Mudry CAP 10

The Mudry CAP 10 is a two-seat training aerobatic aircraft first built in 1970 and still in production in 2007. The plane was developed from the Piel Super Emeraude and was born as the CP100. The name changed to CAP 10 CAP for 'Constructions Aéronautiques Parisiennes'. The CAP 10 was manufactured by Mudry (name of its designer) in Bernay France bought by CAP Industries which then became Apex Aircraft.

for the club fee? The Mudry CAP 10 is a two-seat training aerobatic aircraft first built in 1970 and still in production in 2007.1
Aerobatics in a Mudry CAP 10 Aerobatics in a Mudry CAP 10 * Order: Reorder * Duration: 3:06 * Published: 2
Contemporary of the MUDRY CAP 10 and other ZLIN 226, it is an aerobatic tandem two-seater monoplane equipped with a retract gear.3
El Mudry CAP 10 es un avión acrobático biplaza con la configuración de pilotos lado a lado construido en 1970 y que aún seguía en producción en el año 2007.4

Made by Avions Mudry & Cie.

It is the successor of the Piel Emeraude .

Mudry CAP 10, MS-88 Rallye, Falcon 10, Xingu Marine nationale Parent unit Armées françaises (French military) Components 5
the club fee? The Mudry CAP 10 is a two-seat training aerobatic aircraft first built in 1970 and still in production in 2007.6
The Mudry CAP 10 is a two-seat training aerobatic aircraft first built in 1970 and still in production.7
60 cubic inch/10cc glow-powered Vinh Quang Model Mudry CAP 10 is a fully aerobatic, low-wing, "sport scale" model plane with slight dihedral This homebuilt high-wing model is an example of the 8
Height Main
2.55 m
Designer
Mudry
Predecessor
Piel Emeraude
Stall Speed Main
85.0
Length Alt
716.28
Max Takeoff Weight Main
830.0
Jet Or Prop
prop
Range Main
1200.0
More Performance
* G-loads: version +6; -4
5g
Height Alt
8
Type Of Prop
4
Never Exceed Speed Alt
12660.0
Max Speed Main
270.0
Developed From
Piel Super Emeraude
Introduction
1970
Airfoil
NACA 23012
Cruise Speed Main
250.0
Max Takeoff Weight Alt
1829.0
Ceiling Main
5000 m
Number Built
300
Crew
2
Never Exceed Speed Main
340.0
Max Speed More
at sea level
Retired
still built
Unit Cost
160000.0
Span Main
8.06 m
Cruise Speed Alt
9300.0
Area Main
10.85 m²
Span Alt
26
Plane Or Copter?
Power Alt
134.0
Engine(prop)
Lycoming O-360
Manufacturer
First Flight
1968
Climb Rate Main
360.0
Power Main
180 hp
Number Of Props
1
Stall Speed Alt
3180.0
Climb Rate Alt
1180.0
Length Main
7.16 m
Area Alt
116.8
Range Alt
44700.0
Similar Aircraft
*Extra 200*Van's RV-7
Max Speed Alt
10080.0
Empty Weight Main
540.0
Ceiling Alt
16400.0
Empty Weight Alt
1190.0
Category

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