User manual

Aerosoft Wilga X 1.00 Manual
Page 4 of 21
CONSTRUCTION
The PZL-104 I has a high mounted wing that includes slot flap drooped aileron and fixed wing slats. The
fuselage is made up from a semi-monocoque metal frame with partially fabric covered panels. The power plant
consists of the redial reciprocating air-cooled engine АI-14RA with two-blade rotor controllable pitch US -
122000. The twin fuel tanks are in the wings. The cockpit is closed, four-passenger, with dual control, has the
big glass areas for better visibility and has two removable doors. Equipment differs but most aircraft are
equipped with basic navigation and communication radios.
AIRCRAFT DATA
DIMENSIONS
 Length, m 8,1
 Wingspan, m 11,12
 Wing area, m2 15,5
 Height (with antenna), m 2,96
PERFORMANCE
 Maximum speed (low altitude), km/h:
Maximum power 200
Maximum continuous power 185
 Service ceiling, m 4000
 Ferry range (km): 510(Н = 500 m, V = 120 km/h)
 Flight duration(h/min): 4:20(Н = 500 m, V = 120 km/h)
 Liftoff speed, km/h: 90
 Takeoff run, m: 150-160
 Landing speed, km/h: 100
 Rolling distance, m: 220
ENGINE DATA
Engine type: AI-14RA (nine-cylinder, single-row, air-cooled)
 Takeoff output, h.p.: 260-2%
 Rate power, h.p.: 220-2%
 Engine weight, kg: 197+2%
 Tanks capacity, l: 180
 Applied fuel: aviation petrol B-70 or B-91/115
 Oil quantity, l: max16/ min11
 Applied oil: MS-20 or MS-22
PROPELLER DATA
 Prop type: US-122000(two-bladed)
 Prop direction of rotation: left