Lower Display Information
At the bottom of each PFD is a row of infor-
mation that continuously display these items:
COMM1, ATC squawk, UTC, RAT (ram air
temperature) and COMM2 (Figure 16-21).
Pressing the push-to-talk button on the yoke or
microphone will highlight the appropriate
COMM frequency label with a blue box. The
ATC selection will show which transponder is
chosen and whether that transponder is on
STBY or active. It does not display the differ-
ence between ON and ALT. The RAT is de-
rived from the currently selected air data
computer.
Figure 16-21. PFD Lower Display
Information
MULTIFUNCTION DISPLAY
(MFD)
The MFD displays engine indications, diag-
nostic pages, weather radar, two formats of
navigation information, and terrain informa-
tion. A typical MFD display is shown in Fig-
ure 16-22.
The MFD has the following controls and indi-
cations:
BRT/DIM Rocker Switch
The BRT/DIM Rocker Switch provides sec-
ondary intensity control of the MFD. The
PILOT DISPLAYS rheostat, on the overhead
panel, provides primary intensity control. This
PILOT DISPLAYS rheostat will control all
three displays: the PFD; MFD; and Control
Display Unit (CDU) on the pedestal, simulta-
neously. Each display does not have to be in-
dividually dimmed or brightened but can be
operated together. The BRT/DIM Rocker
Switch will then allow each individual display
to be fine tuned to make its brightness com-
patible with the surrounding displays.
Line Select Keys
Four line select keys (LSK) are located on
each side of the MFD. The keys are used in co-
ordination with the information being viewed
on the individual MFD display. LSKs that are
currently active are denoted by carets (< >)
displayed adjacent to the LSK.
Engine Display
The engine instrument display is shown at the
top of the MFD. This is called the Engine In-
dicating System (EIS). The EIS is always visi-
ble with aircraft power on. Refer to Chapter 7,
Powerplant, of this
Pilot Training Manual
for
more information.
BRT
DIM
ATC1
UTC
RAT
COM1
COM2
121.800
4336
125.250
14:41
15
o
C
<
1
<
ET
01:42
RADAR ON
16-11
FOR TRAINING PURPOSES ONLY
KING AIR C90GTi/C90GTx
PILOT TRAINING MANUAL
16
A
VIONICS
Figure 16-22. Pilot's MFD Display
Collins
BRT
DIM
FMS
DTK 251
( 6 9 3 5)
TTG
0.
8NM
251
W
30
24
21
TAS
SAT
GS
ISA
0
0
+13
o
C
15
o
C
<
RDR <
TERR
F
50
WX
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
AFX
RW25
( 6 9 3 5)
SXW152
KBJC
0 . 0NM
0 . 8NM
4 . 4NM
198NM
- : - -
- : - -
- : - -
CL I MB
( 6 9 3 5) 6 9 3 5 A
- : - - / 0 . 8NM
:
:
:
:
25
T+5.7
SXW152
( 6 9 3 5)
/ 6 9 3 5 A
KEGE
RLG
/ 1 4 0 0 0 A
-- : --
FIRE
TFC <
ABOVE
<
Summary of Contents for C90GTi
Page 5: ......
Page 7: ......
Page 9: ......
Page 11: ......
Page 13: ......
Page 45: ......
Page 47: ......
Page 49: ......
Page 87: ......
Page 89: ......
Page 97: ......
Page 99: ......
Page 101: ......
Page 113: ......
Page 115: ......
Page 117: ......
Page 139: ......
Page 141: ......
Page 193: ......
Page 195: ......
Page 203: ......
Page 205: ......
Page 207: ......
Page 215: ......
Page 217: ......
Page 219: ......
Page 241: ......
Page 243: ......
Page 259: ......
Page 261: ......
Page 263: ......
Page 277: ......
Page 279: ......
Page 281: ......
Page 283: ......
Page 285: ......
Page 311: ......
Page 313: ......
Page 315: ......
Page 323: ......
Page 333: ......
Page 437: ......
Page 439: ......
Page 441: ......
Page 443: ......
Page 467: ......
Page 471: ......
Page 483: ......
Page 485: ......
Page 487: ......
Page 491: ......
Page 493: ......
Page 495: ......
Page 515: ......
Page 517: ......
Page 519: ......
Page 521: ......
Page 547: ......
Page 555: ......
Page 557: ......