Last site update: 03-10-2008

 

         

 

  

 

PZL Orlik

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PZL 130TC-1 Turbo Orlik

The PZL-130 Orlik (Spotted Eaglet) is intended to serve  for the full spectrum of civil and military training, ranging from pre-selection to aerobatics, and including air combat, air gunnery, ground attack and reconnaissance.

Construction of four piston-engine prototypes (one-static testing #001) began in 1982. The first flying prototype SP-PCA #002 flew on October 12, 1983. The piston-engined  Orlik was abandoned in 1990.

Turboprop power

The third flying airframe (#004) SP-PCC was re-engined with a Pratt & Whitney  Canada PT6A-25A turboprop engine and reregistered as SP-RCC. It made his maiden flight in this configuration on July 13, 1986, but was lost in a crash on January 20,1987. By mid-1994, nine PZL-130TBs, has been delivered to the Polish Air Force, 45 LED at Radom and 60 LPSz at Deblin. From airframe # 009 the prototype PZL-130TB, aircraft are converted to the PZL-130TC-1 the standard trainer of the Polish Air Force. Now days you can find the PZL-130TC-1 Turbo Orliks by 2.OSL at Radom

Team Orlik

Team Orlik is an demonstration team of the Polish Air Force, the team with five PZL-130TC-1, presented their first show during the International Air Tattoo in July 1998 at Fairford, Great Britain. In 2000 the decision was made to increase the number of aircraft to seven.

 

 

Developing nation: Poland.
Manufacturer/designer: EADS - PZL Warsaw-Okecie.
Production line: Warszawa-Okecie.
Task: Advanced turboprop trainer.
First flight:

- PZL-130 October 12, 1983, SP-PCA.

- PZL-130T September 18, 1991, SP-RCC.

First delivery: mid 1994.
  PZL-130TC-1 Turbo Orlik
Crew: 2.
Ejection seat: Martin Baker.
Wing Span: 9,00 m.
Wing Area: 13 mē.
Length: 9,00 m.
Height: 3,53 m.
Tail plane span: 3,50 m.
Wheelbase: 2,90 m.
Wheel track: 3,10 m.
Engines:

One Pratt & Whitney  Canada PT6A-62 turboprop rated 708 kW.

Propeller: 5 blades.
Weight:

- Empty: 1.600 Kg.

- Internal fuel: 504 liters.

- External fuel: 340 liters.

- Max. payload: 480 Kg.

Max. take off weight: 2.700 Kg.
Max. speed: 501 km/h.
Service ceiling: 10.060 m.
Range:

- range 970  km without drop tanks.

Performance:

- max. rate of climb at sea level 798 m per minute.

- take-off run 222 m at normal take-off weight.

g limits: - 3/+ 6
Underwing hardpoints: 6.
Weapons:

- Zeus 7.26 mm gun pods.

- 57 mm rocket pods.

- 80 mm rocket pods.

- Strela IR-homing AAM's.

- free-fall bombs.

                                                        

  

PZL-130 Orlik operator:

Polish Air Force.

- 2 PZL-130.

- 2 PZL-130T.

- 3 PZL-130TB-1.

- 3 PZL-130TM.

- 40 PZL-130TC-1.

- 1 PZL-130TC-2.

 

 

PZL-130 Orlik written-off by accidents: 

  •     20jan87        004 (SP-RCC)

  •     25jan96        009

  •     09may01       036 w/o?

  •     11oct01        034

  •     05jun02        039

 

 

 

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