage:
Length 6,62 m
Width 1,09 m
Height 2,28 m
Wings:
Wingspan 8,14 m
2
Wing surface 9,44 m
Empennage:
2
Horizontal tail surface 1,47 m
2
Vertical tail surface 1,02 m
Undercarriage:
Track 1,70 m
Wheelbase 1,36 m
Empty weight ..................kg ± 2 %
Maximum Take-Off weight 450 kg
Useful load 170 kg
Fuel capacity 90 liters
Maximum baggage weight 20 kg
Maximum loads +4,4 / -2
Stall speed without flaps 79 km/h
Stall speed with flaps 64 km/h
Never exceeded speed 280 km/h
Maximum horizontal speed 240 km/h
Cruise speed 210 km/h
Climb speed 8 m/s
Ceiling 3 650 m
Range (45 min. reserve) 1 200 km
Term of engine overhaul is given as 2000 flight hours or 10 years for ROTAX 912 UL/S
(first reached is valuable). See Rotax Bulletins – operational condition of engine manufacturer
Had to be changed every 5 years:
• air supplying hose for carburetors (AIRBOX)
• all rubber hoses of cooling circuit
1.2. BASIC DIMENSIONS
1.3. WEIGHTS AND PERFORMANCES
1.4. ENGINE LIFETIME
1.5. ENGINE PARTS WITH RESTRICTED LAIFETIME
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