BendixKing SG 465 System EFS 40/50 - Manual (Page 141)

EADI Displays
4.2.6 Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Software release 06 added the
following autopilot failure warning
annunciations. They are listed in
order of priority and will be dis-
played in the SR field:
• PTRM RED = pitch
auto/manual trim fail
• LTRM RED = lateral autotrim
fail
• PTCH RED = elevator servo
failure
• ROLL RED = aileron servo
failure
• YAW RED = rudder servo
failure
• PITCH YELLOW = elevator
mistrim
• ROLL YELLOW = aileron
mistrim
• YAW YELLOW = rudder
m i s t r i m
Two additional failure annuncia-
tions were added by software
release 09 to accomodate the
KFC 500.
• RTRM RED = roll auto trim fail
• YTRM RED = yaw autotrim fail
The KFC 500 will use these two
annunciations instead of “LTRM”.
If the flight director data becomes
invalid, a RED “FD” enclosed in a
RED box will be displayed at the
right center of the display.
If the autopilot has been on and
then disengaged, a RED “AP” will
be annunciated in the upper left
hand corner. Depending on the
autopilot type, the RED “AP” may
flash when disengaged.
In dual autopilot installations, the
active side is annunciated by a
green “AP” and the inactive side
will be annunciated by a yellow
“AP” with a yellow arrow pointing
toward the active side.
Beginning with software release
09, the KFC 500 autopilot cou-
pled status “SAS” may be dis-
played in place of “AP”. As with
the “AP” annunciation, “SAS” will
be either green or yellow to indi-
cate active and inactive sides
respectively and flashing red
when disconnected. A steady red
SAS annunciation indicates an
autopilot power loss. See the
KFC 500 pilots guide for more
i n f o r m a t i o n .
Yaw damper, if engaged, may
flash RED when disconnected
depending on the autopilot type.
Beginning with software version
05, the following autopilot com-
mand reference data will be dis-
played in green when interfaced
with the KFC 4 0 0 / 5 0 0 :
• AIRSPEED
0 to 512KTS in 1KT
i n c r e m e n t s .
• MACH
0 to 4.096M in
0.005M increments.
• VERTICAL SPEED
+/-20,480F/M in
100F/M increments.
• ALTITUDE
0 to 65536FT in 10FT
i n c r e m e n t s .
• HIGH PROFILE
“ H ”
• NORMAL PROFILE
“ N ”
• LOW PROFILE
“ L ”
N o t e : Lateral/vertical modes
and other annunciators are
determined by the auto-
pilot/flight director sys tem
installed.
Section 4.2mp 10/13/10 2:54 AM Page 4.2.6