P Z L   -   1 3 0   O r l i k

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PZL - 130 Orlik

Construction: PZL-130 Orlik - trainer

Producer: PZL - Warsaw-Okecie

First flight: April 1984

Engine: Motorlet Walter M601T turboprop engine with 560kW of power

Dimensions:

Length: 9.0m

Wingspan: 9.0m

Height: 3.53m

Weight: 1350kg

Max take-off weight: 2700kg

Min. speed: 148km/h

Max speed: 480km/h

Climbing: 17m/s

Max. G-load: +7/-3g

Crew: 2 (student & instructor)

Max combat range: 2300km

Ceiling: 10000m

Fuel: 430l (internal) + 2x150l (external tanks)

Weapon: 6 pylons for external stores (unguided missiles, rocket pods, fuel tanks)

Aerobatic Orlik: the aircrafts used for team aerobatic are exactly the same as the aircrafts in regiment

Orlik in service: 36 aircrafts are used for primary training in the 2-nd Basic Flying Training Center in Radom.

T e a m   m e m b e r s

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Leader Lt. Dariusz Stachurski	Left wing Capt. Artur Bielas	Right wing Capt. Zbigniew Kosterna
Slot Lt.Col. Andrzej Sowa	Left wing Capt. Piotr Jablonski	Right wing Lt. Slawomir Chojnacki
Left wing Lt. Krzysztof Kidacki	Right wing Capt. Olgierd Szerksznis	Slot Capt. Dariusz Stanczyk
Team Commander Lt.Col. Dariusz Kleczaj	Ground co-ordinator Maj. Arkadiusz Lesniewski	Speaker Capt. Dariusz Sarnecki
Spare pilot Lt. Robert Osys