PZL Bielsko SZD-52: Difference between revisions
Content deleted Content added
→Notes: stub tagging using AWB |
|||
| Line 20: | Line 20: | ||
}} |
}} |
||
|} |
|} |
||
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 [[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" /> |
||
==Variants== |
==Variants== |
||
| Line 179: | Line 179: | ||
*[[List of sailplanes]] |
*[[List of sailplanes]] |
||
}} |
}} |
||
==References== |
==References== |
||
===Notes=== |
===Notes=== |
||
{{reflist|refs= |
{{reflist|refs= |
||
| Line 186: | Line 188: | ||
<!-- ==External links== --> |
<!-- ==External links== --> |
||
{{PZL aircraft}} |
{{PZL aircraft}} |
||
{{aviation lists}} |
|||
[[Category:Polish sailplanes 1980–1989]] |
[[Category:Polish sailplanes 1980–1989]] |
||
[[Category:PZL aircraft|SZD52]] |
[[Category:PZL aircraft|SZD52]] |
||
{{Aero-1980s-stub}} |
{{Aero-1980s-stub}} |
||
Revision as of 21:25, 23 June 2015
| SZD-52 | |
|---|---|
| Role | Standard-class sailplane |
| National origin | Poland |
| Manufacturer | PZL Bielsko |
| First flight | 28 February 1981 |
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
- SZD-52 Jantar 15
- SZD-52-1 Jantar 15SI
- SZD-52-2 Krokus
- SZD-52-3 Krokus S
- SZD-52-4 Krokus C
Sepcifications (SZD52-3)
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
- Never exceed speed: 255 km/h (158 mph, 138 kn)
See also
Related lists
References
Notes
- ^ a b c d "Type Certificate Data Sheet A-441 SZD-52 Krokus" (PDF). European Aviation Safety Agency. 14 February 2007. Retrieved 2009-12-26.
 | This article on an aircraft of the 1980s is a stub. You can help Wikipedia by expanding it. |