[{"@context":"http:\/\/schema.org\/","@type":"BlogPosting","@id":"https:\/\/wiki.edu.vn\/en\/wiki24\/pzl-130-orlik-wikipedia\/#BlogPosting","mainEntityOfPage":"https:\/\/wiki.edu.vn\/en\/wiki24\/pzl-130-orlik-wikipedia\/","headline":"PZL-130 Orlik – Wikipedia","name":"PZL-130 Orlik – Wikipedia","description":"From Wikipedia, the free encyclopedia Trainer aircraft The PZL 130 Orlik (English: Eaglet) is a Polish turboprop, single engine, two","datePublished":"2016-06-15","dateModified":"2016-06-15","author":{"@type":"Person","@id":"https:\/\/wiki.edu.vn\/en\/wiki24\/author\/lordneo\/#Person","name":"lordneo","url":"https:\/\/wiki.edu.vn\/en\/wiki24\/author\/lordneo\/","image":{"@type":"ImageObject","@id":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","url":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","height":96,"width":96}},"publisher":{"@type":"Organization","name":"Enzyklop\u00e4die","logo":{"@type":"ImageObject","@id":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","url":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","width":600,"height":60}},"image":{"@type":"ImageObject","@id":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/1\/10\/PZL-130TC-1_Orlik_044_%2811738108953%29.jpg\/220px-PZL-130TC-1_Orlik_044_%2811738108953%29.jpg","url":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/1\/10\/PZL-130TC-1_Orlik_044_%2811738108953%29.jpg\/220px-PZL-130TC-1_Orlik_044_%2811738108953%29.jpg","height":"147","width":"220"},"url":"https:\/\/wiki.edu.vn\/en\/wiki24\/pzl-130-orlik-wikipedia\/","about":["Wiki"],"wordCount":1755,"articleBody":"From Wikipedia, the free encyclopediaTrainer aircraftThe PZL 130 Orlik (English: Eaglet) is a Polish turboprop, single engine, two seat trainer aircraft.Table of ContentsDevelopment and design[edit]Operational history[edit]Variants[edit]Operators[edit]Specifications (PZL-130TC II Orlik)[edit]See also[edit]References[edit]External links[edit]Development and design[edit]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 US 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\u00a0kW (550\u00a0shp) 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\u00a0kW (750\u00a0shp) 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[edit]Deliveries of PZL-130TBs to Poland started in 1994, with the aircraft equipping the Military Pilot Academy at D\u0119blin 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[edit]    PZL-130 OrlikThe original aircraft with one Vedeneyev M14Pm piston enginePZL-130T Turbo OrlikVariant with a Pratt & Whitney Canada PT6A-25P turboprop enginePZL-130TM OrlikVariant with a Walter M601E turboprop enginePZL-130TB OrlikVariant with a Walter M601T turboprop enginePZL-130TC I OrlikVariant with added Martin-Baker Mk.11, zero-zero class ejection seats and modernized avionicsPZL-130TC II Orlik (Garmin)Variant with Pratt & Whitney Canada PT6A-25C turboprop, added winglets, modernized Garmin avionics and changed flight tutor’s seat position[7]PZL-130TC II Orlik (GC)Variant with glass cockpit and Head-Up Display, company name is Orlik MPT (Multi Purpose Trainer).[8]Operators[edit]\u00a0PolandSpecifications (PZL-130TC II Orlik)[edit]General characteristicsCrew: 2Length: 9.3\u00a0m (30\u00a0ft 6\u00a0in)Wingspan: 10\u00a0m (32\u00a0ft 10\u00a0in)Height: 3.53\u00a0m (11\u00a0ft 7\u00a0in)Wing area: 14.56\u00a0m2 (156.7\u00a0sq\u00a0ft)Empty weight: 1,825\u00a0kg (4,023\u00a0lb)Gross weight: 2,400\u00a0kg (5,291\u00a0lb)Max takeoff weight: 2,950\u00a0kg (6,504\u00a0lb)Powerplant: 1 \u00d7 Pratt & Whitney Canada PT6A-25C turboprop, 560\u00a0kW (750\u00a0shp)PerformanceMaximum speed: 550\u00a0km\/h (340\u00a0mph, 300\u00a0kn)Cruise speed: 490\u00a0km\/h (300\u00a0mph, 260\u00a0kn)Range: 2,200\u00a0km (1,400\u00a0mi, 1,200\u00a0nmi)Service ceiling: 10,000\u00a0m (33,000\u00a0ft)Rate of climb: 14.4\u00a0m\/s (2,830\u00a0ft\/min)ArmamentHardpoints: 6 with a capacity of 700\u00a0kg (1,500\u00a0lb)See also[edit]Aircraft of comparable role, configuration, and era^ Air International October 1985, pp. 167\u2013170.^ a b Air International October 1985, p.170.^ Air International October 1985, p.172.^ Taylor 1988, pp. 195\u2013196.^ a b Lambert 1993, p.246.^ Taylor 1999, pp. 48\u201349.^ Orlik z Garminem 22 September 2010. (in Polish)^ Prezentacja Orlika MPT. 7 March 2014. (in Polish)References[edit]Lambert, Mark. Jane’s All The World’s Aircraft 1993\u201394. Coulsdon, UK:Jane’s Data Division, 1993. ISBN\u00a00-7106-1066-1.“Orlik\u2026A Polish Fledgeling”. Air International, October 1985, Vol 29 No 4. pp.\u00a0167\u2013172. ISSN 0306-5634.Taylor, John W. R.  Jane’s All The World’s Aircraft 1988\u201389. Coulsdon, UK:Jane’s Defence Data, 1988. ISBN\u00a00-7106-0867-5.Taylor, Michael J.H. Brassey’s World Aircraft & Systems Directory 1999\/2000. London: Brassey’s, 1999. ISBN\u00a01-85753-245-7.External links[edit]  "},{"@context":"http:\/\/schema.org\/","@type":"BreadcrumbList","itemListElement":[{"@type":"ListItem","position":1,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki24\/#breadcrumbitem","name":"Enzyklop\u00e4die"}},{"@type":"ListItem","position":2,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki24\/pzl-130-orlik-wikipedia\/#breadcrumbitem","name":"PZL-130 Orlik – Wikipedia"}}]}]