Digital aircraft checklist

Beechcraft

Beechcraft King Air 200 Checklist Template

Bring the Beechcraft King Air 200 into ACE with a structured, editable template designed for a faster and more deliberate setup.

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Beechcraft

Beechcraft King Air 200
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Checklists
37
Total items
561
File format
ACE

Preview only. This sample is not an operational checklist. Always use the applicable approved aircraft documentation.

01 PreflightPreflight Inspection 90 items
  1. 01 Cockpit:
  2. 02 Control Locks REMOVE
  3. 03 Elevator Trim SET TO "0"
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02 PreflightBefore Engine Starting 56 items
  1. 01 Cabin Door/Cargo Door LOCKED
  2. 02 Check cabin door security by attempting to turn handle toward unlocked position without depressing release button. Handle should not move. Check cargo door security by opening handle access panels and attempting to open cargo door latches w...
  3. 03 WARNING
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03 PreflightUse of External Power 18 items
  1. 01 CAUTION
  2. 02 Never connect an external power source to the airplane unless a battery indicating a charge of at least 20 volts is in the airplane. If the battery voltage is less than 20 volts, the battery must be recharged, or replaced with a battery ind...
  3. 03 When an auxiliary power source is used, ascertain that the polarity of the APU is the same as that of the airplane. If polarity of the APU is unknown, use a voltmeter to assure correct polarity before connecting it to the airplane.
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04 PreflightEngine Starting 40 items
  1. 01 On serials 88-2 through 88-36
  2. 02 (except those serials modified per Service Instructions No 070.1-356)
  3. 03 The BATTERY CHG annunciator will illuminate 4 to 6 seconds after Right ignition and Engine Start switch is on.
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05 PreflightEngine Clearing 6 items
  1. 01 Condition Lever CUTOFF
  2. 02 Ignition and Start Switch STARTER ONLY
  3. 03 for a minimum of 15 seconds
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06 PreflightAfter Starting, and Taxiing 10 items
  1. 01 Inverter ON
  2. 02 DC Voltage and Load Meters CHECK
  3. 03 AC Voltage and Frequency CHECK
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07 PreflightBefore Takeoff (Runup) 61 items
  1. 01 Avionics and Radar CHECK
  2. 02 Pressurization SET
  3. 03 Autopilot CHECK
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08 PreflightBefore Takeoff (Final Items) 6 items
  1. 01 Bleed Air Valves OPEN
  2. 02 Annunciator Lights EXTINGUISHED
  3. 03 or considered
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09 PreflightTakeoff Roll 5 items
  1. 01 Autofeather Annunciators ILLUMINATED
  2. 02 Ignition On Annunciators EXTINGUISHED
  3. 03 Refer to PERFORMANCE Section for minimum take-off power, take-off speed, distance and climb data.
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10 In FlightClimb 12 items
  1. 01 Landing Gear UP
  2. 02 Flaps UP
  3. 03 Yaw Damp ON
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11 In FlightCruise 9 items
  1. 01 WARNING
  2. 02 Do not lift Power Levers in flight.
  3. 03 Cruise Power SET
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12 In FlightDescent 9 items
  1. 01 Cabin Pressurization Controller SET
  2. 02 Cabin Altitude Selector Knob SET
  3. 03 Rate Control Selector Knob SET INDEX AT 12-0'CLOCK POSITION.
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13 In FlightApproach 13 items
  1. 01 CAUTION
  2. 02 Propeller operation in the range of 1750-1850 RPM should be avoided as it may cause ILS glide slope interference.
  3. 03 To ensure constant reversing characteristics, the propeller control must be in FULL INCREASE RPM position.
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14 In FlightLanding 7 items
  1. 01 Landing Assured:
  2. 02 Flaps DOWN
  3. 03 Yaw Damp OFF
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15 PostflightAfter Landing 6 items
  1. 01 Landing and Taxi Lights AS REQUIRED
  2. 02 Ice Protection OFF
  3. 03 Engine Auto-Ignition OFF
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16 PostflightShutdown and Securing 28 items
  1. 01 Parking Brake SET
  2. 02 Inverter OFF
  3. 03 Avionics Master OFF
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17 LandingsMaximum Reverse Thrust Landing 6 items
  1. 01 Condition Levers HIGH IDLE
  2. 02 Propeller Levers FULL FORWARD
  3. 03 Power Levers LIFT AND REVERSE AFTER TOUCHDOWN
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18 LandingsBalked Landing 6 items
  1. 01 Power MAXIMUM ALLOWABLE
  2. 02 Airspeed ESTABLISH 100 KNOTS
  3. 03 When clear of obstacles:
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19 Engine FailureEmergency Engine Shutdown 11 items
  1. 01 ENGINE TORQUE INCREASE - UNSCHEDULED (Ground or Flight) (Not Responsive to Power Lever Movement) ENGINE FIRE IN FLIGHT ENGINE FAILURE IN FLIGHT ILLUMINATION OF MAGNETIC CHIP DETECTOR ANNUNCIATOR
  2. 02 Affected Engine:
  3. 03 Condition Lever CUTOFF
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20 FireEngine Fire On Ground 6 items
  1. 01 Affected Engine:
  2. 02 Condition Lever CUT-OFF
  3. 03 Fuel Firewall Valve CLOSED
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21 FireLanding Gear Retraction After Practice Manual Extension 7 items
  1. 01 After a practice manual extension of the landing gear, the gear may be retracted electrically as follows:
  2. 02 Emergency Engage Handle ROTATE CCW
  3. 03 and push down
