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ice, standing water or snow except in the interest of safety.
AR Certified Airplanes
(2) During taxi, do not use thrust reversers if movement area surfaces are covered with
slush, ice, standing water or snow except in the interest of safety.
(3) The maximum crosswind component for take-off and landing on a wet runway with water
depth no more than 3.00 mm (0.125 inch) is defined in the following table for different
values of the coefficient of friction:
COEFFICIENT OF FRICTION MAXIMUM CROSSWIND COMPONENT
0.3 (poor braking) 10 knots (5 meters/sec)
0.4 (average braking) 15 knots (8 meters/sec)
0.5 (good braking, equivalent to dry) 24 knots (12 meters/sec)
(4) The maximum crosswind component for take-off and landing on a contaminated runway
is 10 knots (5 meters/sec).
(5) Operation on runways with a coefficient of friction less than 0.3 is prohibited.
D. Emergency Procedures
The emergency procedures in Chapter 3 are applicable.
E. Normal Procedures
The normal procedures in Chapter 4 are applicable.
F. Abnormal Procedures
The abnormal procedures in Chapter 5 are applicable.
G. Performance
The performance data given in Chapter 6 are applicable in addition to paragraphs 2. through
4. in the following pages.
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE
A. General
Take-off performance data are calculated based on the assumption that maximum available
reverse thrust is used down to a complete stop.
The following charts are used to obtain the take-off distance and V1 speed data for varying
conditions of temperature, airport pressure altitude, and airplane weight for the specified
take-off conditions, for a wet runway.
If the take-off distance on a wet runway is less than the take-off distance on a dry runway,
use the take-off distance for a dry runway.
The take-off distance charts herein present the most limiting of the following:
(1) The distance from the start of the take-off roll to the point at which the airplane attains a
height of 15 feet above the take-off surface, with a failure of the critical engine at VEF, or
(2) 115% of the distance from the start of the take-off roll to the point at which the airplane
attains a height of 35 feet above the take-off surface, with all engines operating, or
(3) The accelerate-stop distance.
B. Take-Off Distance, Flaps 20° – Anti-Icing Off – 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 off, is given by Figure 07−02−1 (Page 1 of 2).
NOTE
When dispatching with one thrust reverser inoperative, the take-off
distance derived from Figure 07−02−1 (Page 1 of 2) must be
increased by 200 meters (656 feet).
Example:
Associated Conditions:
Ambient temperature = 20°C
Airport pressure altitude = 4,000 ft
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
Thrust reversers = Both available
The example in Figure 07−02−1 (Page 1 of 2) shows that for the above associated
conditions, the take-off distance is 1,750 meters (5,741 feet).
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
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 off, is given by Figure 07−02−1 (Page 2 of 2).
NOTE
When dispatching with one thrust reverser inoperative, the take-off
distance derived from Figure 07−02−1 (Page 2 of 2) must be
increased by 200 meters (656 feet).
Example:
Associated Conditions:
Ambient temperature = 20°C
Airport pressure altitude = 10,000 ft
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
Thrust reversers = Both available
The example in Figure 07−02−1 (Page 2 of 2) shows that for the above associated
conditions, the take-off distance is 2,170 meters (7,119 feet).
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−4
REV 66, Feb 01/07
DOT Approved
　
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