King Air C90GTi, Руководство по подготовке пилотов

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PFD provides secondary intensity control of
the PFD. The PILOT DISPLAYS rheostat, lo-
cated on the overhead panel, will control
three displays simultaneously; the PFD, MFD,
and Control Display Unit (CDU) on the
pedestal. This allows all three displays to be
brightened together. The BRT/DIM Rocker
Switch will then allow each display to be fine
tuned to make its brightness even with the
surrounding displays.
Line Select Keys
Four line select keys (LSK) are located on
each side of the AFD. These keys are used in
conjunction with the information being
viewed on the AFD display. LSKs that are cur-
rently active are denoted by carets (< >) dis-
played adjacent to the LSK.
Attitude Display
The primary function of the PFD is to show
airplane attitude. The attitude display on the
PFD, additionally shows the following: flight
director steering commands; flight guidance
system status/mode annunciations; vertical/lat-
eral deviation; marker beacon annunciations;
and radio altitude.
A rectangular-shaped slip/skid indicator is lo-
cated at the base of the “sky-pointer” bank
Figure 16-2. Primary Flight Display
Collins
BRT
DIM
10
10
20
HDG PTCH
ALTS
14
000
6
60
540
20
400
600
700
1
2
4
4
2
1
30.16IN
<
PRESET
VOR1
FORMAT >
FMS1
DTK 251
(6935)
0.
8NM
25
251
W
30
24
21
ATC1 UTC RAT COM1 COM2
121.800 4336 125.250 14:41
15 o C
<
140
80
60
6935
RDR
TERR
<
ET
01:42
TERM
F
50
ACC -.02
TERRAIN
0
FMS
RADAR ON
144
069
TCAS OFF
TFC >
>
110
93
93
V
2
V
R
V
1
16-3
FOR TRAINING PURPOSES ONLY
KING AIR C90GTi/C90GTx PILOT TRAINING MANUAL
16
A
VIONICS