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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
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                                    | 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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