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53 Cards in this Set
- Front
- Back
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CONDITION: An attempt to bank the aircraft to the left results in no lateral movement of the
wings. Which statement best describes the problem and a solution? |
Ailerons jammed; 1st Officer controls roll with spoilers
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Which answer is correct regarding elevator feel system operation?
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Operates with either "A” or "B" system pressure available
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What does an illuminated elevator FEEL DIFF PRESS light indicate?
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Excessive differential pressure is sensed by the elevator feel computer with the flaps UP
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Which statement is correct for mach trim system operation?
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Operates automatically above .615 mach and moves the elevator
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How is a mach trim system, single channel failure indicated?
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MACH TRIM FAIL light, FLT CONT annunciator and MASTER CAUTION lights come on
when recall is activated |
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Which statement is correct for the stabilizer trim system?
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Main electric trim speed is faster with flaps extended
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What is the function of the STAB TRIM CUTOUT switches? (300/500)
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Shuts off autopilot and main electric trim motors
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What action is required to stop a runaway stabilizer trim?
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Move control column in opposite direction of runaway trim to remove power from both
autopilot and main electric trim motors |
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Which statement contains some of the conditions necessary for the automatic speed trim system
to function? |
During low speed flight, at a low gross weight, and with an aft CG, it uses the autopilot
stab trim to trim the aircraft |
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What indicates to the crew that the speed trim system is operating?
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Stabilizer trim wheel rotates at autopilot stab trim speed with the autopilot not engaged
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How is a dual channel speed trim failure indicated?
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SPEED TRIM FAIL, FLT CONT annunciator, and MASTER CAUTION lights illuminate
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Which answer best describes the operation of the rudder?
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Powered by either "A”, “B”, or Standby hydraulic systems
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Which statement is correct regarding the aileron and rudder trim systems?
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Both Hydraulic and Electrical power are required for each system to trim the aircraft
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Which statement is correct regarding the operation of the Rudder Pressure Reducer (RPR)
system above 1000' RA after takeoff? |
System "A" pressure to the rudder is reduced to 1000 PSI
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Which statement regarding the yaw damper system is correct?
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Uses "B" hydraulic system pressure and provides rudder deflection commands and turn
coordination |
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Which actions trip the YAW DAMPER switch to the OFF position?
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“B” FLT CONTROL switch placed to OFF or STBY RUD
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What is the hydraulic power source for the ground spoilers?
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A" system for both inboard and outboard ground spoilers
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Which action causes the flight spoilers to deploy at touchdown with the speed brake lever
ARMED? |
Wheel spin-up occurs on any two main wheels
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What occurs after touchdown when all spoiler panels are deployed and either throttle is
advanced? |
The SPEED BRAKE lever automatically moves to the down detent and all Ground and
Flight spoilers retract |
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All spoiler panels extend when a takeoff is rejected above 60 knots and __________.
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The reverse thrust levers are positioned to reverse thrust
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What does an illuminated green SPEED BRAKE ARMED light indicate?
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Speed brake lever is selected to ARMED with valid system inputs
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When approaching a stall angle of attack, what does the autoslat system provide?
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Automatic slat extension to the "full extend" position with trailing edge flaps at the 1
through 5 positions |
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When is the Power Transfer Unit (PTU) activated with flaps 1 through 5 selected?
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Loss of system "B" engine driven pump pressure
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How does the Power Transfer Unit provide power for the autoslat system?
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Allows system "A" pressure to power a hydraulic pump which pressurizes system "B"
fluid |
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What is the maximum altitude for flap extension?
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20,000 feet
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Which statement is correct for operation of the alternate flap system?
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No asymmetry protection is provided and LE devices cannot be retracted
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When are the LE slats in the EXTEND position?
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Trailing edge flaps are in the 1 through 5 position
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With an amber LE TRANSIT light on (normal conditions), which other light(s) will illuminate on the
forward panels? |
None
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At cruise, what does an illuminated AUTO SLAT FAIL light, MASTER CAUTION light, and FLT
CONT light indicate? (NO RECALL) |
A dual channel autoslat computer failure
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What occurs when the alternate flap position switch is held in the down position with the
ALTERNATE FLAPS master switch in the ARM position? |
Electric motor extends trailing edge flaps, and the leading edge control valve opens to
hydraulically extend the leading edge devices |
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Speedbrakes inflight __________.
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Should not be deployed at RA less than 1000' nor with flaps extended beyond 15 –
degrees |
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What is the Mach limit with both channels of the Mach Trim system failed?
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.740
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If the loss of hydraulic system “A” and the FEEL DIFF PRESS light illuminated, the elevator feel
system is still operative |
True
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With normal hydraulic system pressure indications, placing either FLT CONTROL switch to the
STBY RUD position, should cause the respective flight control LOW PRESSURE light to illuminate, then extinguish |
True
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The takeoff configuration warning horn will sound if a takeoff is attempted with the speed brake
lever in the SPEED BRAKE ARMED position |
True
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With the flaps set at "5" for takeoff, which leading edge annunciator will be illuminated on the
center instrument panel? |
LE FLAPS EXT
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With the SPEED BRAKE DO NOT ARM light illuminated before Ianding, the speed brake lever
should be manually moved to __________ after touchdown |
Up (all the way back)
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The Yaw Damper uses:
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'B' system hydraulic pressure only
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When the leading edge devices are extended with the ALTERNATE FLAPS Position Switch, the
LE slats extend to FULL EXT regardless of TE flap position |
True
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The MACH TRIM FAIL light, in conjunction with the MASTER CAUTION and the System
Annunciator FLT CONT light, illuminate if a dual channel failure of the Mach trim occurs. |
True
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What function does the flap load limiter system provide? (300/500)
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It causes the flaps to move from 40 degrees to 30 degrees in event of excessive airspeed
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With the hydraulic A system flight control switch in STBY RUD
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The Standby hydraulic pump is activated
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The trailing edge flaps are at 15 degrees. The correct indication on the aft overhead panel for the
leading edge devices is: |
Leading edge Devices (SLATS) FULL EXT lights are illuminated green
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Duty cycle for alternate flap extension to greater than 15 degrees and back to 0 degrees is:
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1 cycle - 25 minutes off
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Speed brakes should not be used with flaps greater than 15.
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True
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The elevator FEEL DIFFERENTIAL PRESSURE light is inhibited when __________.
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The flaps are extended
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A trailing edge flap asymmetry is sensed _________.
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In the trailing edge flap position indicator
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The ground spoilers are powered by the "A" hydraulic system and
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Can only be powered by the “A” hydraulic system
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The FLAP INHIBIT position of the GPWS switch
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Cancels an alert for landing with flaps less than 30 degrees
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The trailing edge flaps are normally operated by __________.
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The "B” hydraulic system
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What powers or operates the ailerons and elevators?
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Hydraulic pressure from “A” and “B” systems and the standby system
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When is the wheel to rudder interconnect system (WTRIS) used (700/800/900)
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During manual reversion flight when both “A” and “B” hydraulic systems are inoperative
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When does the B737-800 wheel to rudder interconnect system begin to operate?
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When both flight control switches are positioned to STBY RUDDER and the yaw damper
switch is repositioned to ON. |
