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22
20
A/C WEIGHT (kg)
THOUSANDS
DFM0203_004
A/C WEIGHT (lb)THOUSANDS
40
18
16
35
14
30
12
25 2530 35
40 A/C CG % MAC
Centre of Gravity Limits (MTOW 48,200 lb) Figure 02.03.1
CL.605 Flight Crew Operating Manual
PSP 605.6
LIMITATIONS Centre of Gravity Vol. 1 02.03.2
Oct 05/06
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CL.605 Flight Crew Operating Manual
PSP 605.6
LIMITATIONS Operating Limitations Vol. 1 02.04.1
Oct 05/06
1. ALTITUDE AND TEMPERATURE OPERATING LIMIT
The altitude and temperature operating limit is as shown in Figure 02.04.1.
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Maximum airport pressure altitude for take-off and landing is 10,000 feet.
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Maximum operating altitude is 41,000 feet.
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Maximum ambient air temperature approved for take-off and landing is ISA + 35°C.
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Minimum ambient temperature approved for take-off is –40°C (–40°F).
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At altitudes above 25,000 feet, a safety harness must be worn by at least one pilot.
LIMITATIONS Operating Limitations Vol. 1 02.04.2
Oct 05/06
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).
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:
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There is visible moisture (rain, drizzle, sleet, snow, fog, etc); or
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Water is present on the wings; or
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The difference between the dew point temperature and the OAT is 3°C (5°F) or less; or
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