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22 Environmental SystemsPressurization System 8 items
  1. 01 Differential Pressure in Red
  2. 02 Any time differential pressure goes into the Red Arc:
  3. 03 Cabin Altitude Controller SELECT HIGHER SETTING
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23 Environmental SystemsLoss of Pressurization 3 items
  1. 01 In the event of pressurization loss at high altitude:
  2. 02 Oxygen USE
  3. 03 Descend AS REQUIRED
24 Environmental SystemsAuto-Deployment Oxygen System 5 items
  1. 01 In the event the PASS OXY ON annunciator does not illuminate following illumination of the ALT WARN annunciator:
  2. 02 First aid mask can only be deployed manually.
  3. 03 to deploy passenger masks.
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25 Environmental SystemsIllumination of "Duct Overtemp" Annunciator (If Installed) 6 items
  1. 01 Cabin Temp Knob SELECT LOWER TEMPERATURE
  2. 02 Vent Blower HI POSITION
  3. 03 Cabin Air Knob PUSH TO INCREASE
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26 Environmental SystemsBleed Air Line Failure Warning System 9 items
  1. 01 Warning
  2. 02 Annunciators should be monitored during engine start procedure. Either engine will extinguish both annunciators Upon starting.
  3. 03 Illumination of a warning annunciator in flight
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27 Ice Protection SystemsElectrothermal Propeller Deice (Auto System) 31 items
  1. 01 Abnormal Readings on Deice Ammeter.
  2. 02 Normal operation: 14 to 18 amps:
  3. 03 Zero Amps:
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28 Ice Protection SystemsElectrothermal Propeller Deice (Manual System) 8 items
  1. 01 On Airplanes
  2. 02 BB-Z, BB-6 thru BB-875, BB-877 the BB-824, BL-7 thru BL-29:
  3. 03 To use manual system, hold switch in outer position for approximately 30 seconds, then in inner position for approximately 30 seconds.
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29 Ice Protection SystemsEmergency Exit 7 items
  1. 01 Emergency Exit Handle PULL
  2. 02 This is a plug-type door and opens into the cabin
  3. 03 CAUTION
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30 Static Air SystemPilot's Alternate Static Air Source 9 items
  1. 01 The pilot's alternate static air source should be used for conditions where the normal static source has been obstructed.
  2. 02 Pilot's Static Air Source ALTERNATE 2
  3. 03 Right Side Panel
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31 SpinsInadvertent Spin Entry: 11 items
  1. 01 Control Column FULL FORWARD
  2. 02 Rudder APPLY FULL
  3. 03 opposite direction of spin
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32 SpinsIllumination of Cabin Door Warning Light (200) Warning 6 items
  1. 01 Do not attempt to check the security of the airstair door in flight. Remain as far from the door as possible with seatbelts securely fastened until the airplane has landed.
  2. 02 The cabin-door locking mechanism must be in the over-centered position (indicated by positioning of safety arm around the diaphragm plunger) in order to provide complete positive locking of the cabin door.
  3. 03 If cabin is pressurized and door is not completely locked, any movement of the door handle toward the unlocked position may cause rapid, complete unlocking and opening of the door.
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33 SpinsIllumination of Cabin/Cargo Door Warning Light (200C) Warning 5 items
  1. 01 Do not attempt to check the security of either the airstair door or cargo door in flight. Remain as far from the door as possible with seatbelts securely fastened until the airplane has landed.
  2. 02 If the cabin is pressurized and either door is not completely locked, any movement of a door handle toward the unlocked position may cause rapid, complete unlocking and opening of the door.
  3. 03 1. If cabin/cargo door warning light on annunciator panel indicates that cabin/cargo door may not be secure, depressurize cabin (consider Altitude before depressurizing cabin) by activating cabin pressurization dump switch on pedestal •
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34 SpinsCracked or Shattered Windshield 16 items
  1. 01 The following procedure should be used when one or more cracks occur in the inner or outer ply of the windshield. The procedure is also applicable if the windshield shatters. This usually occurs in the inner ply and is characterized by a mu...
  2. 02 Altitude MAINTAIN 25,000 FT OR LESS
  3. 03 If possible
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35 SpinsCrack in Any Side Window (Cockpit or Cabin) 7 items
  1. 01 Altitude DESCEND IF REQUIRED
  2. 02 Descend to an Altitude not requiring oxygen, if possible, or descend to at least 25,000 feet if passengers are on board.
  3. 03 Crew and Passengers DON OXYGEN MASKS
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36 SpinsSimulating One-Engine-Inoperative (Zero Thrust) 5 items
  1. 01 When establishing zero thrust operation, use the power setting listed below. By using this power setting to establish zero thrust, one avoids the inherent delays of restarting a shut-down engine and preserves almost instant power to counter...
  2. 02 Propeller 1600 RPM
  3. 03 Power Lever SET 120 FT-LBS TORQUE
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37 IcingExiting Severe Icing: 13 items
  1. 01 ATC REQUEST PRIORITY HANDLING
  2. 02 Crack in Any Side Window (Cockpit or Cabin)
  3. 03 If autopilot is not engaged:
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Source checklist: Beechcraft King Air 200 Checklist

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