Since 1928 we have been pioneers of Polish aerospace.

PORTFOLIO

  • 40 a/c produced in the 1990 in TC-I version
  • 16 a/c TC-II version delivered to PAF with Garmin avionics, new wing, new powerplant.
  • New project – Orlik Multi Purpose Trainer, in consortium with Polish companies (ITWL)
  • Integrated glass cockpit avionic system (mission computer, HUD)
  • Aircraft demonstrator for promotion and commercial purposes.
  • Completing Flight test

Aircraft manufacturing

Production of PZL-130 Orlik – turboprop two-seat aircraft for military pilots training

PZL-130 ORLIK TC-II

Its the first version, PZL-130 TC I, has proven its effectiveness and excellent safety record, responding to the requirements for a basic trainer that enables basic piloting without visibility, aerial navigation and acrobatic. The Polish Air Force counts on 30 of these aircraft
PZL-130 TC II, designed in 2000, incorporates distinctive features from its predecessor (PZL-130 TC I): new wing with winglets and more powerful powerplant with the Pratt & Whitney Canada PT6A-25C and 4-bladed Hartzell. A more reliable and durable aircraft that concludes in a lower cost per hour of training for the operator.

 

PZL 130 TC-II ADVANCED

 

COST-EFFECTIVE SOLUTION TO MAINTAIN TRAINING EXCELLENCE

The PZL-130 ORLIK TC-II basic and advanced packages are adaptable for the most correct and cost-effective transition within any Air Force training system.

 

MAJOR DIMENSIONS

Wing Span:  32 ft 9 in    10.00 m
Wing area:  156.72 ft2   14.56 m2
Length:  31 ft 5in   9.58 m
Height:  11 ft 7 in   3.53 m
Landing Gear Track:  10 ft 2 in   3.10 m
Landing Gear Wheel Base:  7 ft 3 in   2.20 m
Fuselage Width:  2 ft 4 in   0.90 m
Propeller Diameter:  8 ft 0 in   2.44 m

 

VERSATILE AND AFFORDABLE, DESIGNED FOR EFFICIENT TRAINING

For a training system based on one, two or three-steps syllabus, PZL-130 ORLIK TC-II fits more adequately within the scope of training from basic to advanced phases, while offering the highest cost effectiveness to the overall training system.

PZL-130 ORLIK TC-II is designed to create the appropriate experience from initial training phases, transition, instruments, formation, navigation to introduction for combat flights.

ORLIK training system consists of:

PZL-130 ORLIK TC-II ADVANCED aircraft

 

 

 

 

 

PERFORMANCE
Maximum speed:  242 ktas    448 km/h
Stalling speed:  65 ktas   121 km/h
Service ceiling:  26650 ft   8120 m
Maximum range:  700 nm   1290 km
Maximum operating speed:  280 ktas   520km/h
G limits:   +7 to -3

ENGINE
Pratt&Whitney PT6A-25C (559 KW/750 SHP)

COCKPIT
Martin-Baker MkPL11b Ejection Seats
Stepped Tandem Configuration
Ergonomic Design and High Visibility in cockpit

AVIONICS

 

  • Electronic Flight Instruments PFD(1), HSI (2) with doubled AHRS platforms
  • GPS/VOR/ILS/GS (3) navigation system
  • Mode S Transponder (4) ADS-B out/in (Optionally IFF) with Traffic Awareness System (5)
  • A/C Warning Panel (6) with Master Warning (7)
  • VHF Communication Radio System118 to 151MHz (8)
  • Speed (9) Altitude (10) Climb(11) G (12) Radio Altimeter (13), DME (14), ADF (15) ILS (16) MB (17) Engine Instruments (18)

 

Flight Simulator

  • 180 x 80 deg field of view dome projection system
  • flight controls loads simulation and seat vibration included
  • double operator station for formation flight training

 

Egress Procedure Trainer

  • Ejection training with 3.5 G ejection simulation on real MB seat

 

Computer Based Training

  • For pilots
  • For maintenance staff

Maximum speed:  242 ktas    448 km/h
Stalling speed:  65 ktas   121 km/h
Service ceiling:  26650 ft   8120 m
Maximum range:  700 nm   1290 km
Maximum operating speed:  280 ktas   520km/h
G limits:   +7 to -3

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