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• 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 50, Apr 17, 2006 Flight Crew Operating Manual
CSP 700−6
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:
• Twenty two (22), or
• The number for which seating accommodation approved for take-off and landing is
provided.
G. Cold Weather Operations
Airplane operation in cold weather conditions is to be conducted in accordance with Flight
Crew Operating Manual, Volume 1, Chapter 7, SUPPLEMENTARY PROCEDURES − Cold
Weather Operations. The minimum ambient temperature approved for take-off is −40 °C
(−40 °F).
Take-off is prohibited with frost, ice, snow or slush adhering to any critical surface (wings,
horizontal stabilizer, vertical stabilizer, control surfaces, engine inlets and upper surface of the
fuselage).
WARNING
Even small amounts of frost, ice, snow or slush on the wing leading
edges and forward upper wing surface may adversely change the
stall speeds, stall characteristics and the protection provided by the
stall protection system, which may result in loss of control on
take-off.
NOTE
1. Comprehensive procedures for operating in cold weather are
provided in Flight Crew Operating Manual, Volume 1, Chapter 7;
SUPPLEMENTARY PROCEDURES − Cold Weather
Operations.
2. Take-off is permitted with frost adhering to the underside of the
wing that is caused by cold soaked fuel, in accordance with the
instructions provided in Flight Crew Operating Manual, Volume
1, Chapter 7; SUPPLEMENTARY PROCEDURES − Cold
Weather Operations − Pre-flight Preparation, External Safety
Inspection.
LIMITATIONS
OPERATING LIMITATIONS
Flight Crew Operating Manual REV 52, Nov 10, 2006
CSP 700−6
Volume 1
02−04−4
1. OPERATING LIMITATIONS (CONT'D)
H. Runway Surface Condition
Operations from unprepared (i.e. gravel, grass, etc.) runways are prohibited.
I. Minimum Enroute Climb Gradient and Clearance
It is recommended that the minimum enroute net climb gradient with one engine inoperative is
positive and all terrain and/or obstacles be cleared by at least 1,300 feet along the enroute
flight path.
LIMITATIONS
OPERATING LIMITATIONS
REV 52, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−04−5
LIMITATIONS
OPERATING LIMITATIONS
Flight Crew Operating Manual REV 50, Apr 17, 2006
CSP 700−6
Volume 1
02−04−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. ENGINE OPERATING LIMITS
A. Type
BR700−710A2−20, quantity two.
B. Engine Operating Limits Table
CONDITION CORE RPM N2 % FAN RPM N1 % ITT°C
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