Digital flygplanschecklista

Beechcraft

Beechcraft Baron B55 Garmin ACE-checklista

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Beechcraft

Beechcraft Baron B55 (BE55)
ACE

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Utforska Beechcraft Baron B55 (BE55)-checklistan

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Checklistor
35
Punkter totalt
388
Filformat
ACE

Endast förhandsvisning. Det här exemplet är ingen operativ checklista. Använd alltid gällande godkänd flygplansdokumentation.

01 PreflightWalk Around 67 punkter
  1. 01 Emergency Locator Transmitter ARMED
  2. 02 Location may vary with individual airplanes.
  3. 03 Cockpit
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02 PreflightBefore Starting 18 punkter
  1. 01 Seats POSITION AND LOCK
  2. 02 Seat Backs UPRIGHT
  3. 03 Seatbelts FASTEN
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03 PreflightStarting 25 punkter
  1. 01 Throttle Position APPROXIMATELY 1/2" OPEN
  2. 02 Propeller Control LOW PITCH (HIGH RPM)
  3. 03 Mixture Control FULL RICH
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04 PreflightAfter Starting and Taxi 5 punkter
  1. 01 CAUTION
  2. 02 Do not operate engine above 1200 RPM until oil temperature reaches 75 degrees F.
  3. 03 Brakes RELEASE AND CHECK
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05 PreflightBefore Takeoff 25 punkter
  1. 01 Seat Belts and Shoulder Harnesses CHECK
  2. 02 Parking Brake SET
  3. 03 Fuel Boost Pumps OFF
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06 In-FlightTakeoff 8 punkter
  1. 01 Takeoff Power: Full Throttle, 2625 RPM
  2. 02 Minimum Takeoff Oil Temperature: 75 degrees F
  3. 03 Power SET TAKE-OFF POWER (MIXTURE - SET FUEL FLOW TO ALTITUDE) BEFORE BRAKE RELEASE
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07 In-FlightMaximum Performance Climb 11 punkter
  1. 01 Power SET MAXIMUM CONTINUOUS POWER
  2. 02 Mixture LEAN TO APPROPRIATE FUEL PRESSURE
  3. 03 Cowl Flaps OPEN
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08 In-FlightCruise 8 punkter
  1. 01 Maximum Cruise Power: 24.5 in Hg at 2450 RPM
  2. 02 Recommended Cruise Power: 24.0 in Hg at 2300 RPM
  3. 03 Recommended Cruise Power: 22.0 in Hg at 2200 RPM
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09 In-FlightDescent 8 punkter
  1. 01 Altimeter SET
  2. 02 Cowl Flaps CLOSED
  3. 03 Windshield Defroster AS REQUIRED
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10 In-FlightBefore Landing 11 punkter
  1. 01 Seat Belts and Shoulder Harnesses FASTENED
  2. 02 Seat Backs UPRIGHT
  3. 03 Fuel Selector Valves CHECK MAIN TANKS
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11 In-FlightBalked Landing 7 punkter
  1. 01 Propellers LOW PITCH (HIGH RPM)
  2. 02 Power MAXIMUM ALLOWABLE
  3. 03 Airspeed BALKED LANDING CLIMB SPEED
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12 Post-FlightAfter Landing 5 punkter
  1. 01 Landing and Taxi Lights AS REQUIRED
  2. 02 Flaps UP
  3. 03 Trim Tabs SET TO ZERO
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13 Post-FlightShutdown 10 punkter
  1. 01 Parking Brake SET
  2. 02 Propellers HIGH RPM
  3. 03 Throttles 1000 RPM
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14 One Engine Inoperative ProceduresEngine Failure During Take-Off 5 punkter
  1. 01 Throttles CLOSED
  2. 02 Braking MAXIMUM
  3. 03 If insufficient runway remains for stopping:
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15 One Engine Inoperative ProceduresEngine Failure After Lift-off and In Flight 16 punkter
  1. 01 An immediate landing is advisable regardless of take-off weight. Continued flight cannot be assured if take-off weight exceeds the weight determined from the TAKE-OFF WEIGHT graph. Higher take-off weights will result in a toss of altitude w...
  2. 02 Landing Gear and Flaps UP
  3. 03 Throttle (inoperative engine) CLOSED
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16 Air StartAir Start 21 punkter
  1. 01 CAUTION
  2. 02 The pilot should determine the reason for engine failure before attempting an air start.
  3. 03 Fuel Selector Valve MAIN OR AUXILIARY
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17 Engine FireEngine Fire on the Ground 5 punkter
  1. 01 Mixture Controls IDLE CUT-OFF
  2. 02 Continue to crank affected engine
  3. 03 Fuel Selector Valves OFF
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18 Engine FireEngine Fire In Flight 7 punkter
  1. 01 Shut down the affected engine according to the following procedure and land immediately. Follow the applicable single-engine procedures in this section.
  2. 02 Fuel Selector Valve OFF
  3. 03 Mixture Control IDLE CUT-OFF
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19 Emergency DescentEmergency Descent 5 punkter
  1. 01 Propellers 2625 RPM
  2. 02 Throttles CLOSED
  3. 03 Airspeed 153 KTS (176 MPH)
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20 GlideGlide 5 punkter
  1. 01 Propellers FEATHER
  2. 02 Flaps UP
  3. 03 Landing Gear UP
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21 Landing EmergenciesGear-Up Landing 11 punkter
  1. 01 If possible, choose firm sod or foamed runway. When assured of reaching landing site:
  2. 02 Cowl Flaps CLOSED
