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50 Cards in this Set
- Front
- Back
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Minimum flight crew |
Two pilots |
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May be flown day and night in |
Visual VFR instrument IFR and icing conditions |
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Maximum runway slope |
Plus or minus 2% of runway length |
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Runway surface |
Paved |
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Maximum tailwind component for takeoff and landing |
10 knots |
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minimum altitude |
-1000 feet |
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Maximum altitude for takeoff 145/er |
8,000 feet |
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Maximum altitude for takeoff 145 XR |
10,000 feet |
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Maximum altitude |
37,000 feet |
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Minimum static air temperature at -1000 feet |
-54 degrees Celsius |
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Minimum SAT for take off |
-40 degrees Celsius |
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Maximum SAT at -1000 feet |
52 degrees Celcius |
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Minimum SAT at 37,000 feet |
-65 degrees Celsius |
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Maximum SAT at 37,000 feet |
-21.5 degrees Celsius |
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Maximum SAT |
SAT +35 degrees Celcius |
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In the event of a landing below -40 degrees Celsius |
The airplane may not take off without a maintenance inspection |
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Total air temperature increase height above 25,000 feet is limited to |
-45 degrees Celcius. However if momentary deviations occur. - -50 degrees Celsius no maintenance action is required |
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Landing gear operation speed for retraction |
200 knots indicated |
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Landing gear operation speed for extension |
250 knots indicated |
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Landing gear extended speed |
250 knots indicated |
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Maneuver speed |
200 knots indicated |
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Maximum flap extended speed 9 degrees |
250 knots indicated |
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Maximum flap extended speed 18 degrees |
200 knots indicated |
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Maximum flap extended speed 22 degrees |
200 knots indicated |
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Maximum flaps extended speed 45 degrees EP / LR |
145 knots indicated |
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Maximum flap extended speed 45° XR |
160 knots indicated |
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Maximum flap extended speed above 10000 feet with yaw damper disengaged 22° XR |
180 knots indicated |
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Maximum flap extended speed above 10000 feet with yaw damper disengaged |
145 knots indicated |
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Maximum airspeed after take off during climb without retrimming |
160 knots indicated |
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Turbulent air penetration at or below 10000 feet |
200 knots indicated |
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Turbulent air penetration above 10,000 feet |
250 knots indicated or Mach .63 whichever is lower |
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Maximum windshield wiper operating |
170 knots indicated. Do not operate on dry windshield |
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Maximum permitted fuel imbalance between wing tanks |
800 pounds |
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Minimum fuel tank temperature |
-40 degrees Celsius |
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Maximum fuel tank temperature |
52 degrees Celsius |
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Minimum altitude for autopilot engagement |
500 feet AGL |
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Minimum altitude for autopilot disengagement during visual approach |
200 feet AGL |
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Minimum altitude during cat1 ILS approach for autopilot disengagement |
200 feet AGL |
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minimum altitude during cat 2 ILS approach for autopilot disengagement |
85 feet AGL |
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Minimum altitude during non-precision approach for autopilot disengagement |
Before leaving MDA |
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Maximum operating time on only batteries for integrated standby instrument system |
40 minutes |
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The maximum duration of battery power can be extended to |
45 minutes if the pit 03 sensor heating button is turned off when not operating in icing conditions |
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The airplane must not be moved during |
Power up initialization. Do not cage attitude in turning flight |
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Maximum altitude for flap extension |
20,000 feet |
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Maximum differential pressure |
7.8 psi |
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Maximum differential overpressure |
8.1 psi |
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Maximum differential negative pressure |
-.3 psi |
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Minimum temperature for manual anti-ice operation |
-40 degrees Celsius |
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Maximum temperature for manual anti-ice operation |
10 degrees Celsius |
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Holding configuration |
Landing gear up. Flaps 0. Minimum airspeed 200 knots indicated. |
