AEROPRAKT AEROPRAKT-32, Руководство по эксплуатации для пилотов

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AEROPRAKT-32 Pilot Operating Handbook A32-240-POH
6
1
General information
1.1 General description of the airplane
AEROPRAKT-32 (A-32) is a two-seat, high-wing strut braced monoplane of "classic"
aerodynamic layout with closed cockpit, non-retractable landing gear with steerable nose
wheel, Rotax-912 engine with tractor three-blade on-ground adjustable pitch propeller.
AEROPRAKT-32 is approved for flying in VFR, simple meteorological conditions.
AEROPRAKT-32 was designed in accordance with the German Airworthiness
Requirements for Three axes standard control Ultra Light Aircraft (LTF-UL
–
Lufttüchtigkeitsforderungen für aerodynamisch gesteuerte Ultraleichtflugzeuge).
1.2 Airplane specifications
Specification US units Metric
Wing span 31 ft 9.45 m
Wing area 138 sq ft 12.83
m²
Length 20 ft 7 in 6.27 m
Height 7 ft 3 in 2.22 m
Wheel base 4 ft 2 in 1.27 m
Wheel track 5 ft 9 in 1.75 m
Gross weight (Maximum Take-Off Weight, MTOW) 992 lb 450 kg
Maximum level speed at sea level, ISA conditions 116.6 kts 216 km/h
Cruising speed (IAS) at 1000 ft, ISA conditions, engine RPM:
3500 54 kts 100 km/h
3800 67 kts 125 km/h
4200 81 kts 150 km/h
4650 94 kts 175 km/h
5150 108 kts 200 km/h
5500 116 kts 215 km/h
Maximum noise level with Kievprop 263 propeller at 500 ft,
ISA conditions 65 dB 65 dB
Range with full tanks (30 min. reserve) at 1000 ft, still air, ISA
conditions, 3 700 RPM 706 nm 1307 km
Best angle of climb speed (V
X
), IAS 43 kts 80 km/h
Best rate of climb speed (V
Y
), IAS 65 kts 120 km/h
Stalling speed at MTOW, flaps up (V
S
), IAS 30 kts 55 km/h
Stalling speed at MTOW, full flaps (V
S0
), IAS 24 kts 45 km/h
Maximum engine power at 5800 RPM (5 minutes limit) 80/100 hp 59.6/73.5 kW
Total fuel capacity (standard tanks) 23.8 US gal 90 l
Usable fuel (standard tanks) 23.3 US gal 88 l
Total fuel capacity (optional tanks) 30.1 US gal 114 l
Usable fuel (optional tanks) 29.6 US gal 112 l
Approved fuel types: unleaded mogas min. RON 95 or avgas 100LL