Eiri KY PIK-20 E - Page 52

PIK-20 E Flight manual
A
Fig 7.2: ROT AX 501 Power curve 1 V = 0 km/h Takeoff power
(with propeller) 2 V= 100 km/h
3 V= 150 km/h
4 V = 100 km/h Max continuous
5 V= 100 km/h 75 % power
6 V= 135 km/h
(equals max continuous)
7.2.2 Fuel consumption
1 Take-off power 31.7 kW (43 hp) at 6200 rpm at 100 km/h
22,4 l/h (5.9 gall U.S./h)
2 Max continuous
power (climb) 29.4 kW (40 hp) at 6000 rpm at 100 km/h
22,4 l/h (5.9 gall U.S./h)
3 75 % power (cruise) 22.1 kW (30 hp) at 6000 rpm at 135 km/h
17,2 l/h (4,5 gall U.S./h)
Note: Add 1.0 l/h, if the electric fuel pump is used in flight.
EIRI KY
J
Kisällinkatu 8
SF-15170 Lahti 17
page I -44