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and airplanes 5301 to 5571 NOT incorporating Service Bulletin 604−27−009 or 604−27−012:
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−4.
The airplane including interior payload, passengers and fuel (refer to Figure 02−05−2) must be
loaded such that the airplane weight and centre of gravity are maintained within the specified limits
(including variations due to fuel consumption, passenger movement, retraction of landing gear,
etc.).


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
Centre of Gravity Limits (MTOW 47,600 lb)
Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604−28−007 and
airplanes 5301 to 5571 NOT incorporating Service Bulletin 604−27−009 or 604−27−012
Figure 02−03−4





     







 



 







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+67/0.26./4869
,234:826486;2;
<.,:244.926432;-+6.

REV 58, Dec 05/05
@Figure 02–04–1@Altitude and Temperature Operating Limits
Figure 02–04–1
LIMITATIONS
Operating Limitations
02–04–1
1. ALTITUDE AND TEMPERATURE OPERATING LIMIT (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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 2, Nov 30/95
LIMITATIONS
Operating Limitations
02–04–2
2. 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.
A. Cowl Anti-ice System
(1) Ground Operations
The engine cowl anti-ice system must be on when the OAT is 10C (50F) 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 10C (50F) 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 10C (50F) or
below and visible moisture in any form is encountered
(such as clouds, rain, snow, sleet or ice crystals), except
when the SAT is –40C (–40F) or below.
The engine cowl anti-ice system must be on:
At or above 22,000 feet:

when ice is indicated by the ice detection system, or

when in icing conditions, if an ice detector has failed.
Below 22,000 feet:

when in icing conditions, or

when ice is indicated by the ice detection system.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 50, Mar 28/03
@Figure 02–04–1@Altitude and Temperature Operating Limits
Figure 02–04–1
LIMITATIONS
Operating Limitations
02–04–1
1. ALTITUDE AND TEMPERATURE OPERATING LIMIT (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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 2, Nov 30/95
LIMITATIONS
Operating Limitations
02–04–2
2. OPERATION IN ICING CONDITIONS
　
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