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時間:2010-09-27 07:43來源:藍天飛行翻譯 作者:admin
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Airport pressure altitude = 2,000 ft
10th stage bleeds = Closed
Ambient temperature = 0°C
Wind = 30 knots headwind
Runway slope = +2%
APR = Off
Thrust reversers = Both available
The example in Figure 07−02−3 shows that for the above associated conditions, V1 is equal
to 128.3 KIAS.
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−11
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_005 V1604JP_AIOFF_WET_HA−1MAY96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−12
REV 66, Feb 01/07
V1 Speed (Flaps 20°) – Anti-Icing Off – Wet Runway
Figure 07−02−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
E. Take-Off Decision Speed, V1 (Flaps 20°) – Anti-Icing On – Wet Runway
Figure 07−02−4 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 use of anti-icing.
NOTE
When dispatching with one thrust reverser inoperative, the take-off
decision speed, V1, derived from Figure 07−02−4 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)
Airport pressure altitude = 8,000 ft
Cowl anti-icing = On
Ambient temperature = –20°C
Wind = 30 knots headwind
Runway slope = +2%
APR = Off
Thrust reversers = Both available
The example in Figure 07−02−4 shows that for the above associated conditions, V1 is equal
to 142.5 KIAS.
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−13
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. WET RUNWAY TAKE-OFF PERFORMANCE (CONT'D)
DFM0702_006 V1604JP_AION_WET_HA−18JUL96
SUPPLEMENT 2
Operation on Wet and Contaminated Runways
07−02−01−14
REV 66, Feb 01/07
V1 Speed (Flaps 20°) – Anti-Icing On – Wet Runway
Figure 07−02−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. CONTAMINATED RUNWAY TAKE-OFF PERFORMANCE
A. General
Contaminated runway distances have been estimated assuming that the runway is
completely contaminated. However, selection of the type and amount of contaminant should
be based on the runway conditions where the high speed portion of the take-off will occur
and, in the case of an ice covered runway, where braking would be used during a rejected
take-off.
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 performance data for varying conditions of
temperature, airport pressure altitude, and airplane weight for the specified take-off
conditions, for runways contaminated by ice, compacted snow or slush (or its equivalent, i.e.
standing water or loose snow).
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 on a Runway Contaminated with Ice
NOTE
Dispatch with one thrust reverser inoperative on a runway
contaminated with ice is not recommended.
(1) ANTI-ICING OFF
The take-off distance for a flaps-20° take-off with anti-icing off, on ice-contaminated
runways, is given by Figure 07−02−5.
The V1 speed for a flaps-20° take-off with anti-icing off, on ice-contaminated runways, is
given by Figure 07−02−6.
(2) ANTI-ICING ON
The take-off distance for a flaps-20° take-off with anti-icing on, on ice-contaminated
runways, is given by Figure 07−02−7.
The V1 speed for a flaps-20° take-off with anti-icing on, on ice-contaminated runways, is
given by Figure 07−02−8.
The charts are utilized in the same manner as described in the previous examples for wet
 
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本文鏈接地址:龐巴迪挑戰(zhàn)者604飛機飛行手冊CL604 Airplane Flight Manual 2(61)
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