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Runway slope = +2%
APR = Armed
The example in Figure 06−03−5 (Page 2 of 2) shows that for the above associated
conditions, the take-off distance is 2,250 meters (7,382 feet).
PERFORMANCE
Take−Off Performance
06−03−13
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
DFM0603_007 BFL604RC_AION_VMCG−31JUL96
PERFORMANCE
Take−Off Performance
06−03−14
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing On (Page 1 of 2)
Figure 06−03−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
DFM0603_008 BFL604RC_AION_HA−31JUL96
PERFORMANCE
Take−Off Performance
06−03−15
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing On (Page 2 of 2)
Figure 06−03−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. TAKE-OFF DISTANCE (CONT'D)
C. Rolling Take-Off Procedure
When using a rolling take-off procedure:
• The aircraft take-off distance is to be increased by 200 feet.
• For obstacle clearance calculation, use either obstacle distance from end of runway or
obstacle distance from corrected take-off distance.
If the FMS take-off function is used to derive the performance information for a rolling take-off:
• The available runway length, reduced by 200 feet, must be manually entered on the CDU
TAKEOFF REF pages.
• For obstacle clearance calculation, set OBST DIST to either of the following values on the
CDU TAKEOFF REF pages:
• Obstacle distance from end of runway (not reduced by 200 feet), or
• Obstacle distance derived using the uncorrected take-off field length.
NOTE
When RWY LENGTH is manually entered, the FMS does not compute
headwind/crosswind; these must be manually entered on the CDU.
4. TAKE-OFF SPEEDS
The following charts are used to determine the take-off speeds (V1, VR and V2).
V1 can not be less than V1MCG nor greater than VR.
A. Minimum V1 Limited By Control on the Ground – V1MCG
Figure 06−03−6 is used to determine the minimum V1 limited by control on the ground
(V1MCG) for varying conditions of take-off weight, ambient temperature, airport pressure
altitude and runway slope.
The V1MCG speeds derived from Figure 06−03−6 are applicable for all engine bleed
configurations.
Example:
Associated Conditions:
Take-off weight = 19,000 kg (41,887 lb)
Airport pressure altitude = 6,000 feet
Ambient temperature = 0°C
Runway slope = +2%
The example in Figure 06−03−6 shows that for the above associated conditions, V1MCG
is equal to 102.5 KIAS.
PERFORMANCE
Take−Off Performance
06−03−16
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
DFM0603_009 V1MCG604DKC−13JUN96
PERFORMANCE
Take−Off Performance
06−03−17
REV 66, Feb 01/07
Minimum V1 Limited by Control on the Ground – V1MCG
Figure 06−03−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
B. Take-Off Decision Speed, V1 – Flaps 20° – Anti-Icing Off
Figure 06−03−7 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 various bleed configurations.
Example:
Associated Conditions:
Take-off weight = 20,000 kg (44,092 lb)
Airport pressure altitude = 4,000 feet
10th stage bleeds = Closed
Ambient temperature = 0°C
Wind = 30 knots headwind
Runway slope = +2%
APR = Off
The example in Figure 06−03−7 shows that for the above associated conditions, V1 is
equal to 138.3 KIAS.
PERFORMANCE
Take−Off Performance
06−03−18
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
DFM0603_010 V1604PS_AIOFF_HA_18JUN96
PERFORMANCE
Take−Off Performance
06−03−19
REV 66, Feb 01/07
V1 Speed – Flaps 20°, – Anti-Icing Off
Figure 06−03−7
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. TAKE-OFF SPEEDS (CONT'D)
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