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NOTE
The maximum take-off weight (MTOW) and/or maximum landing weight (MLW) may be further limited due to performance considerations.
B. Buoyancy Limitations
(1) TAKE-OFF ON RUNWAYS NEAR BODIES OF WATER
. For take-off at weights above the maximum landing weight, OUTFLOW VLV 2 must be closed and one air-conditioning pack must be shutdown for take-off.
(2) LANDING ON RUNWAYS NEAR BODIES OF WATER
. For forced / emergency landing at weights above the maximum landing weight, OUTFLOW VLV 2 must be closed and one air-conditioning pack must be shutdown for landing.
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1. CENTRE OF GRAVITY
A. Centre Of Gravity Limits
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02.03.1.
The airplane including interior payload, passengers and fuel must be loaded such that the airplane weight and centre of gravity are maintained within the specified limits (including any variation due to fuel consumption, passenger movement, retraction of landing gear, etc. ).
The airplane must be loaded in accordance with the loading instructions associated with the Weight and Balance Manual (BD 700.1A11.WBM).
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
Centre of Gravity (CG) Envelope
Figure 02.03.1
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
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1. OPERATING LIMITATIONS
A. 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 51,000 feet.
Maximum ambient air temperature approved for take.off and landing is +50 °C (122 °F).
Minimum ambient temperature approved for take-off is .40 °C (.40 °F).
1. OPERATING LIMITATIONS (CONT'D)
A. Altitude and Temperature Operating Limit (Cont’d)
Altitude and Temperature Operating Limit
Figure 02.04.1
1. OPERATING LIMITATIONS (CONT'D)
B. Operation in Icing Conditions
(1) COWL ANTI-ICE SYSTEM
Ground Operations:
.
During take-off, use of cowl anti-ice in AUTO mode is prohibited.
.
The 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 a visibility of 1,500 meters (one mile) or less, rain, snow and ice crystals].
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The cowl anti-ice 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.
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, sleet or ice crystals), except when the SAT is .40 °C (.40 °F) or below.
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