AISA I-11
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Original source: Own work Author Fly-by-Owen [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue
Author: Fly-by-Owen [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue

The I-11 was a two-seat civil utility aircraft manufactured in Spain in the 1950s. Originally designed by the Spanish aircraft company Iberavia its first (of two) prototype flew on 16 July 1951. It was a low-wing monoplane of conventional configuration with fixed tricycle undercarriage and a large bubble canopy over the two side-by-side seats. Flight characteristics were found to be pleasing but before plans could be made for mass production Iberavia was acquired by AISA.

los prototipos del AISA I-11 y los 190 restantes correspondieron a la versiĆ³n I-11B.1

Made by AISAIberavia.

AISA I-11 is the predecessor of the AISA I-115.

Empty Weight Lb
926
Wing Area Sqm
13
Eng 1 Type
Continental C90-12F four cylinder air-cooled horizontally-opposed piston engine
Max Speed Mph
250250
Cruise Speed Kmh
177
Ceiling Ft
15400
Cruise Speed Mph
110
Eng 1 Kw
70
Successor
AISA I-115
Span In
7
Gross Weight Lb
1474
Capacity
1
Number Built
~410
Crew
one pilot
Climb Rate Ftmin
726
Empty Weight Kg
421
Gross Weight Kg
670
Height In
3
Range Km
650
Climb Rate Ms
3
Manufacturer
Range Miles
400
First Flight
1951
Max Speed Kmh
200
Height Ft
6
Span Ft
30
Wing Area Sqft
144
Met Or Eng
met
Span M
9
Length Ft
21
Variants With Their Own Articles
AISA I-115
Height M
2
Ceiling M
4700
Eng 1 Hp
90
Eng 1 Number
1
Length In
3
Length M
6
Category

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