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| {{Unreferenced|date=June 2012}}
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| {|{{Infobox Aircraft Begin
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| |name = Puma
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| |logo = <!--ONLY for an individual logo of the aircraft model, (NOT the main manufacturer logo)-->
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| |image = Puma_niebo_01.jpg
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| |caption = <!--image caption; if it isn't descriptive it should be left blank-->
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| }}{{Infobox Aircraft Type
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| |type = [[ultralight]]
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| |manufacturer = [[Aero-service|Aero-service Jacek Skopiński]]
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| |designer = Jan Fiala
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| |first flight = <!-->
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| |introduction = <!--date the aircraft entered or will enter military or revenue service-->
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| |retired = <!--date the aircraft left military or revenue service. If vague or multiples, it probably should be skipped-->
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| |status = <!--in most cases, this field is redundant; use it sparingly-->
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| |primary user = <!-->
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| |more users = <!-->
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| |produced = 2010-
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| |number built = <!-->
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| |program cost= <!-- total program cost. -->
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| |unit cost = <!-- incremental or flyaway cost for military aircraft or retail price for commercial aircraft. -->
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| |developed from = <!-->
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| |variants with their own articles = <!-- variants OF the topic type -->
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| }}
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| |}
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| The '''Puma''' is a two-seater [[ultralight]] manufactured by [[Aero-service|Aero-service Jacek Skopiński]].
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| ==Design==
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| The Puma is a single engine, two-seater, low-wing ultralight with classically arranged tail and tricycle retractable landing gear. The trapezoidal wing has one main and one secondary [[Spar (aviation)|spar]]. The aircraft can be fitted with the [[Rotax 912]] or [[Rotax 914]] engine.
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| ==Specifications==
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| <big>'''Technical data:'''</big>
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| *Wingspan: 9,15 m
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| *Length: 6,27 m
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| *Height: 2,30 m
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| *Cabin width: 1,24m
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| *Wing area: 11,3 <math>m^2</math>
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| *Wing torsion -2,4 deg
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| *Horizontal tail area: 2,1 <math>m^2</math>
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| *Vertical tail area: 1 <math>m^2</math>
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| *Wing root airfoil: [[NACA]] 4415
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| *Wing tip airfoil: [[NACA]] 4412
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| *Tail airfoil: [[NACA]] 0012
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| <big>'''Weight and Performance:'''</big>
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| *Empty Weight: 290 kg
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| *Max. Takeoff Weight: 472,5 kg
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| *Payload: 182,5 kg
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| *Max. Fuel Capacity: 2x50 l
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| *Max. Load Factors: +4 / -2
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| *Stall Speed (without flaps): 77 km/h
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| *Stall Speed (with flaps): 61 km/h
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| *Never Exceed Speed: 220 km/h
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| *Max. Speed in horizontal flight: 270 km/h
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| *Cruising speed: 240 km/h
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| *Rate of climb: 8 m/s
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| *Ceiling: 3650 m
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| *Range (45 min. reserves): 1200 km
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| ==See also==
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| * [[Skopiński Panda]]
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| ==External links==
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| *[http://www.aero-service.com Aero-service Jacek Skopiński website]
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| {{DEFAULTSORT:Skopinski Puma}}
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| [[Category:Polish ultralight aircraft 2010–2019]]
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| {{aero-2010s-stub}}
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Should a customer have trouble figuring out how long it will increase the evaluated worth of the support posts and self-drilling fasteners. Plus, two car garage steel building solar or battery operated garage doors often come with the household owner having two years to come- and your loved ones remain protected under a secure home office, industrial and multi family purposes.
My webpage :: Childers Carports And Structures Inc