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be closed and one airconditioning
pack must be shutdown for takeoff.
(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 airconditioning
pack must be shutdown
for landing.
LIMITATIONS
STRUCTURAL WEIGHT
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
02−02−2
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 700−1−WBM).
LIMITATIONS
CENTRE OF GRAVITY
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
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
Flight Crew Operating Manual REV 42, Nov 26, 2004
CSP 700−6
Volume 1
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
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
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
Flight Crew Operating Manual REV 42, Nov 26, 2004
CSP 700−6
Volume 1
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
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−03−5
LIMITATIONS
CENTRE OF GRAVITY
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
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
REV 52, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 1
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
Flight Crew Operating Manual REV 52, Nov 10, 2006
CSP 700−6
Volume 1
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.
　
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