Honeywell SPZ-8000 Pilot's Manual page 54

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