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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 700−1−WBM).
LIMITATIONS
CENTRE OF GRAVITY
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−03−1
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
FM8203_001
LIMITATIONS
CENTRE OF GRAVITY
Centre of Gravity (CG) Envelope
Figure 02−03−1
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−03−2
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
(If 43,091 kg (95,000 lb) MTOW placard is installed)
FM8203_002
Centre of Gravity (CG) Envelope
Figure 02−03−1
LIMITATIONS
CENTRE OF GRAVITY
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−03−3
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
(If 43,545 kg (96,000 lb) MTOW placard is installed)
FM8203_003
Centre of Gravity (CG) Envelope
Figure 02−03−1
LIMITATIONS
CENTRE OF GRAVITY
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−03−4
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
(If 44,452 kg (98,000 lb) MTOW placard is installed)
FM8203_004
Centre of Gravity (CG) Envelope
Figure 02−03−1
LIMITATIONS
CENTRE OF GRAVITY
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−03−5
LIMITATIONS
CENTRE OF GRAVITY
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−03−6
THIS PAGE INTENTIONALLY LEFT BLANK
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).
LIMITATIONS
OPERATING LIMITATIONS
DOT Approved
REV 52, Nov 10, 2006
Airplane Flight Manual
CSP 700−1A
02−04−1
1. OPERATING LIMITATIONS (CONT'D)
A. Altitude and Temperature Operating Limit (Cont’d)
FM0204_002
LIMITATIONS
OPERATING LIMITATIONS
Altitude and Temperature Operating Limit
Figure 02−04−1
DOT Approved
REV 52, Nov 10, 2006
Airplane Flight Manual
CSP 700−1A
02−04−2
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].
• 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.
• The engine cowl anti-ice system must be ON, when in icing conditions, or when ICE is
annunciated by the ice detection system.
(2) WING ANTI-ICE SYSTEM
Ground Operations:
• During take-off, use of the wing anti-ice system in AUTO is prohibited.
• The wing anti-ice system must be ON for take-off when the OAT is 5 °C (41 °F) or
below and visible moisture in any form is present (such as fog with visibility of 1,500
meters (one mile) or less, rain, snow, sleet and ice crystals).
• The wing anti-ice system must also be ON for take-off when the OAT is 5 °C (41 °F) or
below and the runway is contaminated with surface snow, slush or standing water.
• When SAE Type II, Type III or Type IV anti-icing fluids have been applied, the wing
　
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