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Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−03−2
1. CENTRE OF GRAVITY (CONT'D)
A. Centre Of Gravity Limits (Cont’d)
Aircraft incorporating 40,687 kg (89,700 lb) MTOW placard
Centre of Gravity (CG) Envelope
Figure 02−03−1
LIMITATIONS
CENTRE OF GRAVITY
REV 13, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−03−3
LIMITATIONS
CENTRE OF GRAVITY
Flight Crew Operating Manual REV 8, Jan 05, 2006
CSP 700−5000−6
Volume 1
02−03−4
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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).
LIMITATIONS
OPERATING LIMITATIONS
REV 13, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−5000−6
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 13, Nov 10, 2006
CSP 700−5000−6
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.
• 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
anti-ice system must only be selected ON, if required, just prior to thrust increase for
take-off.
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 wing anti-ice system must be ON when in icing conditions, or when ICE is
annunciated by the ice detection system.
• Do not hold in icing conditions with the slats extended.
• When in icing conditions, maintain a minimum engine speed of 76% N2.
LIMITATIONS
OPERATING LIMITATIONS
REV 11, Apr 17, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−04−3
1. OPERATING LIMITATIONS (CONT'D)
C. Runway Slopes
The maximum runway slopes approved for take-off and landing are:
+2% (uphill)
−2% (downhill)
D. Tailwind Conditions
The maximum tailwind component approved for take-off and landing is 10 knots.
E. Minimum Flight Crew
The minimum flight crew is one pilot and one copilot.
F. Maximum Occupants
The total number of occupants, including no more than nineteen (19) passengers, must not
exceed the lesser of the following:
　
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