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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.
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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).
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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.
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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.
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The wing anti-ice system must be ON when in icing conditions, or when ICE is annunciated by the ice detection system.
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Do not hold in icing conditions with the slats extended.
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When in icing conditions, maintain a minimum engine speed of 76% N2.
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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Twenty two (22), or
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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).
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.
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