SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Electronic Flight Instrument System (EFIS)
4-10
Mode Transition Flashing Annunciator
Vertical Modes
ASEL arm to ASEL capture ASEL
Glideslope (GS) arm to GS
capture
GS
VPTH capture to VALT VALT
VPTH capture to VFLC VFLC
Flashing Annunciator for
Flight Director Mode Transitions
Table 4- -2
D Flight Director Couple Arrow -- The direction that the couple arrow
is pointing indicates the EHSI and DADC that are coupled to the
flight guidance computers. The arrow points in the same direction
as the CPL arrow on the flight guidance controller. The arrow on the
EADI is green if the flight director source is from same side and
amber if the flight director source is from cross--side flight guidance
computer . To select the cross--side flight director information after
the loss of the on--side flight director, push the FD REV (reversion)
button.
D Roll Attitude Pointer And Scale -- The roll pointer displays actual
roll attitude. The roll scale has fixed index reference marks at 0_ ,
10_,20_ ,30_,45_, and 60_.
D Autopilot Engage Annunciator -- Autopilot engage annunciators
arelistedinTable4--3.
Condition
Annunciator
Autopilot (AP) engage AP
Autopilot disengage AP (flashing)
Flight guidance computer
transfer (autopilot remains
engaged)
AP flashing for 5 seconds,
then steady
TCS button pushed TCS replaces AP while the
TCS button is pushed
Autopilot Engage Annunciators
Table 4- -3
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