CAP 230
Picture has been licensed under a GFDL license.
Original source: Own work Author Guillaume Paumier (user:guillom) Permission (Reusing this file) Own work, attribution required (Multi-license with GFDL and Creative Commons CC-BY 2.5)
Author: Guillaume Paumier (user:guillom) Permission (Reusing this file) Own work, attribution required (Multi-license with GFDL and Creative Commons CC-BY 2.5)

The CAP Aviation CAP-23x family is a family of high-performance aircraft designed for competition aerobatics. The CAP 230 airframe was a direct development of the CAP 21 competition single seater strengthened to cope with a 300 hp 6-cylinder Lycoming AEIO-540 engine instead of the 200 hp original 4-cylinder Lycoming AEIO-360.

Cap 230 IAFF Fire Fighters Firefighting Hat Ball Cap Returns: Accepted within 14 days Enlarge 0 Bids $0.1
The cap 230 includes a series of threads on an interior surface of the cap 230 for mating with a series of threads on the exterior surface of the housing 220.2

Made by Avions Mudry & Cie.

It is the successor of the Mudry CAP 20 .

The nipple cap 230 includes, as shown in FIG.3
* CAP 230 (redirection depuis Cap 231) Les CAP 230, 231 et 232 font partie d'une famille de monoplaces de compétition de voltige 4
Jet Or Prop
prop
Height Alt
6
Predecessor
Mudry CAP 20
Stall Speed Main
90.0
Length Alt
22
Max Takeoff Weight Main
820.0
Power Alt
300 hp
Range Main
360.0
Loaded Weight Main
730.0
Max Speed Alt
12300.0
Never Exceed Speed Alt
14880.0
Loading Main
74
Power/mass Main
Developed From
Mudry CAP 20
Introduction
1998
Power/mass Alt
684.0
Height Main
1.90 m
Airfoil
V16F
Cruise Speed Main
300.0
Max Takeoff Weight Alt
1807.0
Type Of Prop
air-cooled flat-six
Crew
one
Never Exceed Speed Main
400.0
Max Speed More
at sea level
Climb Rate Main
16 m-s
Cruise Speed Alt
11160.0
Area Main
9.86 m²
Primary user
Royal Moroccan Air Force
Span Alt
807.72
Plane Or Copter?
plane
Engine(prop)
Lycoming O-540
Sequence
CAP-21 -CAP-230 -CAP-231 -CAP-231EX -CAP-232
Manufacturer
Avions Mudry & Cie
First Flight
1997
Loaded Weight Alt
1609.0
More Performance
+10; -10g* Roll rate at 300 km-h
Number Of Props
1
Stall Speed Alt
3360.0
Max Speed Main
330.0
Climb Rate Alt
3150
Length Main
6.75 m
Span Main
8.80 m
Area Alt
106.0
Range Alt
13380.0
Similar Aircraft
*Zivko Edge 540*Sukhoi Su-26*Extra 300
Empty Weight Main
630.0
Power Main
224.0
Category
Aerobatic aircraft
French sport aircraft 1990-1999
Low wing aircraft
Propeller aircraft
Single-engine aircraft
Empty Weight Alt
1389.0
Loading Alt
15

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