CP23

MUDRY CAP-230/231/232

Aircraft
Name
CAP-230/231/232
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, high set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tailwheel fixed
Manufacturered as
MUDRY CAP-230
MUDRY CAP-232
MUDRY CAP-231
CAP AVIATION CAP-232
AKROTECH EUROPE CAP-232

CP23

The CAP Aviation CAP-23x family is a family of 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.

Technical Data
Wing span (metric)
8.10 m
Length (metric)
6.75 m
Height (metric)
1.60 m
Powerplant

1 x 300 HP Lycoming AEIO-540-L1B5D piston engine with 2, 3 or 4 blade propeller (depending on the version CAP 230, 231 or 232).

Engine Model(s)
Lycoming O-540
Indicative Performance Data
Take-Off
V2
n/a
Distance
200 m
MTOW
800 kg
Initial Climb (to 5000 ft)
IAS
95 kts
ROC
1400 ft/min
Initial Climb (to FL150)
IAS
100 kts
ROC
500
Initial Climb (to FL240)
IAS
100 kts
ROC
0 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
150 kts
MACH
n/a
Ceiling
150
Range
640 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
130 kts
ROD
500 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
68 kts
ROD
n/a
Approach
Vapp (IAS)
60 kts
Distance
450 m

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