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 m
2
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 /

Dimensions:
Span - 8.8 m
Length - 6.5 m
Wing area - 11.44 m
2

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 /