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30 Cards in this Set
- Front
- Back
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An ___ knot range on the airspeed scale is always in view
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80
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____ 100 amp, tarnsformer rectifier units convert the AC supply to 28 volts DC and power the airplanes buses.
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5
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The ADG (Air Driven Generator) is automatically deployed if there is a complete _____ failure.
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AC Power
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The ADG is pushed into the airstream where ___ turns the turbine
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Ram Air
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The main generators are ____, 115 VAC, three phase, 400 HZ , integrated driver generators.
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30 KVA
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Power to the AC service bus is supplied directly from the ____ or the ____.
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External Power receptacle / APU Generator
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The AC Service bus is supplies power to those circuits mecessary for ____, without having to energize the remainer of the electrical system.
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Ground Servicing Operations
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The APU bleed air directly feeds the right side of the 10th stage manifold to feed the right pack.
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False, The left pack
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In case of failure of both packs, ____ can be used as the sole source of ventilation
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Ram Air
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The left pack primarily supplies the flight compartment ___% and supplements the flow to the passenger cabin ___%
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70/30
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In the air conditioning system the dual bypass valves modulate as necessary to blend bypassed hot air with cooled air cycle machine air to achieve the selected temperature.
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True
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Pack fault Light indicates a(an) ___ or ___ condition has been detected
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Over pressure/Over temperature
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If live cargo is being transported at high ambient temperatures, the cargo switch should be only be set to ___ after takeoff
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COND AIR
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The CPKT and CABIN temp control knobs adjust the temp setting for the related compartment
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TRUE
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Rotation of the V/S pitch wheel changes the pitch reference value by ____ degrees per click.
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1/2
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The vertical takeoff mode generates a ____ degree pitch up flight director command. Loss of an engine limits the pitch up comment to ___ degrees.
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15,10
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Go-around mode generates a ___ degree pitch up command
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10
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Automatic switch over from IAS to Mach occurs when climbing through ___ feet 31,600 (AFM)
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True
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The square HDG push button on the FCP selects or deselects the heading mode.
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True
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When a pilot selects a HDG change > ____ degrees, the aircraft will initiate a roll in the direct of the selected heading change.
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180
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Aircraft limitations prohibit the use of ____ submode during approach (either FD or autopilot coupled)
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DES
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Automatic transition to half-bank mode occurs when climbing above ___ feet (PA) or if the airplane is above half-bank transition altitude when the flight director is engaged
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31,600
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Half bank mode reduces the maximum command bank angle to ___ degrees
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15
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Traffic advisories (TA) indicate the relative positions of intruding airplanes that are about ___ seconds from the closest point of approach (CPA) and may require a later resolution advisory.
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40
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The TCAS resolution advisory programs are based on the pilot initiating the RA manuever within approximately ___ seconds
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5
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Pitch-Limit Indicator (PLI) (yelllow) displayed during wind shear warning or alert for a minimum of ___ seconds, it displays the maximum pitch attitude that can be made before encounting the stall angle-of-attack.
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60
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For aircraft equipped with Mach transducers, each Mach transducer supplies primary Mach compensation data to the ____ computer
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stall protection
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The radio altimeter provides absolute altitude in a range of 0 to ___ feet
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2500
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The AUTO X FLOW INHIB - EICAS message will remain if the fueler leaves the power switch on the Refuel/Defuel control panel selected ON.
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True, will be manual and not be able to do automatically.
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The green low speed awareness indicator bar indicates ___ times the computed stall speed.
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1.27
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