King Air C90GTi, Pilot Training Manual

Page: 374 / 557

Figure 16-77. Control Display Unit (CDU)
EXEC
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MFD
D A T A
MFD
A D V
CLR
DEL
B R T
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
/
ACT FPLN
KICT
ORIGIN
1/4
DIST DEST
ROUTE ALTN
ORIG RWY
VIA TO
<COPY ACTIVE
<SEC FPLN
[
[
PERF INIT>
KDEN 452
KAPA PLANT2
ICT DIRECT
-------------------
KING AIR C90GTi/C90GTx PILOT TRAINING MANUAL
It is necessary to reselect a desired mode after
the aircraft is configured in the go-around to
regain full flight director control.
See the Flight Guidance Mode Annunciations
table at the end of this chapter.
Figure 16-76. PFD Go-Around (GA) Mode
CONTROL DISPLAY UNIT
(CDU)
The Control Display Unit (CDU-3000) serves
as a control of the communication and navi-
gation radios, Flight Management System
(FMS) and limited display control for the
PFDs and MFD (Figure 16-77). The pedestal
can contain either one or two CDUs. The sec-
ond CDU is an option. If two are installed,
each CDU will communicate only with the re-
spective FMS. In the optional two CDU in-
stallation, reversionary mode is not available
should one fail. The remaining CDU will be
capable of communicating with the on-side
FMS only.
The CDU has a normal operating temperature
range of –20˚C to +70˚C. Should the unit tem-
Collins
10
10
20
GA GA
14
000
6
60
540
20
400
600
700
1
2
4
4
2
1
30.16IN
251
W
24
<
140
80
60
6935
TERM
ACC -.02
T
0
V
2
V
R
V
1
110
93
93
FOR TRAINING PURPOSES ONLY
16-41
16
A
VIONICS