曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
only fuel in left and
right main tanks is
permitted in this zone.
MAX RAMP WEIGHT (48300 lb/21909 kg)
16.0%
45
40
21.0% 29.0% 38.0%
TAKE−OFF LIMIT
44750 lb/20298 kg
M.T.O.W
(48200 lb/21863 kg)
39500 lb/17917 kg
M.L.W. (38000 lb/17237 kg)
MIN FLIGHT WEIGHT (26000lb/11794 kg)
M.Z.F.W. (32000 lb/14515 kg)
43000 lb/19505 kg
28.0% @ 47700 lb/21637 kg)
Centre of Gravity Limits (MTOW 48,200 lb)
Figure 02−03−1
LIMITATIONS
Centre of Gravity
Vol. 1 02−03−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
LIMITATIONS
Centre of Gravity
Vol. 1 02−03−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. ALTITUDE AND TEMPERATURE OPERATING LIMIT
The altitude and temperature operating limit is as shown in Figure 02−04−1.
• Maximum airport pressure altitude for take-off and landing is 10,000 feet.
• Maximum operating altitude is 41,000 feet.
• Maximum ambient air temperature approved for take-off and landing is ISA + 35°C.
• Minimum ambient temperature approved for take-off is –40°C (–40°F).
• At altitudes above 25,000 feet, a safety harness must be worn by at least one pilot.
DFM0204_001 CHP1−01−17APR92
Altitude and Temperature Operating Limits
Figure 02−04−1
LIMITATIONS
Operating Limitations
Vol. 1 02−04−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
2. COLD WEATHER OPERATIONS
Take-off is prohibited with frost, ice, snow or slush adhering to any critical surface (wings,
horizontal stabilizer, vertical stabilizer, control surfaces, engine inlets and upper surface of the
fuselage).
WARNING
Even small amounts of frost, ice, snow or slush on the wing leading
edges and forward upper wing surface may adversely change the stall
speeds, stall characteristics and the protection provided by the stall
protection system, which may result in loss of control on take-off.
NOTE
1. Comprehensive procedures for operating in cold weather are
provided in Chapter 6; SUPPLEMENTARY PROCEDURES – COLD
WEATHER OPERATION .
2. Take-off is permitted with frost adhering to the underside of the wing
that is caused by cold soaked fuel, in accordance with the
instructions provided in Chapter 6; SUPPLEMENTARY
PROCEDURES – COLD WEATHER OPERATION – PRE-FLIGHT
PREPARATION – External Safety Inspection .
In addition to a visual check, a tactile check of the wing leading edge, wing forward upper surface
and wing rear upper surface is required during the External Walkaround inspection to determine
that the wing is free from frost, ice, snow or slush when the outside air temperature (OAT) is 5°C
(41°F) or less, or it cannot be determined that the wing fuel temperature is above 0°C (32°F);
and:
• There is visible moisture (rain, drizzle, sleet, snow, fog, etc); or
• Water is present on the wings; or
• The difference between the dew point temperature and the OAT is 3°C (5°F) or less; or
• The atmospheric conditions have been conducive to frost formation.
NOTE
Ice and frost may continue to adhere to wing surfaces for some time
even at outside air temperatures above 5°C (41°F).
LIMITATIONS
Operating Limitations
Vol. 1 02−04−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
3. OPERATION IN ICING CONDITIONS
During cold weather operations, the flight crew must ensure that the airplane fuselage, wings and
tail surfaces are free from ice, snow or frost.
AR Certified Airplanes
WARNING
Even small accumulations of ice on the wing leading edge can
change the stall speed, stall characteristics or the warning margin
provided by the stall protection computer.
A. Cowl Anti-ice System
(1) Ground Operations
The engine cowl anti-ice system must be on when the OAT is 10°C (50°F) or below and
visible moisture in any form is present (such as fog with visibility of one mile or less, rain,
snow, sleet and ice crystals).
The engine cowl anti-ice system must also be on when the OAT is 10°C (50°F) or below
when operating on runways, ramps, or taxiways where surface snow, ice, standing water
or slush is present.
(2) Flight Operations
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F) or below and
visible moisture in any form is encountered (such as clouds, rain, snow,
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者605机组操作手册 CL605-LIMITATIONS(3)
