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The PZL 130 Orlik (Spotted Eagle) is a Polish turboprop, single engine, two seat trainer.
Development
PZL-130 Orlik TC-I of Orlik Aerobatic Team
The Orlik was designed by PZL Warszawa-Okecie as a trainer for the Polish Air Force. It was also designed to meet the American FAR 23 standard. The project was under the supervision of Andrzej Frydrychewicz, head engineer of PZL Warszawa-Okecie. The aircraft was originally designed with the Russian Vedeneyev M-14Pm piston engine but, since PZL-130 was thought to have some attributes of a jet plane, it was replaced by a turboprop engine. The first prototype Orlik flew on the 24 October 1984. In 1986 the Turbo Orlik, with a Pratt & Whitney PT6A-25P turboprop engine was flown for the first time. It was later equipped with the Czech-built Walter M-601E turboprop engine.
Variants
PZL 130TC-1 #049
PZL-130 Orlik
The original aircraft with one Vedeneyev M-14Pm piston engine
PZL-130T Turbo Orlik
Variant with a Pratt & Whitney Canada PT6A-25P turboprop engine
PZL-130TM Orlik
Variant with a Walter M601E turboprop engine
PZL-130TB Orlik
Variant with a Walter M601T turboprop engine
PZL-130TC I Orlik
Variant with added Martin-Baker Mk.11, 0-0 class ejection seats and modernized avionics
PZL-130TC II Orlik
Variant with Pratt & Whitney Canada PT6A-25C turboprop, added winglets, modernized avionics and changed tutor's seat position
PZL-130TC III Orlik
Variant with modernized avionics (for example: added Head-Up Display)
Operators
Poland
* Polish Air Force
[edit] Specifications (PZL-130TC II Orlik)
General characteristics
* Crew: 2: student, instructor
* Length: 9.30 m ()
* Wingspan: 10.00 m ()
* Height: 3.53 m ()
* Wing area: 14.56 m² ()
* Empty weight: 1,825 kg ()
* Loaded weight: 2,400 kg ()
* Max takeoff weight: 2,950 kg ()
* Powerplant: 1× Pratt & Whitney Canada PT6A-25C turboprop, 750 hp ()
Performance
* Maximum speed: 501 km/h
* Range: 2,200 km ()
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