AEROPRAKT-32L Pilot Operating Handbook
A32L-FO-POH
5 Performance
5.1 General
This section contains performance data of A-32L airplane of standard (basic) configuration
at maximum takeoff weight in the following environmental conditions: ICAO standard
atmosphere (ISA), mean sea level (MSL), no wind, hard and even runway. Those data may
vary depending upon the configuration and technical condition of a particular aircraft and
actual environmental conditions of its operation.
5.2 Takeoff and landing distances
The minimum takeoff and landing distances of A-32L for the above conditions are specified below.
However pilots should always keep in mind that actual takeoff and landing distances depend on
condition of the aircraft, environment and pilot skill.
Engine
Rotax-912UL
Rotax-912ULS
Takeoff/Landing run
100/80 m (328/262 ft)
80/80 m (262 ft)
Takeoff distance to 15 m (50 ft)
280 m (918 ft)
250 m (820 ft)
Landing distance from 15 m (50 ft)
350 m (1148 ft)
350 m (1148 ft)
5.3 Climb performance
The rate of climb depends on atmospheric conditions, airplane takeoff weight and flap
setting. The climb performance data of A-32L in ISA conditions at MSL, maximum takeoff
weight are specified below:
Engine
Rotax-912UL
Rotax-912ULS
Best angle of climb speed Vx
80 km/h (50 mph, 43 kts)
80 km/h (50 mph, 43 kts)
Best rate of climb speed Vy
120 km/h (75 mph, 65 kts) 120 km/h (75 mph, 65 kts)
Maximum rate of climb at Vx
3.5 m/s (689 fpm)
4.3 m/s (846 fpm)
Maximum rate of climb at Vy
4.2 m/s (826 fpm)
5 m/s (984 fpm)
5.4 Cruise speeds and fuel consumption at various RPM settings
The cruise speeds and fuel consumption depend upon a multitude of factors: propeller pitch
and engine adjustments, fuel quality, atmospheric conditions, flight altitude, aircraft loading
and condition of its outer surface, etc.
With the KievProp three-blade propeller adjusted to take-off RPM of 5100 per minute and
standard condition of atmosphere and aircraft the following cruise speeds and fuel
consumption values may be used for flight planning:
Engine RPM
Cruise speed ( AS)
Fuel consumption
3400
80 km/h
50 mph
43 kts
6.9 I/h 1.83 US gal/h
3500
100 km/h 62 mph
54 kts
7.2 I/h 1.90 US gal/h
3800
125 km/h 78 mph
67 kts
8.5 I/h 2.24 US gal/h
4200
150 km/h 93 mph
81 kts 10.5 I/h 2.78 US gal/h
4650
175 km/h 109 mph 94 kts 13.0 I/h 3.43 US gal/h
5150
200 km/h 124 mph 108 kts 16.9 I/h 4.47 US gal/h
5500
215 km/h 134 mph 116 kts 21.51/h 5.69 US gal/h
However these values should be considered as approximate as they may vary due to effect
of the above mentioned factors. It is recommended to verify those values for the particular
conditions in which the exact values are required.
2 3
AEROPRAKT-32L Pilot Operating Handbook
A32L-FO-POH
