| PZL-104 WILGA
2000
Airframe
All metal construction tail wheel design, high wing monoplane
of STOL capability, spacious 4 place cabin with in-flight
operable, removable doors
Engine
Textron Lycoming 10-540-K1B5 Six Cylinder fuel injected, rated
at 300hp
Propeller
Hartzell-HC-C3YR-1RF/F8068 3-blade constant speed
| Airframe Dimensions |
|
Span |
11.12m |
36.48 ft |
Length |
8.10m |
26.58 ft |
|
Wing Area |
15.00m² |
161.47 ft² |
Doors |
1.5 x 0.9m |
4.92 x 2.95 ft |
|
Fuel |
400 |
105.6 gal |
| Weights |
|
Max. takeoff weight |
1500 kg |
4008 lbs |
Empty weight |
900 kg |
1985 lbs |
|
Useful Load |
600 kg |
1323 lbs |
| Performance |
|
Cruising speed (75%) |
190 km/h |
118 mph |
Stall speed |
89 km/h |
55 mph |
|
Max. speed |
211 km/h |
131 mph |
Max. range |
1500 km |
931.5 mi |
|
Takeoff run |
168 m |
551 ft |
Landing run |
150 m |
492 ft |
|
