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FlightSafety LEARJET 45 - Page 389

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600s collect information from the data acqui-
sition units (DAUs) for the Engine Instrument
and Crew Alerting System (EICAS) and the dis-
play of systems information.
The flight guidance function of the IC-600
provides digital processing of heading, navi-
gation, and air data information to the elec-
tronic flight instrument system (EFIS). The
IC-600 computes flight director command bar
steering in response to pilot selections on the
flight guidance controller for flight director
and autopilot operation. When the autopilot is
engaged and coupled to the flight director
commands, the No.2 IC-600 controls the air-
plane using the same commands that are dis-
played on the selected flight director. The
autopilot is not aware of which flight direc-
tor mode(s), if any, are active. The autopilot
simply tracks the pitch and roll steering com-
mand as attitude change.
LEARJET 45 PILOT TRAINING MANUAL
16-4
FOR TRAINING PURPOSES ONLY
FlightSafety
international
N1
ITT
SAT °C
END
CAS
FUEL
FLT
ECS
HYD
ELEC
SUMRY
LF
1000
R
1750
FLAPS
20
6.5
PITCH TRIMLBSFUEL
4450
-15
50.0
76
60
984
50.0
80
60
1002
N2
OIL PSI
OIL °C
FF PPH
550
550
75.0
75.0
1700
ELECT
VOLTS
EMER-V
AMPS
TEMP °C
28.5 28.0
28.0
50 65
30
50
HYD/ECS
MAIN
B-ACUM
CAB ALT
OXY QTY
3000
3000
1300
669
FLT
SPLR
PIT
AIL
RUD
0
6.5
R 1
L 1
DU 1 DU 2 DU 3 DU 4
RMU 1 RMU 2
3
3
3
0
W
N
3
6
E
1
2
1
5
S
2
1
24
3
2
1
0
1
2
3
1000
20
20
10
10
10
10
150
4500
29.92 IN
50
00
160
180
14
1
0
9
120
100
160
.400 M
GS
LOC
HDG
AP YD
SPD
GS
180 RA
HDG
001
359 CRS
ILS1
13.1 NM
25
TGT
VOR1
ADF2
RA/BARO
STD
BARO
MINIMUMS
43
80
20
00
Honeywell Honeywell
Honeywell Honeywell
3
3
3
0
W
N
3
6
E
1
2
1
5
S
2
1
24
3
2
1
0
1
2
3
1000
20
20
10
10
10
10
150
4500
29.92 IN
50
00
160
180
14
1
0
9
120
100
160
.400 M
GS
LOC
HDG
AP YD
SPD
GS
180 RA
HDG
001
359 CRS
ILS1
13.1 NM
25
TGT
VOR1
ADF2
RA/BARO
STD
BARO
MINIMUMS
43
80
20
00
Honeywell
Honeywell
SYS MFD
MENU
WX
CKLST PLAN
MAP
TCAS
Honeywell
Honeywell
STAB
TGT
WX
-4°
315°
47.0
30
33
N
3
6
5050
360
KDVT
LL01
PBD01
PLAB1
PLAB2
#TOC
FL300
25
FMS1
KDVT
12.5 NM
12 MIN
CHK EICAS
300 TAS
+15 SAT
245 GSPD
00
-05
+20
-10
-12
TCAS TEST
ABV
FL
RA NO BRG
TA NO BRG
6
123.20
162.5
500
300
25.5
- - -
Honeywell
TUNE
SQ
DIM 1/2
STO
DME
TST
PGEID
Honeywell
TUNE
SQ
DIM 1/2
STO
DME
TST
PGEID
COM 1
NAV 1
ATC/TCAS
ADF 1
TCAS DSPY
123.20
COM 1
123.20
131.27
MEMORY-3
1471
1 ATC ON
RANGE: 40
BELOW
110.25
109.35
MEMORY-1
162.5
ANT
NARROWSQ
MEMORIES
BANDWIDTH
SELECT
1
136.92
2 122.20
3 131.27
4 125.07
5 121.02
6 118.17
MORE INSERT
RETURN DELETE
NB
Figure 16-2. Primary Display Units

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