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52 Cards in this Set
- Front
- Back
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where are the ailerons located
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trailing edge of each wing tip
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what does one aileron do when the other goes up
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goes down
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what hydraulic system does the ailerons use
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none
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what forces the ailerons to move
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aerodynamics and control tabs. the control yoke operates the control tab via cable on each aileron.
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how are the control yokes linked
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by torque tubes
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where are the aileron control tabs located
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inboard portion of the ailerons
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where are the aileron trim tabs located
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outboard portion of the ailerons
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where are the spoiler located
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top aft portion of each wing
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what are the functions of the spoilers
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1 spoil lift upon touchdown.
2 shorten landing roll of A/C by creating drag 3 assist while banking 4 assist ailerons 5 speed brakes in flight |
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how are the spoiler and ailerons linked
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mechanical aileron spoiler mixer assembly
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when the aileron control wheel is moved to ______ degrees , the cam follower starts to extend the flight spoilers on the downward moving wing
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5
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where is the mechanical aileron spoiler mixer assembly located
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port and stbd wheel well
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where is the spoiler handle located
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center pedestal
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inboard spoiler actuator is supplied by what hydraulic system
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left
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outboard spoiler actuator is supplied by what hydraulic system
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right
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what hydraulic system powers the rudder
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right
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how does the q-limiter restrict the rudder
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airspeed
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at _1_ and _1_ flap settings, the flap-controlled rudder stop is held in the engaged position by dual mechanical springs. it is withdrawn by a hydraulic actuator at _2_, _2_, and _2_ flap setting. the actuator is controlled by a valve ___3___ connected to the ___4___ and ___4___
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1. 0 degrees and 5 degrees
2. 15, 25 and 50 degrees 3. mechanically 4. flap follow-up and control valve mechanism |
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the Q-limiter allows the rudder to operate unrestricted(+/-22 degrees) up to ____ knots
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177
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from ___ to ____ knots the rudder is restricted to +/-17 degrees
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177 and 195
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the rudder is modulated from +/-17 degrees to +/-2 1/2 degrees from ___ to ___ knots
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195 and 304
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rudder stop assembly is also know as __________
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auxiliary rudder throw limiter
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how is the rudder stop assembly retracted and extended
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hydraulically retracted and mechanically extended
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rudder stop mechanically limits rudder throw to 17 degrees when flaps are in the __ and __detents
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0 degrees and 5 degrees
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full rudder travel is available when flaps are extended to ___ and beyond
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15 degrees
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flap/rudder stop inop light on annunciator panel illuminates when
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flap position and rudder stop position do not agree
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the control yoke in the cockpit operates the ________ on each elevator
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control tab
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control tabs are installed on the ______ side of each elevator
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inboard
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how many hydraulic powered boost cylinders are installed on each elevator
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1
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what is the purpose of the hydraulic powered boost cylinders
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force the elevators down in the event of a aircraft stall
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geared tabs are installed on the ______ side of each elevator
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outboard
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the elevator hydraulic powered boost cylinders operate from what hydraulic system
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only left
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the elevator hydraulic powered boost cylinder system will nose down assist if the elevator control tab is displaced approximately ___degrees. normally, the maximum elevator nose down tab used is ___ degrees
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10, 8
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there are two electrically driven motors that drive a _________ that will raise or lower the horizontal stabilizer
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jackscrew
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the larger trim motor on the horizontal stabilizer is called the _______
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primary motor
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the smaller trim motor on the horizontal stabilizer is called the _______
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alternate motor
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the primary trim motor on the horizontal stabilizer can be operated from what 3 places
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thumb switch on pilot/co-pilot yoke or suit case handle
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the alternate trim motor on the horizontal stabilizer can be operated from_________
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the alternate trim motor knobs under the throttles
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auto pilot operates what trim motor
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alternate trim motor
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the primary and alternate electric motors incorporate a ____1____ switch. if an overload condition of the electric motor should cause overheating, the ____1____ will open and electrical power to the motor will be temporarily disrupted. when over heated conditions dissipate (approx. _2_ seconds), the ___1___ switch will automatically reset and the electrical power will be restored
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1. thermal trim cutout
2. 20 |
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the stabilizer position indicator is _________ connected to the horizontal stabilizer
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mechanically
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the flap inboard cylinders receive pressure from what hydraulic system
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right hydraulic system
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where is the flap position indicator
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secondary engine display
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how are the flaps actuated
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hydraulically from both left and right systems
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the flap outboard cylinders receive pressure from what hydraulic system
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left hydraulic system
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what are the 6 flap settings
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0, 5, 15, 25, 40 & 50 degrees
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what does the flap followup cable system operate
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takeoff warning switch and landing gear warning switch
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what hydraulic system actuates the slats
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both
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where is the position gage for the slats
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there is none, there is a blue slat extended light located near the landing gear handle
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what does the flap followup cable system operate
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takeoff warning switch and landing gear warning switch
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what hydraulic system actuates the slats
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both
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where is the position gage for the slats
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there is none, there is a blue slat extended light located near the landing gear handle
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