King Air C90GTi, Pilot Training Manual

Page: 379 / 557

Figure 16-84. MFD Text Page
The CDU is the primary interface with the
FMS. Each CDU will communicate with the
“on-side” FMS (e.g., Left CDU for No. 1 FMS,
Right CDU for No. 2 FMS). The FMS’s can be
synchronized so that selected operations on
one CDU (and its related FMS) will automat-
ically be transferred to the cross-side CDU
(and its related FMS). (See FMS quick refer-
ence guides and other handouts for informa-
tion on how to synchronize the units.)
The FMS database is updated using the
Database Unit (DBU). The DBU 5000 con-
sists of two USB ports on top of the pedestal.
These are used to upload data to the aircraft
or download data from the aircraft. This can
include avionics malfunction reports (Figure
16-85).
The aircraft battery and avionics need to be
ON. It is strongly recommended that a ground
power unit be applied to the aircraft for this
operation.
Collins
BRT
DIM
FORMAT
TAS SAT GS ISA
0 0
+13 o C 15 o C
<
<
0
0.0
ITT
26
TORQ
0
FF
PRESS
OIL
TEMP o C
0
0
46
430
120
73
N I
98.5
PROP
1980
TORQ
2000
ITT
734
WPT DIST ETA FUEL (LB)
KICT 3.6NM 20:07 0
ICT 7.4NM 20:11 2450
MUGER 16.6NM 20:15 2390
WUKOL 19.8NM 20:16 2370
WUKUS 20.4NM 20:16 2370
HUT 29.8NM 20:20 2310
OATHE 218NM 21:32 1170
SELLS 283NM 21:56 760
TFC
<
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
FMS ACT PROGRESS 1/3
DEST
KDEN 415NM 22:47 0
ALTN
KAPA 435NM 22:54 0
RESERVE 0
EXTRA 0
16-46
FOR TRAINING PURPOSES ONLY
KING AIR C90GTi/C90GTx PILOT TRAINING MANUAL
16
A
VIONICS
Figure 16-83. MFD Advance Key (CDU)
EXEC
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<PREV WPT
[
[
<NEXT WPT
<TO WPT
ACT PLAN MAP CENTER
CTR WPT
<-----
SIDE
L /R>
EXEC
NEXT PREV
MFD
DATA
MFD
ADV
CLR
DEL
BRT
DIM
DEP
ARR
PERF LEGS FPLN DIR
MSG
TUN
IDX
MFD
MENU
A B C D F G
H I J K L M
O P Q R T U
V X Y Z
SP
/
E
N
S
W
1 2 3
4 5 6
7 8 9
+ -
/
0
/
LEFT DISPLAY ADVANCE
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[
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