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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 m2 |
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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
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