  3. 03 Wing Flaps AS DESIRED
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22 Landing EmergenciesOne Engine Inoperative Landing 8 punkter
  1. 01 On final approach and when it is certain that the field can be reached:
  2. 02 Landing Gear DOWN
  3. 03 Flaps AS REQUIRED
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23 Landing EmergenciesOne Engine Inoperative Go-Around 6 punkter
  1. 01 WARNING
  2. 02 Level flight might not be possible for certain combinations of weight, temperature and altitude. In any event, DO NOT attempt a one engine inoperative go-around after flaps have been fully extended.
  3. 03 Power MAXIMUM ALLOWABLE
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24 Systems EmergenciesOne-Engine Inoperative Operation On Crossfeed 12 punkter
  1. 01 NOTE
  2. 02 The fuel crossfeed system is to be used only during emergency conditions in level flight only.
  3. 03 Left engine inoperative:
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25 Systems EmergenciesElectrical Smoke or Fire 10 punkter
  1. 01 Action to be taken must consider existing conditions and equipment installed:
  2. 02 Battery and Generator/Alternator Switches OFF
  3. 03 WARNING
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26 Systems EmergenciesIllumination of Over-voltage Light or Alternator Out Light(s) 16 punkter
  1. 01 In the event of the illumination of a single ALTERNATOR OUT light:
  2. 02 Check the respective loadmeter for load indication
  3. 03 a. No load - Turn off affected alternator
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27 Systems EmergenciesLanding Gear Manual Extension 11 punkter
  1. 01 Reduce airspeed before attempting manual extension of the landing gear.
  2. 02 LDG GR MOTOR Circuit Breaker PULL
  3. 03 Landing Gear Handle DOWN
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28 Systems EmergenciesLanding Gear Retraction After Practice Manual Extension 4 punkter
  1. 01 After practice manual extension of the landing gear, the gear may be retracted electrically, as follows:
  2. 02 Hand crank CHECK, STOWED
  3. 03 Landing Gear Motor Circuit Breaker IN
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29 Systems EmergenciesSurface Deice System 7 punkter
  1. 01 a. Failure of AUTO Operation
  2. 02 Surface Deice Switch MANUAL
  3. 03 Do not hold more than 8 seconds
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30 Systems EmergenciesElectrothermal Propeller Deice System 11 punkter
  1. 01 Loss of one alternator
  2. 02 Turn off unnecessary electrical equipment. Turn the prop deice system off while operating the cabin heater blower or the landing gear motor. Monitor electrical loads so as not to exceed alternator capacity of 1.0 on the loadmeter.
  3. 03 An abnormal reading on the Propeller Deice Ammeter indicates need for the following action:
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31 Systems EmergenciesEmergency Static Air Source System 6 punkter
  1. 01 THE EMERGENCY STATIC AIR SOURCE SHOULD BE USED FOR CONDITIONS WHERE THE NORMAL STATIC SOURCE HAS BEEN OBSTRUCTED. When the airplane has been exposed to moisture and/or icing conditions (especially on the ground), the possibility of obstruct...
  2. 02 Emergency Static Air Source - Valve OPEN
  3. 03 lower sidewall adjacent to pilot
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32 Systems EmergenciesEmergency Exits 4 punkter
  1. 01 Emergency exits, provided by the openable window on each side of the cabin, may be used for egress in addition to the cabin door and the optional cargo door. An emergency exit placard is installed below the left and right middle windows.
  2. 02 To open each emergency exit:
  3. 03 1. Lift the latch.
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33 Systems EmergenciesUnlatched Door in Flight 1 punkter
  1. 01 If the cabin door is not locked it may come unlatched in flight. This may occur during or just after take-off. The door will trail in a position approximately 3 to 4 inches open. Flight characteristics of the airplane will not be affected e...
34 Simulated One Engine InoperativeZero Thrust (Simulated Feather) 6 punkter
  1. 01 Use the following power setting (only on one engine at a time) to establish zero thrust. Use of this power setting avoids the difficulties of restarting an engine and preserves the availability of engine power.
  2. 02 The following procedure should be accomplished by alternating small reductions of propeller and then throttle, until the desired setting has been reached.
  3. 03 Propeller Lever RETARD TO FEATHER DETENT
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35 SpinsInadvertent Spin Entry 3 punkter
  1. 01 Immediately move the control column full forward, apply full rudder opposite to the direction of the spin and reduce power on both engines to idle. These three actions should be done as near simultaneously as possible; then continue to hold...
  2. 02 NOTE
  3. 03 Federal Aviation Administration Regulations did not require spin demonstration of airplanes of this weight; therefore, no spin tests have been conducted. The recovery technique is based on the best available information.

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