BLOCK 8

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Author:
carLORENZ0
ID:
253220
Filename:
BLOCK 8
Updated:
2013-12-15 02:49:22
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Description:
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  1. + is used to make minor adjustments to the aircraft about its VERTICAL axis (YAW).
    Rubber Trim Tab Control System
  2. located on the trailing edge of the ruder.
    Rudder Trim Tab
  3. To yaw right (NOSE RIGHT)
    the rudder trim tab is moved to the LEFT.
  4. To yaw left (NOSE LEFT),
    the rudder trim tab is moved to the RIGHT.
  5. located on the Trim Control Panel,3 position toggle switch is used to operate the rudder trim tab.
    Rudder Tab Control Switch
  6. this component actually moves the rubber trim tab.
    Rudder Trim Tab Actuator
  7. this component displays the rudder trim tab position (in degrees) for the pilot and co-pilot. 

    - receives a signal from the Position Indicator Transmitter within the Rudder Trim Tab Actuator assembly.
    Rudder Trim Tab Position Indicator
  8. + is used to make minor adjustments to the aircraft about its LONGITUDINAL AXIS (roll).
    AILERON TRIM TAB SYSTEM:
  9. located on the trailing edge of both left and right ailerons.
    Aileron Trim Tabs -
  10. - is fixed and can only be adjusted manually.
    Right Aileron Trim Tab
  11. is used in flight & it is controlled electrically.
    Left Aileron Trim Tab -
  12. ~ located on the Trim Control Panel, this multi use, recessed toggle switch is used to operate the left aileron trim tab.
    Trim Tab Control Switch:
  13. these relays control voltage to the Aileron Trim Tab Actuator.
    Aileron Trim Control Relays (K56E, K56F) -
  14. this component actually moves the left aileron trim tab.

    - driven by a reversible AC motor & contains a magnetic brake, limit switches & a Position Indicator Transmitter.
    Aileron Trim Tab Actuator -
  15. this component displays the roll condition (in degrees) for the pilot & co-pilot.

    - receives a signal from the Position Indicator Transmitter within the Aileron Trim Tab Actuator assembly.
    Aileron Trim Tav Position Indicator -
  16. + is used to make minor adjustments to the aircraft about its LATERAL axis (pitch).
    ELEVATOR TRIM TAB SYSTEM
  17. located on the trailing edge of both the left and right elevators.
    Elevator Trim Tabs -
  18. located on the Power Control Quadrant, this detented switch is used to select modes of operation for the elevator trim tab system.
    Elevator Tab Trim Switch -
  19. located on the outboard side of each control wheel, these switches control the elevator trim tab system when operating in Normal mode.
    Pilots/ Co-pilots Control Wheel Elevator Tab Switch
  20. ~ located on the Trim Control Panel, this multi use, recessed toggle switch is used to operate the elevator trim tabs in EMERGENCY MODE. (which also operates the left aileron trim tab [vise-versa])
    Trim Tab Control Switch -
  21. this relay is energized whenever the autopilot system is engaged.

    + Overrides Normal Mode of operation - allowing the autopilot system to control the elevator trim tabs.
    Manual Elevator Tab Control Disengage Relay (K30C)
  22. These relays are used ONLY in Normal Mode of operation when autopilot is on.
    Autopilot Trim Tabs Isolation Relays (K50D, K50E)
  23. - These relays control voltage to the Elevator Trim Tab Actuator.
    Elevator Trim Control Relays (K90A, K90B, K90C, & K90D)
  24. this component actually moves the elevator trim tabs. 

    + driven by a reversible AC motor in NORMAL MODE & during AUTOPILOT operation.
    Elevator Trim Tab Actuator -

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