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Jihlavan will deliver first serial batches of 43 aerospace components (hydraulics, wheels, brakes) for each of 12 L-39NG airplanes of the VIETNAM project. July 2022 Jihlavan will take part in the Farnborough International Air Show (FIA) on 18-22 July 2022 in the form of our own booth within the Czech exposition Older news FREE CAPACITIES
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Jihlavan is a single-source supplier of 14 types of hydraulic safety locks and valves for most Airbus aircraft types. This was one of the pilot projects for the CESA Aero company for BTP supplies for the Airbus supply chain and represents a significant step in fulfilling our long-term business strategy.
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Jihlavan KP-5 Rapid 500 Jihlavan KP-5 Skyleader 500 Jihlavan KP-5 Skyleader 600. Technical Data Wing Span 9.8 Length (m) 7.1 Height (m) 2.5 Take Off Distance (m) 150 Landing Distance (m) 170 Absolute Ceiling (x100ft) 150 Optimum Ceiling (x100ft) 100 Maximum Speed (kts/M) 130 Optimum Speed (kts/M) 100 Fuel Capacity (ltr) 50 MTOW (t)
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Find 2013 Jihlavan SKYLEADER 600 with serial number on Aircraft.com. View photos, ownership, registration history, and more. Aircraft.com …
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Sep 25, 2006 . one is the Jihlavan (pronounced “YEE-la-von”) KP-5, better known to Americans by its importer’s name- Kappa Aircraft KP-5. It is an elegantly styled, all-metal LSA with a high-visibility cockpit, a high-performance wing with well-regarded Fowler flaps, tough trailing link landing gear, and the popular Rotax 912 powerplant. In its ready-to-fly form,
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Jihlavan Aircraft built the Kappa Sova for Kappa 77 from 1997 to 2004 and obtained marketing rights in 2005 when Kappa became insolvent. They became a subsidiary of Skyleader Aircraft in 2008 when the type was redesignated Jihlavan Skyleader. It is an all-metal design apart from a carbon fibre cockpit frame. It has two- spar tapered wings with 6° of dihedral, electrically …
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At a slightly modest 4,900-rpm power setting and at a low altitude, we were indicating 115 to 120 mph. In a timed 1-minute descent rate check with power to idle thrust and best glide speed of 70 Dynon mph, the KP-5 descended 550 feet. Jihlavan developers claimed that with retractable gear and an adjustable prop, the KP-5's glide could be 18:1.
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Max speed 260 km/h Range 1100 km Category UL/LSA Capacity 2 The SKYLEADER is an all metal two-seat, low wing constructed aircraft with a trapezoidal wing. The SKYLEADER is an all metal two-seat, low wing constructed aircraft with a trapezoidal wing.
Jihlavan
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Max speed 265 km/h Range 1600 km Category UL/LSA Capacity 2 The SKYLEADER 600 is an all metal two-seat, low wing constructed aircraft with a trapezoidal wing. The aircraft has a tricycle towed fixed landing gear with wheel pants and a steerable …
Jihlavan
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Jihlavan A.S. CEO, CFO, CTO, CMO Email and Phone Number Jihlavan A.S. employs 18 employees. View
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Specifications Empty weight: 690 lbs (313 kg) MTOW: 1278 lbs (580 kg) Stall speed: 31 kts (36 mph) (57 kph) Cruise speed: 120 kts (138 mph) (222 kph) VNE: 129 kts (148 mph) (239 kph) Engine: Rotax 912 UL (80hp) engine, optionally with Rotax 912 ULS (100hp) or …
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They became a subsidiary of Skyleader Aircraft in 2008 when the type was redesignated Jihlavan Skyleader. It is an all-metal design apart from a carbon fibre cockpit frame. It has two- spar tapered wings with 6° of dihedral , electrically operated Fowler …
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Custom hydraulic devices, systems, construction of hydraulic distributors according to customer requirements, own production of hydraulic products and components. Precision machining, precision parts and components of hydraulic motors, parts for other industries. Aircraft hydraulics, hydraulic instruments and components for aerospace industry.
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THE ENGINE & PROPELLER The airplane is equipped with ROTAX 912 UL (80hp) engine, optionally with ROTAX 912 ULS (100hp) or ROTAX 914 UL (115hp turbo) engine. The engine is attached by welded bed with the use of rubber shock absorbers through the firewall into the fuselage stringers and central tunnel.
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They became a subsidiary of Skyleader Aircraft in 2008 when the type was redesignated Jihlavan Skyleader. It is an all-metal design apart from a carbon fibre cockpit frame. It has two-spar tapered wings with 6° of dihedral, electrically operated Fowler flaps and upturned Küchemann tips. The fin and rudder are swept.
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This ultralight airplane, powered by an unconventional power plant, consisting of a reciprocating internal combustion engine driving the fan, was conceived through the cooperation of the staff and students of the Department of Aerospace Engineering at the Faculty of Mechanical Engineering of the Czech Technical University Prague, and the companies LA composite, s.r.o., and Zall …
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Specifications Empty weight: 622 lbs (282 kg) MTOW: 992 lbs (450 kg) Stall speed: 26 kts (30 mph) (48 kph) Cruise speed: 113 kts (130 mph) (209 kph) VNE: 140 kts (161 mph) (259 kph) Climb: 1280 ft/min (6.5 m/s) Take-off distance: 328 ft (100 m) Landing distance: 459 ft (140 m) Engine: Rotax 912UL Fuel consumption: 4 GPH (15.1 LPH)
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Jihlavan was selected as a partner for the development of hydraulic components, wheels and brakes for the LG B-350 (UAE) military aircraft As part of collaboration, Jihlavan offers free production capacities in its hardening and galvanising rooms and also in the performance of non-destructive tests.
As part of collaboration, Jihlavan offers free production capacities in its hardening and galvanising rooms and also in the performance of non-destructive tests. If interested, please contact the respective workplace (s) and we will provide you with more detailed information.
Jihlavan will take part in the Farnborough International Air Show (FIA) on 20-24 July 2020 Jihlavan was selected as a partner for the development of hydraulic components, wheels and brakes for the LG B-350 (UAE) military aircraft