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PZL-112 Junior performance and specifications
A two seat, low
wing aircraft for basic training including limited
aerobatics and spins. It has been built according
to JAR 23 / FAR 23 and allows IFR flights.
LYCOMING (4 cylinder) 118 HP & fixed pitch HOFFMAN
propeller.
Dimensions:
Span - 8.8
m
Length - 6.5 m
Wing area - 11.44 m2 |
Weights:
MTOW -750
kg
Empty weight - 520 kg |
Performance (estimated):
Cruise
speed (H = 500m) - 190 km/h
Rate of climb (H = 0m) - 3.5 m/s
Max. range - 750 km
Stalling speed - 80 km/h
Service ceiling (theor.) - 4000 m
Take-off run / Landing run - 180 /
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Dimensions:
Span - 8.8
m
Length - 6.5 m
Wing area - 11.44 m2 |
Weights:
MTOW -750
kg
Empty weight - 520 kg |
Performance (estimated):
Cruise
speed (H = 500m) - 190 km/h
Rate of climb (H = 0m) - 3.5 m/s
Max. range - 750 km
Stalling speed - 80 km/h
Service ceiling (theor.) - 4000 m
Take-off run / Landing run - 180 /
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