Garmin Flight Deck 100 ユーザーズマニュアル

190-00728-04  Rev. A

®

449

The following AFCS controls are located separately from the AFCS Control Unit:

Disengages the autopilot and yaw damper, and interrupts pitch trim operation

An AP DISC Switch is located on each control wheel.

This switch may be used to acknowledge an autopilot disconnect alert and mute 

the associated aural alert.

While pressed, allows manual control of the aircraft while the autopilot is engaged and

synchronizes the flight director’s Command Bars with the current aircraft pitch (if not
in Glideslope or Glidepath Mode) and roll (if in Roll Hold Mode)

A CWS Button is located on each control wheel.

Upon release of the CWS Button, the flight director may establish new pitch and 

roll references, depending on the current vertical and lateral modes. CWS operation
details are discussed in the respective mode sections of this manual.

Disengages  the  autopilot,  if  engaged,  and  selects  flight  director  Takeoff  Mode  (on

ground) or Go Around Mode (in air)

The TO/GA Switch is located on the throttle handle.

This switch also activates the missed approach when the selected navigation source 

is GPS or when the navigation source is VOR/LOC and a valid frequency has been
tuned.

Used to command manual electric pitch trim

An MEPT Switch is located on each control wheel.

The pilot side MEPT Switch has priority over the copilot side MEPT Switch.

This composite switch is split into left and right sides. The left switch is the ARM

contact and the right switch controls the DN (forward) and UP (rearward) contacts.
Manual trim commands are generated only when both sides of the switch are operated
simultaneously. Pushing either MEPT Switch disengages the autopilot, if engaged, 
but does not affect yaw damper operation.