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{{Short description|Polish single-seat glider, 1981}}
__NOTOC__
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{|{{Infobox aircraft begin
| name=SZD-52
| name=SZD-52
| image=
| image=
| caption=
| caption=
}}{{Infobox Aircraft Type
}}{{Infobox aircraft type
| type=Standard-class [[Glider aircraft|sailplane]]
| type=Standard-class [[Glider aircraft|sailplane]]
| national origin=[[Poland]]
| national origin=[[Poland]]
| manufacturer=[[PZL Bielsko]]
| manufacturer=[[Państwowe Zakłady Lotnicze|PZL Bielsko]]
| designer=Adam Kurbiel
| designer=Adam Kurbiel
| first flight=28 February 1981
| first flight=28 February 1981
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|}
|}
{{external media
{{external media
| align = right
| float = right
| width = 312px
| width = 312px
| image1 = [https://www.flickr.com/photos/26267225@N03/7520970462 SZD-52-2 ''Krokus'' in flight]}}
| image1 = [https://www.flickr.com/photos/26267225@N03/7520970462 SZD-52-2 ''Krokus'' in flight]}}


The '''PZL Bielsko SZD-52''' is a [[Poland|Polish]] single-seat standard class [[Glider aircraft|sailplane]] produced by [[PZL Bielsko]].<ref name="tcds" /> It is a cantilever high-wing [[monoplane]] with a T-tail and has a retractable main landing gear and a fixed tailwheel.<ref name="tcds" /> The wings have integral water ballast tanks.<ref name="tcds" />
The '''PZL Bielsko SZD-52''' is a Polish single-seat standard class [[Glider aircraft|sailplane]] produced by [[Państwowe Zakłady Lotnicze|PZL Bielsko]].<ref name="tcds" /> It is a cantilever high-wing [[monoplane]] with a T-tail and has a retractable main landing gear and a fixed tailwheel.<ref name="tcds" /> The wings have integral water ballast tanks.<ref name="tcds" />


==Variants==
==Variants==
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;SZD-52-4 Krokus C
;SZD-52-4 Krokus C


==Sepcifications (SZD52-3)==
==Specifications (SZD52-3)==
{{Aircraft specs
{{Aircraft specs
|ref=<ref name="tcds" />
|ref=<ref name="tcds" />
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|related=<!-- related developments -->
|related=<!-- related developments -->
|similar aircraft=<!-- similar or comparable aircraft -->
|similar aircraft=<!-- similar or comparable aircraft -->
|sequence=<!-- designation sequence, if appropriate -->
|lists=<!-- related lists -->
|lists=<!-- related lists -->
*[[List of gliders]]
*[[List of gliders]]
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<ref name="tcds">{{cite web | title=Type Certificate Data Sheet A-441 SZD-52 Krokus | url=https://www.easa.europa.eu/system/files/dfu/EASA-TCDS-A.441_SZD--52_Krokus-01-14022007.pdf| date=14 February 2007| publisher=European Aviation Safety Agency}}</ref>
<ref name="tcds">{{cite web | title=Type Certificate Data Sheet A-441 SZD-52 Krokus | url=https://www.easa.europa.eu/system/files/dfu/EASA-TCDS-A.441_SZD--52_Krokus-01-14022007.pdf| date=14 February 2007| publisher=European Aviation Safety Agency}}</ref>
}}
}}

<!-- ==External links== -->
{{PZL aircraft}}
{{PZL aircraft}}


⚫
[[Category:1980s Polish sailplanes]]
⚫
[[Category:PZL aircraft|SZD52]]
{{Polish gliders}}
{{Polish gliders}}

⚫
[[Category:PZL aircraft|SZD52]]
⚫
[[Category:1980s Polish sailplanes]]
[[Category:Aircraft first flown in 1981]]
[[Category:SZD aircraft]]

Latest revision as of 18:05, 3 December 2023

SZD-52
Role Standard-class sailplane
National origin Poland
Manufacturer PZL Bielsko
Designer Adam Kurbiel
First flight 28 February 1981
Number built 8
External image
image icon SZD-52-2 Krokus in flight

The PZL Bielsko SZD-52 is a Polish single-seat standard class sailplane produced by PZL Bielsko.[1] It is a cantilever high-wing monoplane with a T-tail and has a retractable main landing gear and a fixed tailwheel.[1] The wings have integral water ballast tanks.[1]

Variants[edit]

SZD-52 Jantar 15
SZD-52-1 Jantar 15SI
SZD-52-2 Krokus
SZD-52-3 Krokus S
SZD-52-4 Krokus C

Specifications (SZD52-3)[edit]

Data from [1]

General characteristics

  • Crew: 1
  • Length: 7 m (23 ft 0 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Height: 1.55 m (5 ft 1 in)
  • Wing area: 10.3 m2 (111 sq ft)
  • Aspect ratio: 21.8
  • Empty weight: 248 kg (547 lb)
  • Gross weight: 370 kg (816 lb) without water ballast

Performance

See also[edit]

Related lists

References[edit]

Notes[edit]

  1. ^ a b c d "Type Certificate Data Sheet A-441 SZD-52 Krokus" (PDF). European Aviation Safety Agency. 14 February 2007.
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