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CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_001 BFL604JP_AIOFF_WET_VMCG−1JUN96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−5
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing Off − Wet Runway (Page 1 of 2)
Figure 07−02−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_002 BFL604JP_AIOFF_WET_HA_1MAY96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−6
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing Off − Wet Runway (Page 2 of 2)
Figure 07−02−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
C. Take-Off Distance, Flaps 20° – Anti-Icing On – Wet Runway
The take-off distance for a flaps 20° take-off on a wet runway, at airport pressure altitudes of
10,000 feet and below, with anti-icing on is given by Figure 07−02−2 (Page 1 of 2).
NOTE
When dispatching with one thrust reverser inoperative, the take-off
distance derived from Figure 07−02−2 (Page 1 of 2) must be
increased by 200 meters (656 feet).
Example:
Associated Conditions:
Ambient temperature = –30°C
Airport pressure altitude = 6,000 ft
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
Thrust reversers = Both available
The example in Figure 07−02−2 (Page 1 of 2) shows that for the above associated
conditions, the take-off distance is 1,750 meters (5,741 feet).
The take-off distance for a flaps 20° take-off on a wet runway, at airport pressure altitudes
above 10,000 feet, with anti-icing on is given by Figure 07−02−2 (Page 2 of 2).
NOTE
When dispatching with one thrust reverser inoperative, the take-off
distance derived from Figure 07−02−2 (Page 2 of 2) must be
increased by 200 meters (656 feet).
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−7
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
Example:
Associated Conditions:
Ambient temperature = –30°C
Airport pressure altitude = 12,000 ft
10th stage bleeds = Closed
Cowl anti-ice = On
Gross weight = 16,000 kg (35,274 lb)
Wind = 30 knots headwind
Runway slope = +2%
APR = Armed
Thrust reversers = Both available
The example in Figure 07−02−2 (Page 2 of 2) shows that for the above associated
conditions, the take-off distance is 2,030 meters (6,660 feet).
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_003 BFL604JP_AION_WET_VMCG−16JUL96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−9
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing On − Wet Runway (Page 1 of 2)
Figure 07−02−2
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_004 BFL604JP_AION_WET_HA−16JUL96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−10
REV 66, Feb 01/07
Take-Off Distance, Flaps 20° − Anti-Icing On − Wet Runway (Page 2 of 2)
Figure 07−02−2
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
D. Take-Off Decision Speed, V1 (Flaps 20°) – Anti-Icing Off – Wet Runway
Figure 07−02−3 is used to determine the V1 speed for a flaps 20° take-off (balanced field
length) on a wet runway, for varying conditions of take-off weight, ambient temperature,
airport pressure altitude, wind, runway slope and various bleed configurations.
NOTE
When dispatching with one thrust reverser inoperative, the take-off
decision speed, V1, derived from Figure 07−02−3 must be reduced by
2.0 KIAS. If the reduced V1 speed is lower than V1MCG, use V1 = V1MCG.
Example:
Associated Conditions:
Take-off weight = 20,000 kg (44,092 lb)
　
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