The PZL-112 Junior was designed by PZL Warszawa-Okecie in collaboration with the Warsaw University of Technology as a low-cost trainer for Polish flying clubs. It was originally known as the Koliber Junior as it used some components from the PZL-110 Koliber.[1] The Junior is a metal low-wing cantilever monoplane with a swept back vertical tail and a small ventral fin.[1] It has a fixed tricycle landing gear and is powered by a nose-mounted Lycoming O-235-L2C flat-four piston engine driving a two-bladed propeller.[1] It has two side-by-side configuration seats in an enclosed cabin with a gull-wing canopy.[1] Construction of the prototype was started in 1997 and it first flew on 17 Jun 2000.[1]
Specificationsedit
Data from Jane's All the World's Aircraft 2003-04[1]
Jackson, Paul, ed. (2003). Jane's All the World's Aircraft 2003-04. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN0-7106-2537-5.
May 12, 2024
junior, eads, polish, single, engine, seat, trainer, built, warszawa, okecie, role, trainer, national, origin, poland, manufacturer, eads, warszawa, okecie, first, flight, 2000, number, built, contents, development, design, specifications, also, references, no. The EADS PZL PZL 112 Junior is a Polish single engine two seat trainer built by PZL Warszawa Okecie 1 PZL 112 Junior Role Trainer National origin Poland Manufacturer EADS PZL Warszawa Okecie First flight 17 Jun 2000 Number built 1 Contents 1 Development and design 2 Specifications 3 See also 4 References 4 1 Notes 4 2 BibliographyDevelopment and design editThe PZL 112 Junior was designed by PZL Warszawa Okecie in collaboration with the Warsaw University of Technology as a low cost trainer for Polish flying clubs It was originally known as the Koliber Junior as it used some components from the PZL 110 Koliber 1 The Junior is a metal low wing cantilever monoplane with a swept back vertical tail and a small ventral fin 1 It has a fixed tricycle landing gear and is powered by a nose mounted Lycoming O 235 L2C flat four piston engine driving a two bladed propeller 1 It has two side by side configuration seats in an enclosed cabin with a gull wing canopy 1 Construction of the prototype was started in 1997 and it first flew on 17 Jun 2000 1 Specifications editData from Jane s All the World s Aircraft 2003 04 1 General characteristicsCrew two Length 6 651 m 21 ft 10 in Wingspan 8 803 m 28 ft 11 in Height 2 625 m 8 ft 7 in Wing area 11 44 m2 123 1 sq ft Empty weight 520 kg 1 146 lb Max takeoff weight 750 kg 1 653 lb Powerplant 1 Lycoming O 235 L2C Flat four piston engine 87 kW 116 hp Propellers 2 bladed Hoffmann HO 14HM 175 131 Performance Maximum speed 210 km h 130 mph 110 kn Cruise speed 97 km h 60 mph 52 kn Stall speed 80 km h 50 mph 43 kn Flaps down Never exceed speed 262 km h 163 mph 141 kn Range 750 km 470 mi 400 nmi Service ceiling 4 000 m 13 000 ft g limits 4 4 1 8 Rate of climb 3 50 m s 689 ft min Wing loading 65 56 kg m2 13 43 lb sq ft See also editRelated development PZL 110 KoliberReferences edit nbsp Wikimedia Commons has media related to PZL aircraft Notes edit a b c d e f g Jackson 2003 pp 333 334 Bibliography edit Jackson Paul ed 2003 Jane s All the World s Aircraft 2003 04 Coulsdon Surrey United Kingdom Jane s Information Group ISBN 0 7106 2537 5 Retrieved from https en wikipedia org w index php title PZL 112 Junior amp oldid 1169471509, wikipedia, wiki, book, books, library,
