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C. Take-Off Decision Speed, V1 – Flaps 20° – Anti-Icing On
Figure 06−03−8 is used to determine the V1 speed for a flaps-20° take-off (balanced field
length), for varying conditions of take-off weight, ambient temperature, airport pressure
altitude, wind, runway slope, APR usage and use of anti-icing.
Example:
Associated Conditions:
Take-off weight = 20,000 kg (44,092 lb)
Airport pressure altitude = 4,000 feet
Cowl anti-icing = On
Ambient temperature = –20°C
Wind = 30 knots headwind
Runway slope = +2%
APR = Off
The example in Figure 06−03−8 shows that for the above associated conditions, V1 is
equal to 138.5 KIAS.
PERFORMANCE
Take−Off Performance
06−03−20
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
DFM0603_011 V1604PS_AION_HA_18JUN96
PERFORMANCE
Take−Off Performance
06−03−21
REV 66, Feb 01/07
V1 Speed – Flaps 20°, – Anti-Icing On
Figure 06−03−8
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
D. Rotation Speed, VR, Flaps 20° – Anti-Icing Off
Figure 06−03−9 is used to determine the rotation speed (VR) for a flaps-20° take-off, for
varying conditions of ambient temperature, airport pressure altitude, bleed configurations,
take-off weight, runway slope and use of APR.
VR must not be less than 121 KIAS.
Example:
Associated Conditions:
Ambient temperature = 0°C
Airport pressure altitude = 4,000 feet
10th stage bleeds = Closed
Take-off weight = 18,000 kg (39,683 lb)
Runway slope = +2%
APR = Off
The example in Figure 06−03−9 shows that for the above associated conditions, the
rotation speed is 133 KIAS.
PERFORMANCE
Take−Off Performance
06−03−22
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
DFM0603_012 VR604RC_AIOFF_HA−08APR96
PERFORMANCE
Take−Off Performance
06−03−23
REV 66, Feb 01/07
Rotation Speed, VR, Flaps 20° – Anti-Icing Off
Figure 06−03−9
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
E. Rotation Speed, VR, Flaps 20° – Anti-Icing On
Figure 06−03−10 is used to determine the rotation speed (VR) for a flaps-20° take-off, for
varying conditions of ambient temperature, airport pressure altitude, take-off weight, runway
slope, APR usage and use of anti-icing.
VR must not be less than 121 KIAS.
Example:
Associated Conditions:
Ambient temperature = –20°C
Airport pressure altitude = 4,000 feet
Cowl anti-icing = On
Take-off weight = 18,000 kg (39,683 lb)
Runway slope = +2%
APR = Off
The example in Figure 06−03−10 shows that for the above associated conditions, the
rotation speed is 133 KIAS.
PERFORMANCE
Take−Off Performance
06−03−24
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
DFM0603_013 VR604RC_AION_HA−08APR96
PERFORMANCE
Take−Off Performance
06−03−25
REV 66, Feb 01/07
Rotation Speed, VR, Flaps 20° – Anti-Icing On
Figure 06−03−10
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
F. Take-Off Safety Speed, V2 – Flaps 20°
Figure 06−03−11 is used to determine the take-off safety speed (V2) for a flaps-20° take-off,
for varying conditions of ambient temperature, airport pressure altitude and take-off weight.
NOTE
1. V2 is the greater of the values obtained from Chart A and Chart B of
Figure 06−03−11 .
2. V2 from Chart A is not limiting at weights greater than 17,500 kg
(38,581 lb).
3. V2 from Chart B is not limiting at speeds less than 125 KIAS.
Example:
Associated Conditions:
Outside air temperature = 10°C
Airport pressure altitude = 2,000 feet
Take-off weight = 17,000 kg (37,478 lb)
Chart A of Figure 06−03−11 shows that for the above associated conditions, the take-off
safety speed is 130.0 KIAS.
Chart B of Figure 06−03−11 shows that for the above associated conditions, the take-off
safety speed is 132.5 KIAS.
　
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