Picture yet to be scanned
|
| PZL - 104 Wilga Technical Data | ||
| Length | 8.2 m | ? ft |
| Height | 2.85 m | ? ft |
| Wing span | 11.4 m | ? ft |
| Passanger door width | 1.5 m | ? ft |
| Engine | 2-blade propeller with variable pass, 260 HP engine with 5 cylinders in a star arrangement | |
| Empty Weight | 870 kg | ? lbs |
| Maximum Weight | 1,300 kg | ? lbs |
| Fuel tanks | two fuel tanks in the wings, one near the engine | |
| Main tank capacity | 95 l | ? g |
| Wing fuel tanks capacity | 2x 50 l | ? g |
| Total fuel tanks capacity | 195 l | ? g |
| Fuel | 73, 80, 87, 91, 96 aviation fuel | |
| Oil | 20 l | ? g |
| Fuel consumption | about 15 l/h | ? g/h |
| Maximum speed | 260 km/h | ? knots |
| No-doors optimal jump speed | 110-115 km/h | ? knots |
| No-doors maximum jump speed | 200 km/h | ? knots |
| Maximum Jump Speed (for parachutists) | 180 km/h | ? knots |
The author in a Romanian Airclub An-2, 1999Click on the picture to see the real-size version |
Sorin PZL-104 Wilga page is
1997-2002 by Sorin
A Crâsmarelu from Sorin®Air Group
All rights reserved