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66 Cards in this Set
- Front
- Back
Max ramp weight
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29,300lbs
|
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Max takeoff weight
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29,000lbs
|
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Max zero fuel weight
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26,500lbs
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Max landing weight
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28,500lbs
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Max operating altitude
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25,000ft PA
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Flaps may be extended up to
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13,999 MSL
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Max tailwind component for takeoff and landing is
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10 kts
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Max operating speed (Vmo) from 0 to 16,000ft MSL
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250 KIAS
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Max operating speed (Vmo) at 25,000ft MSL
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210 KIAS
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Flaps extended speed (Vfe) for flaps 7 or 15 degrees
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175 KIAS
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Flaps extended speed (Vfe) for flaps 20 degrees
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165 KIAS
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Maneuvering speed
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180 KIAS
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Landing gear retraction speed (Vlor)
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150 KIAS
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Landing gear extension speed (Vloe)
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200 KIAS
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Landing gear extended speed (Vle)
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200 KIAS
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Emergency extension speed (Vloee)
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200 KIAS
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Rough air penetration speed (Vra) up to 21,000ft
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190 KIAS
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Rough air penetration speed (Vra) above 21,000ft
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Vmo pointer - 30 kts
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Minimum climb speed in icing conditions
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Vclean + 15 kts (160 KIAS best)
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Minimum en route speed in icing conditions
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160 KIAS
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Minimum approach speed with ice
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Vref + 10 kts
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Take off power with APR or go around (5 minutes max)
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107 percent torque
940 degrees C ITT |
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Take off power with APR or go around (2 minutes max)
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107 percent torque
950 degrees C ITT |
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Takeoff power (5 minutes max)
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100 percent torque
917 degrees C ITT |
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Takeoff power (2 minutes max)
|
100 percent torque
927 degrees C ITT |
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Max continuous power (OEI)
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100 percent torque
940 degrees C ITT |
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Transient except takeoff (max 12 seconds)
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112 percent torque
965 degrees C ITT |
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Maximum ITT at engine start
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965 degrees C
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At takeoff power, what is the min-max engine oil pressure?
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30-100 psi
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At takeoff power, what is the min-max engine oil temperature?
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35-122 degrees C
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At takeoff power, what is the min-max propeller oil pressure?
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25-140 psi
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At takeoff power, what is the min-max propeller oil temperature?
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45-77 degrees C
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Total usable fuel per tank
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2845 lbs
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Total usable fuel (both tanks)
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5690 lbs
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Fuel temperature range
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-40 to +43 degrees C
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FUEL LOW TEMP light must be off for
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Takeoff
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For takeoff and landing X FEED and CONN VALVE shall be
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Off and closed
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Max fuel imbalance between tanks
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200 lbs
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Minimum oil temperature for starting
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-40 degrees C
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Prop RPM limitation on ground, unless needed for normal taxi
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1070-1220 rpm
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Two start attempts with fuel introduced require how much cooling between, and how much cooling before subsequent starts
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3 minutes and 25 minutes
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Three 30 second dry motoring with ______ cooling between each, then a ____ cooling period between subsequent starts or motoring
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3 minutes and 1 hour
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Time to lightoff from fuel introduction to ITT rise is
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20 seconds maximum
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Minimum time between starts is
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1 minute
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You must notify maintenance after ____ hung starts
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Two
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Takeoff is prohibited with with either L or R battery above
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64 degrees C
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Cross generator start with either L or R battery is prohibited above
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60 degrees C
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Battery start is prohibited with either L or R battery temp min/max
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Between -20 degrees C and +57 degrees C
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Minimum battery temperature for takeoff is
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-20 degrees C
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Max load on DC generators for 5 minutes is
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600 amps
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DC generator voltage range is
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27.5 to 29 volts
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External power voltage range is
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28 to 29.5 volts
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Takeoff is prohibited after a failed
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battery start
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Maximum tire ground speed is
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165 knots
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Min dispatch oxygen pressure below 10,000 ft MSL is
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800 psi
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Maximum cabin differential pressure is
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7.5 psi
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X VALVE use is limited to
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Ground operations only
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Aft supplemental air conditioning unit may not be used above
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17,500 ft MSL
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After an aborted takeoff with normal braking, _____ cooling time is adequate
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15 minutes
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Engine anti-ice must be ON when the plane is in visible moisture and the temperature is
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+10 degrees C or colder
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After exiting icing conditions, engine anti-ice must remain on for
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5 minutes
|
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During AP operations in icing conditions, the only vertical mode to be used during climb is
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FD/AP IAS
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When is AP and yaw damper operation not authorized
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Takeoff, landing, and go-around
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Minimum altitude for AP operations en route is
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500 ft AGL
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Minimum AP operating altitude for approaches is
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50 ft below MDA/DA
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Minimum autopilot operation altitude for takeoff or go-around is
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500 ft
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