RWD-21
Picture has been licensed under a GFDL license.
Original source: Own work Author Michał Derela (Pibwl) Permission (Reusing this file) GFDL, cc-by-sa-2.5,2.0,1.0 (see below)
Author: Michał Derela (Pibwl) Permission (Reusing this file) GFDL, cc-by-sa-2.5,2.0,1.0 (see below)

The RWD-16bis and RWD-21 were Polish two-seat low-wing touring and sports planes of the late 1930s constructed by the RWD bureau sharing the same construction main difference of the RWD-21 being a stronger engine.

Made by Doświadczalne Warsztaty Lotnicze.

It is the successor of the RWD-16 .

Jet Or Prop
prop
Designer
RWD (aircraft manufacturer)
RWD bureau
Predecessor
RWD-16
Stall Speed Main
70.0
72.0
Max Takeoff Weight Main
685.0
Power Alt
44.0
kW
Range Main
650.0
700.0
Loaded Weight Main
615.0
660.0
Type Of Prop
4
Introduced
1938
Loading Main
41
44
Developed From
RWD-16
Capacity
1
Max Speed Main
180.0
210.0
Cruise Speed Main
155.0
180.0
Ceiling Main
4
150 m
5
500 m
Number Built
>2 RWD-16bis
>6 RWD-21
Crew
1
Retired
1950
Span Main
11 m
Area Main
14.95 m²
Primary user
Poland
Plane Or Copter?
plane
Engine(prop)
Blackburn Cirrus Minor
Walter Mikron II
Manufacturer
Doświadczalne Warsztaty Lotnicze
Number Of Props
1
First Flight
1938
Production End Year
1939
National Origin
Poland
Climb Rate Main
3.1 m-s
4.7 m-s
Power Main
62 hp
90 hp
Production Start Year
1938
Length Main
7.9 m
8.4 m
Similar Aircraft
*Bücker Bü 181 - LWD Żak
Useful Load Main
230.0
235
Empty Weight Main
385.0
425.0
Height Main
2.12 m
2.27 m
Produced
1938
Category
Polish civil utility aircraft 1930-1939
Polish sport aircraft 1930-1939

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