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The wing anti-ice system must be on:
At or above 22,000 feet:
.
when ice is indicated by the ice detection system, or
.
when in icing conditions, if an ice detector has failed.
Below 22,000 feet:
.
when in icing conditions, or
.
when ice is indicated by the ice detection system.
C. Super-Cooled Large Droplet Icing
Continued operation in areas where super-cooled large droplet (SLD) icing conditions exist is prohibited.
SLD icing conditions are indicated by ice accretion on the flight compartment side windows.
.
The wing anti-icing system must be ON in SLD icing conditions.
.
The cowl anti-icing system must be ON in SLD icing conditions.
.
Leave icing conditions when side window icing occurs.
4. RUNWAY SLOPES The maximum runway slopes approved for take-off and landing are: +2% (uphill) –2% (downhill)
5. TAILWIND CONDITIONS
The maximum tailwind component approved for take-off and landing is 10 knots.
6. MINIMUM FLIGHT CREW
The minimum flight crew is one pilot and one copilot.
7. MAXIMUM OCCUPANTS
The total number of occupants, including no more than nineteen passengers, must not exceed the lesser of the following:
.
Twenty-two or,
.
The number for which seating accommodation approved for take-off and landing is provided.
LIMITATIONS Operating Limitations Vol. 1 02.04.5
Oct 05/06
8. MAXIMUM CROSSWIND COMPONENT
AR Certified Airplanes The maximum crosswind component for take-off and landing is 24 knots (12 meters/sec).
SAAU Certified Airplanes The maximum crosswind component for take-off and landing on a dry runway is 24 knots (12 meters/sec). The maximum crosswind component for take-off and landing on a wet runway with water depth no more than 3.00 mm (0.125 inch) is defined in the following table for different values of the coefficient of friction: REPORTED COEFFICIENT OF FRICTION MAXIMUM CROSSWIND COMPONENT 0.3 (poor braking) 10 knots (5 meters/sec) 0.4 (average braking) 15 knots (8 meters/sec) 0.5 (good braking, equivalent to dry) 24 knots (12 meters/sec) The maximum crosswind component for take-off and landing on a contaminated runway is 10 knots (5 meters/sec). Operation on runways with a coefficient of friction less than 0.3 is prohibited.
SAAU Certified Airplanes 9. GROUND OPERATIONS IN HIGH WIND CONDITIONS In the event that the airplane is parked and sustains winds or gust loads in excess of 27 meters/second, an inspection and functional check of the aileron, elevator and rudder power control units is required.
SAAU Certified Airplanes 10. MINIMUM ENROUTE CLEARANCE It is recommended that all terrain and/or obstacles be cleared by at least 1,300 feet along the enroute flight path.
SAAU Certified Airplanes 11. MINIMUM GO-AROUND ALTITUDE Demonstrated minimum altitude for all engines go-around without touching the ground is 50 feet and for single engine go-around is 100 feet.
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