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A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
The PZL Krosno KR-03 Puchatek is a Polish mid-wing , T-tailed , two-seats-in-tandem , glider that was designed by Jerzy Krawczyk and Eugeniusz Pelczar and produced by PZL Krosno , first flying in 1985.[1] [2]
Design and development
[ edit ]
The KR-03 was designed as an ab initio training glider .[1] The name Puchatek is Polish translation of Pooh Bear .[3]
The aircraft is made from aluminium with some parts covered in doped aircraft fabric covering . Its 16.4 m (53.8 ft ) span wing employs a Wortmann FX S-02-158 airfoil . The wing features top and bottom Schempp-Hirth -style dive brakes . The landing gear consists of an oleo-pneumatic sprung, non-retractable main wheel, a tail wheel and a rubber sprung nose skid. The Puchatek has a baggage compartment with a capacity of 5 kg (11 lb ) for soft baggage items.[1] [2] [4]
The aircraft was type certified in the United States on 6 August 1991, with Barry Aviation of Edgewater, Volusia County, Florida as the US certificate holder.[2]
Operational history
[ edit ]
In 1993, a few examples were put into service with the Australian Air Force Cadets (AAFC), totalling to three as of 2012. They are currently assigned to 2 Wing AAFC. They are still in service as of 2014.[5]
As of August 2011 there were 16 KR-03As registered in the United States with the Federal Aviation Administration [6] and in August 2022 there were 10 KR-03As registered.[7]
Variants
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KR-03A
Main production version.[1]
Specifications (KR-03A)
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Instrument panel
Data from Sailplane Directory, Type Certificate G56EU and The Incomplete Guide to Airfoil Usage[1] [2] [4]
General characteristics
Crew: one
Capacity: one passenger
Wingspan: 16.4 m (53 ft 10 in )
Wing area: 19.44 m 2 (209.3 sq ft )
Airfoil : Wortmann FX S-02-158
Empty weight: 350 kg (772 lb )
Gross weight: 540 kg (1,190 lb )
Performance
Never exceed speed : 198 km/h (123 mph, 107 kn )
g limits: +5.3/-2.65
Maximum glide ratio: 27:1 at 88 km/h (55 mph)
Rate of sink: 0.78 m/s (154 ft/min)
Wing loading: 27.78 kg/m2 (5.69 lb/sq ft )
See also
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Related lists
References
[ edit ]
^ Milne, A.A. (2012). Kubuś Puchatek (in Polish). Translated by Irena Tuwim (29th ed.). Wydawnictwo Nasza Księgarnia. ISBN 978-83-10-12033-5 .
^ a b Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage" . Archived from the original on 20 April 2010. Retrieved 1 August 2011 .
^ "PZLPUCHATEK" . 6 May 2014. Retrieved 29 April 2020 .
^ Federal Aviation Administration (August 2011). "Make / Model Inquiry Results" . Retrieved 21 August 2011 .
^ Federal Aviation Administration (August 2022). "Aircraft Inquiry" . Retrieved 3 August 2022 .
External links
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R e t r i e v e d f r o m " https://en.wikipedia.org/w/index.php?title=PZL_Krosno_KR-03_Puchatek&oldid=1165003610 "
C a t e g o r i e s :
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H i d d e n c a t e g o r i e s :
● C S 1 P o l i s h - l a n g u a g e s o u r c e s ( pl )
● A r t i c l e s w i t h s h o r t d e s c r i p t i o n
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● U s e d m y d a t e s f r o m M a y 2 0 2 2
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● T h i s p a g e w a s l a s t e d i t e d o n 1 2 J u l y 2 0 2 3 , a t 1 1 : 1 5 ( U T C ) .
● T e x t i s a v a i l a b l e u n d e r t h e C r e a t i v e C o m m o n s A t t r i b u t i o n - S h a r e A l i k e L i c e n s e 4 . 0 ;
a d d i t i o n a l t e r m s m a y a p p l y . B y u s i n g t h i s s i t e , y o u a g r e e t o t h e T e r m s o f U s e a n d P r i v a c y P o l i c y . W i k i p e d i a ® i s a r e g i s t e r e d t r a d e m a r k o f t h e W i k i m e d i a F o u n d a t i o n , I n c . , a n o n - p r o f i t o r g a n i z a t i o n .
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