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96 Cards in this Set
- Front
- Back
Mmo (above 29,315)
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.721 Mach
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Vmo (8,000 to 29,315)
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276 knots
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Vmo (sea level to 8,000)
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261 knots
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Max Autopilot speed
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276 knots/.721 Mach
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Turbulent Air Penetration Speed
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180 knots
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Max Speed for flaps at Take-off/Approach (7 and 20)
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200 knots
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Max speed flaps land (35)
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172 knots
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Vle and Vlo
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172 knots
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Maximum Tire Ground Speed
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165 knots
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Minimum Speed in Sustained Icing
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160
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Vmca
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83 knots
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Vmcg
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73 knots
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Max Ramp Weight Limit
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15,300 pounds
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Maximum Takeoff Weight
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15,100 pounds
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Maximum Landing Weight
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14,400 pounds
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Zero Fuel Weight
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11,200 pounds
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Maximum Operating Altitude
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43,000 feet
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Maximum Landing/Take-off Altitude
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14,000 feet
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Maximum Take-off Altitude (Flaps 20)
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8,000 feet
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Maximum Ambient Temperature Take-off and Landing
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ISA +39 C
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Minimum Ambient Temperature Take-off and Landing
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-54 degrees C
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Maximum NiCad Battery Start Cycles
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Three starts per hour
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Generator Assisted Starts counts as....
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1/3 of a battery start
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Ground Power start counts as.......
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zero battery starts
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Airborne start counts as......
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one battery start
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Starter limitations
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Three starts in thirty minutes with a sixty second rest between starts
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Battery limitations (NiCad)
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Three starts in one hour
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Generator Load (inflight)
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300 amps
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Generator Load (continuous ground)
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225 amps
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Pitot-Static ground limit
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two minutes
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Thrust reverser maximum ground deployment time
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15 minutes in one hour
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Maximum Tailwind component
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10 knots
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Maximum Crosswind Component with thrust reverser
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25 knots
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Maximum Crosswind Component without thrust reverser
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29 knots
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Maximum Operating Oil Consumption
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one quart per four hours over a ten hour period
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Minimum oil temperature for starting
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-40 degrees
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Minimum battery voltage for starting (NiCad)
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24 volts
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Minimum/Maximum amps for ground power start
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800 and 1000 amps
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Maximum ITT on start
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700C for two seconds
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Maximum ITT for takeoff, two engines
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710C for five minutes
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Maximum ITT for takeoff, one engine
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710C for ten minutes
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Maximum ITT for flight, continuous
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690C
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Maximum N1
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106%
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Maximum N2
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97%
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Emergency Bus Items
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Com 1
Nav 2 Co-pilot's HSI Floodlights |
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Red AC Fail annunciator light
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Indicates power loss from an inverter. Automatic switch over to the other inverter occurs. Non-memory checklist
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Red Battery Overtemp Light
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Memory checklist:
Check amperage Battery to EMER Check amperage |
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Red Cabin Altitude Light
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Memory checklist:
O2 masks on and 100% O2 MIC O2 mask Emergency descent as required |
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Red Oil Press Warn Light
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Non-memory. Check gauge, go to checklist for what to do at different oil pressures.
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Amber Fuel Low Level Light
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Fuel quantity is down to 185 pounds or less.
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Amber Fuel Low Presure Light
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Fuel boost pump should activate automatically.
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Amber Hyd Flow Low light
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Indicates inoperative pump or pumps. If both pumps are inoperative refer to Hydraulic Failure checklist.
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Amber Engine Anti-Ice light
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If continuously illuminated, check N2 over 60%.
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Amber Ice Fluid Pump Fail
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Advisory. The surface pump will supply fluid for all surfaces.
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Amber GEN OFF light
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Indicates the generator power relay is open.
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Amber Inverter Fail 1 and 2
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In conjunction with the red AC FAIL light, tells which inverter failed.
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Amber EMERG PRESS ON
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Indicates air cycle machine shutdown or failure.
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Amber BLD AIR GND light
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The pressurization source selector is in GND position allowing more air to the ACM. Advancing power beyond 72% causes the valve to close, prohibiting too much air going to the ACM.
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Amber POWER BRAKES LOW PRESS
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Brake system pressure has dropped.
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Amber FUEL FLTR BYPASS light
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Possible power loss might occur. If it comes on at high altitude, probably ice crystals.
