PZL Bielsko SZD-52: Difference between revisions
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| type=Standard-class [[Glider aircraft|sailplane]] |
| type=Standard-class [[Glider aircraft|sailplane]] |
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| national origin=Poland |
| national origin=[[Poland]] |
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| manufacturer=[[PZL Bielsko]] |
| manufacturer=[[PZL Bielsko]] |
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| designer= |
| designer=Adam Kurbiel |
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| first flight=28 February 1981 |
| first flight=28 February 1981 |
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| number built=8 |
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Revision as of 07:12, 22 June 2018
SZD-52 | |
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Role | Standard-class sailplane |
National origin | Poland |
Manufacturer | PZL Bielsko |
Designer | Adam Kurbiel |
First flight | 28 February 1981 |
Number built | 8 |
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.