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Example:
Figure 06−03−3 shows that at an ambient temperature of 0°C, pressure altitude of
10,000 feet, calm wind conditions and APR on, the take-off weight limited by maximum
tire speed is 20,830 kg (45,922 lb).
NOTE
If take-off is performed with the APR off, the weight derived from
Figure 06−03−3 must be reduced by 200 kg (440 lb).
PERFORMANCE
Take−Off Performance
06−03−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. MAXIMUM ALLOWABLE TAKE-OFF WEIGHT (CONT'D)
DFM0603_004 VTIRE604RC_HA−15AUG96
PERFORMANCE
Take−Off Performance
06−03−9
REV 66, Feb 01/07
Take-Off Weight Limited by Maximum Tire Speed
Figure 06−03−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE
The following charts are used to obtain the take-off distance for a given value of airplane weight,
ambient temperature, airport pressure altitude, wind, runway slope, APR usage and various
bleed configurations.
These charts present the most limiting of the following:
• Take-off distance with all engines operating, multiplied by a factor of 1.15;
• Take-off distance with one engine inoperative; and
• Accelerate-stop distance.
A. Take-Off Distance, Flaps 20° – Anti-Icing Off
The take-off distance for a flaps-20° take-off, at airport pressure altitudes of 10,000 feet and
below, with anti-icing off, is given by Figure 06−03−4 (Page 1 of 2).
Example:
Associated Conditions:
Temperature = 20°C
Airport pressure altitude = 4,000 feet
10th stage bleeds = Closed
Wing and cowl anti-ice = Off
Gross weight = 19,000 kg (41,887 lb)
Wind = 30 knots headwind
Runway slope = +2%
APR = Armed
The example in Figure 06−03−4 (Page 1 of 2) shows that for the above associated
conditions, the take-off distance is 1,800 meters (5,905 feet).
The take-off distance for a flaps-20° take-off, at airport pressure altitudes above 10,000 feet,
with anti-icing off, is given by Figure 06−03−4 (Page 2 of 2).
Example:
Associated Conditions:
Temperature = 20°C
Airport pressure altitude = 12,000 feet
10th stage bleeds = Closed
Wing and cowl anti-ice = Off
Gross weight = 16,000 kg (35,274 lb)
Wind = 30 knots headwind
Runway slope = +2%
APR = Armed
The example in Figure 06−03−4 (Page 2 of 2) shows that for the above associated
conditions, the take-off distance is 2,880 meters (9,449 feet).
PERFORMANCE
Take−Off Performance
06−03−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
DFM0603_005 BFL604RC_AIOFF_VMCG−21JUNE96
PERFORMANCE
Take−Off Performance
06−03−11
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing Off (Page 1 of 2)
Figure 06−03−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
DFM0603_006 BFL604RC_AIOFF_HA−21JUN96
PERFORMANCE
Take−Off Performance
06−03−12
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing Off (Page 2 of 2)
Figure 06−03−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
B. Take-Off Distance, Flaps 20° – Anti-Icing On
The take-off distance for a flaps-20° take-off, at airport pressure altitudes of 10,000 feet and
below, with anti-icing on is given by Figure 06−03−5 (Page 1 of 2).
Example:
Associated Conditions:
Temperature = –30°C
Airport pressure altitude = 6,000 feet
10th stage bleeds = Closed
Cowl anti-ice = On
Gross weight = 19,000 kg (41,887 lb)
Wind = 30 knots headwind
Runway slope = +2%
APR = Armed
The example in Figure 06−03−5 (Page 1 of 2) shows that for the above associated
conditions, the take-off distance is 1,800 meters (5,905 feet).
The take-off distance for a flaps-20° take-off, at airport pressure altitudes above 10,000 feet,
with anti-icing on, is given by Figure 06−03−5 (Page 2 of 2).
Example:
Associated Conditions:
Temperature = –10°C
Airport pressure altitude = 12,000 feet
10th stage bleeds = Closed
Cowl anti-ice = On
Gross weight = 16,000 kg (35,274 lb)
Wind = 30 knots headwind
　
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