SZD-19 Zefir
Picture has been licensed under a GFDL license.
Original source: Own work Author Michał Derela user:Pibwl Permission (Reusing this file) see below (gnu fdl, cc-by-sa-2.5)
Author: Michał Derela user:Pibwl Permission (Reusing this file) see below (gnu fdl, cc-by-sa-2.5)

SZD19-2A Zefir2A. jpg SZD19-2A Zefir 2A in the Polish Aviation Museum Role Glider National origin Poland Manufacturer SZD Designed by Bogumił Szuba First flight 31 December 1958 Introduced 1960 Number built 22 The SZD-19 Zefir (Szybowcowy Zakład Doświadczalny - Glider Experimental Works) is a single-seat glider aircraft that was designed and built in Poland from 1957.

febrero a bordo de un SZD-19 Zefir 2, con una velocidad media de 95,355 km/h. El piloto obtuvo además el récord nacional polaco de triángulo de 300 km.1

Made by Szybowcowy Zakład Doświadczalny.

Empty Weight Lb
7278
Stall Speed Mph
44
Designer
Bogumił Szuba
Span Ft
55
Max Speed Mph
137
Aspect Ratio
21
Introduced
1960
Wing Profile
NACA632-515
Glide Ratio
35
Span In
9
Wing Area Sqm
14
Gross Weight Lb
915
Sink Rate Ms
1
Number Built
22
Crew
1
Empty Weight Kg
330
Gross Weight Kg
415
Min Sink Speed Mph
54
Height In
5
Stall Speed Kts
38
Stall Speed Kmh
71
Sink Rate Ftmin
163
Manufacturer
Max Speed Kts
119
First Flight
31
Max Speed Kmh
220
Height Ft
5
Origin
Poland
Min Sink Speed Kts
47
National Origin
Poland
Wing Area Sqft
151
Met Or Eng
met
Min Sink Speed Km/h
87
Span M
17
Length Ft
23
Height M
2
Similar Aircraft
*Schemp-Hirth SHK
GLimits
+6 - -3
Length In
11
Length M
7
Category

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