PZL-130 Orlik TC I performance and specifications

A two seat primary and advanced military trainer with turboprop engine. It may be also used as a light ground-attack A/c (6 hard points) as well as for patrolling and sports flights. It conforms with FAR 23.

Dimensions:
Span - 9,0 m
Length - 9,0 m
Wing area - 13,0 m
2
Weights:
Max. take off weight - 2700 kg
Aerobatics weight - 2150
Empty weight - 1825 kg
Max. underwing load - 600 kg
Performance:
Cruise speed (H=6000 m) - 450 km/h
Stalling speed - 131 km/h
Max. rate of climb - 13,3 m/s
Max. range - 1062 km
Max. range with additional tanks - 2000 km
Take-off run / Landing run (aerobatics version) - 355/390 m