PZL-130 Orlik

PZL-130 Orlik
Role trainer
National origin Poland
Manufacturer PZL Warszawa-Okecie
First flight 24 October 1984
Introduction 1994
Primary user Polish Air Force
Number built 50 + 9 prototypes


The PZL 130 Orlik (English: Eaglet) is a Polish turboprop, single engine, two seat trainer.

Development and design

The Orlik was designed by PZL Warszawa-Okecie as a trainer for the Polish Air Force, intended as a replacement for its PZL-110 Kolibers. 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. It was fitted with a low-aspect ratio wing to better simulate the handling characteristics of jet fighters.[1] The aircraft was designed to be powered by a Soviet-designed and built Vedeneyev M14Pm radial engine with the intention of replacing it by a modified Polish built Ivchenko AI-14 engine in production aircraft.[2] The first prototype Orlik flew on 12 October 1984, with a second prototype following in December and a third in January 1985.[2]

While the Polish Air Force planned to power its Orliks with locally produced radial engines, PZL planned a turboprop powered version, the PZL-130T Turbo Orlik for export purposes.[3] The third prototype was therefore re-fitted with a 410 kW (550 shp) Pratt & Whitney PT6A-25P turboprop, flying in this form on 13 July 1986, but was destroyed in a crash in January 1987 while being demonstrated to a representative of the Colombian Air Force.[4] Two further turboprop prototypes followed in 1989 and 1990, powered by a Czech-built 560 kW (750 shp) Walter M-601E and a PT6A-25 as the PZL-130TB and PZL-130TP respectively.[5]

In 1990, development of the piston-engined Orlik was abandoned, as the Polish built radial engines gave insufficient power, with Polish interest switching to the M-601 powered PZL-130TB.[5]

Operational history

Deliveries of PZL-130TBs to Poland started in 1994, with the aircraft equipping the Military Pilot Academy at Dęblin and the 60th Training Air Regiment at Radom. All Polish PZL-130TBs were upgraded to the TC-1 standard type, with better ejection seats and avionics.[6]

Variants

PZL 130 TC-1
PZL-130 TC-2
PZL-130 Orlik
The original aircraft with one Vedeneyev M14Pm 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, zero-zero class ejection seats and modernized avionics
PZL-130TC II Orlik
Variant with Pratt & Whitney Canada PT6A-25C turboprop, added winglets, modernized avionics and changed flight tutor's seat position
PZL-130TC III Orlik
Variant with modernized avionics (for example: added Head-Up Display)

Operators

 Poland

Specifications (PZL-130TC II Orlik)

General characteristics

Performance

Armament

See also

Aircraft of comparable role, configuration and era

References

  1. ↑ Air International October 1985, pp. 167–170.
  2. ↑ 2.0 2.1 Air International October 1985, p.170.
  3. ↑ Air International October 1985, p.172.
  4. ↑ Taylor 1988, pp. 195–196.
  5. ↑ 5.0 5.1 Lambert 1993, p.246.
  6. ↑ Taylor 1999, pp. 48–49.

External links

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