Technical data

Power Plant

Engine	Pratt & Whitney PT6-25C turboprop engine (750 SHP)
Propeller	Hartzell D4N-2DX/D9512AX four blade constant speed fully feathering propeller

Dimensions

Wing Span	10.00 m
Length	9.30 m
Height	3.53 m
Wing area	14.56 m²

Weights

Empty weight	1,825 kg
Max. aerobatic weight	2,400 kg
Max. take-off and landing weight	2,950 kg

Performance

(weight 2,400 kg, ISA)

Cruising speed	480 km/h
Rate of climb	14 m/s
Range (full wing tanks, H= 3,000 m)	1,170 km
Range (full wing tanks with full external stores, H= 3,000 m)	2,200 km
Take off run	345 m
Randing run	300 m
Stalling speed	134 km/h
Altitude limits	10,000 m
Temperature limits	-55°C + 45 °C
Loads (g) limits	-3g +6.5g

AIRCRAFT DESCRIPTION

PZL-130TC-II ORLIK MILITARY TRAINER

European Aeronautic Defence and Space Company EADS N.V.
Mendelweg 30 · 2333 CS Leiden · The Netherlands

EADS Deutschland GmbH · 81663 Munich · Germany
EADS France S.A.S. · 37, boulevard de Montmorency · 75781 Paris Cedex 16 · France
EADS CASA · Ava. de Aragón, 404, 28022 Madrid · Spain

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