Druine Condor
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Original source: Own work Author MilborneOne [edit] Licensing I, the copyright holder of this work, hereby publish it under the following license: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
Author: MilborneOne [edit] Licensing I, the copyright holder of this work, hereby publish it under the following license: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work

The Druine D.60 Condor was a light aircraft developed in France in the 1950s primarily as a trainer. It was an evolution of the Druine Turbi but featured an extensively revised fuselage allowing the pilot and instructor to sit side-by-side under a full canopy. Unlike its predecessors the Condor was not intended for amateur construction and therefore was able to make refinements to the design that would not previously have been possible.

Made by EudoniaRollason Aircraft and Engines.

Empty Weight Lb
900
Wing Area Sqm
11
Designer
Roger Druine
Eng 1 Type
Continental O-200
First Flight
1955
Ceiling Ft
14000
Eng 1 Kw
74
Gross Weight Lb
1475
Crew
Two
pilot-instructor and passenger
Climb Rate Ftmin
570
Empty Weight Kg
409
Gross Weight Kg
670
Span M
8
Range Km
483
Climb Rate Ms
173
Manufacturer
Eudonia
Rollason Aircraft and Engines
Range Miles
300
Max Speed Mph
169
Max Speed Kmh
272
Span In
6
Span Ft
27
Wing Area Sqft
120
Met Or Eng
met
Length Ft
22
Ceiling M
4300
Eng 1 Hp
100
Eng 1 Number
1
Length In
10
Length M
7
Category
Druine aircraft
French civil trainer aircraft 1950-1959

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