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Amber TAIL ICE FAIL light
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A pressure witch in the line between the tail proportioner and each horizontal stabilizer panel monitors each individual panel and illuminates the TAIL ICE FAIL light if the pressure falls too low.
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White SPEED BRAKE EXTEND light
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Speedbrakes on both wings are fully extended.
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Amber AIR DUCT O'HEAT light
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Air duct temperature is more than 157 degrees C. Most likely a large demand on the system for heat and most of the air is bypassing the cooling function of the ACM.
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Amber ACM O'PRESS light
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This malfunction should only occur on the ground with the GROUND selected with the pressurization source selector, the primary pressure switch has failed, and the right throttle is advanced beound approximately 74% N2.
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Amber ANTI-SKID INOP light
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Either the switch is off, or there is a fault in the system. If the brake system pressure drops below 750 psi, the ANTI-SKID INOP and the PWR BRK PRESS LO annunciators both illuminate.
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Amber DOOR NOT LOCKED light
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Indicates unlocked/unlatched nose or tailcone doors, failure or improper position of one or more door switches, and/or possible disengagement of the lower forward cabin door pin.
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Abmber F/W SHUT OFF light
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Operated by engine fire push switches. All electrical, fuel, and hydraulic systems are closed at applicable firewall.
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Amber ICING DETECTED light
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Ice has been detected. Turn on ice protection.
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Amber W/S AIR O'HEAT light
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Windshield bleed air is over 146 degrees C or, with the windshield heat OFF, the light activates if 5 psi pressure is sensed in the duct.
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Amber AOA HEATER FAIL
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If it comes on by itself, power to the Angle of Attack heater has failed.
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Amber ICE FLD LOW light
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Indicates approximately 20 minutes of surface and engine anti-ice protection available.
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Green ICE FLD SYS ON light.
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TKS system has been activated.
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Engine failure or fire during take-off, speed below V1
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Brakes-as required
Throttles-idle Speed brakes-extend |
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Engine failure or fire during take-off, speed above V1
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Positive rate-gear up
At level off altitude and V2+10, retract flaps and accelerate |
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Engine failure during coupled approach
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Increase engine power
Trim rudder Airspeed Vref+10 Flaps T.O and APP until landing assured |
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Amber ICE FLD LOW light
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Indicates approximately 20 minutes of surface and engine anti-ice protection available.
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Green ICE FLD SYS ON light.
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TKS system has been activated.
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Engine failure or fire during take-off, speed below V1
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Brakes-as required
Throttles-idle Speed brakes-extend |
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Engine failure or fire during take-off, speed above V1
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Positive rate-gear up
At level off altitude and V2+10, retract flaps and accelerate |
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Engine failure during coupled approach
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Increase engine power
Trim rudder Airspeed Vref+10 Flaps T.O and APP until landing assured |
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Engine fire
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Throttle-idle
If light remains... Engine fire switch, lift cover and push Illuminated bottle, push |
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Electrical fire or smoke
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Oxygen masks on
Oxygen microphone switches |
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Battery overheat
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Check amperage
Switch to EMER Check amperage |
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Cabin decompression
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Oxygen masks on
Oxygen masks mic on Emergency descent as required |
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Emergency descent
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AP trim disconnect
Throttles idle Speed brakes extend Airplane pitch attitude, initially 20 degrees pitch down |
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Autopilot hardover
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AP/Trim disengage switch, press
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Emergency restart-two engines
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Altitude below FL350
Airspeed 200 knots minimum Ignitions on Boost pumps on Throttles idle |
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Thrust reverser deploy during take-off
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Emergency stow switch EMER
Throttle idle Positive rate of climb, gear up Clear of obstacles and V2 +10, flaps up Maximum airspeed until stowed, 125 knots |
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Thrust reverser deploy inflight
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Emer stow switch, EMER
Throttle, idle Max airspeed, 125 knots |
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Thrust reverser unlock inflight
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Emer stow switch, EMER
Thrust reverser levers, full forward |
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Rapid decompression
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Oxygen masks on
Oxygen control valve, norm or manual drop Oxygen mike switches on Press source selector EMER Make sure passengers are getting oxygen Emergency descent |
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Emergency evacuation
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Parking brake set
Throttles cutoff Engine fire switch, press Fire bottles if required Battery off Evacuate |
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Oil capacity
|
2.08 gallons
|
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Fuel capacity
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862 gallons
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Switch the windshield heat to HI if the OAT is minus ____ or colder
|
18
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Swich the windshield heat to LO if the OAT is minus_____ or warmer.
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18
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