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4
N
33
30
W
24
21
S
15
12
E
6
3
0
1
2
3
1
2
3
ATT
HDGT
EICAS
G
S
LOC
HDG
RAD
IAS
ALT
HDG2
VOR 1
ADF 2
10000
20
80
THRUST HDG AP1 ASEL ATT 2
VAPP VNAV ADC 3
9500
29.92
AT1
VTA
M
0.450M
FMS1
DTK LOC1
360
HDG
330
10400
20
20
10
10
20
20
10
10
9500
10500
300
220
210
200
190
180
170
F3
LE
F1
2
160
150
185
6
4
N
33
30
W
24
21
S
15
12
E
6
3
0
1
2
3
1
2
3
ATT
HDGT
EICAS
G
S
LOC
HDG
RAD
IAS
ALT
HDG2
VOR 1
ADF 2
10000
20
80
THRUST HDG AP1 ASEL ATT 2
VAPP VNAV ADC 3
WX
ET
NO BEARING
RA 9 . 8NM +13
TA 4 . 5NM -04
SAT
GSPD
TERR
-56
TAT
TAS
-40
234
345
INHIB
LX
00 : 10 0 . 05L
HDG MAG2
315
ETE 1+36
12 . 5
KDVT
NM
FL
BELOW
TCAS TEST
360 FMS1
N
5 5
3
6
33
30
- 02
- 02
+ 12
- 04
KABC
KKLM
KKLM
TOC
TOC
KGHJ
KGHJ
LUF
KDEF
KDEF
4000 4000
FL180
+ 09
SG 1-2 FAIL
SG 1 SG 3 SG 2
ALTN ALTN ALTN
NORM NORM NORM
Honeywell Honeywell Honeywell Honeywell
1300
0.00
0
0
90
13 13
20
19 20
22 22
20
OXYGEN
AFT
CABIN (°C)
FWD
CABIN (°C)
CKPT (°C)
OPEN OPEN
OUTFLOW VALVES
CAB ALT
P
CAB RATE
LDG ELEV
0 0
1 2
1 2
1 2
QTY
ENG
APU
RES
OIL (QTS)
APU DOOR 11.2°
RPM EGT
BRAKE TEMP
11.5
100 650
03 06 03 03
11.5
5.2
6.0
%
% %
Honeywell
TOTAL FUEL (LBS) 4155O
1.54
146OO 1OOOO 146OO
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
575O
115
81
1.65
CRZ
EPR
I
G
N
START START
I
G
N
ND
STAB
1.54
1.65
73.3
T/O
N1
SYNC
73.3
789
ITT
SYNC
789 DN DN DN
OUT
3O
GEAR
–TRIMS–
NL RUDDER NR
AIL
LWD RWD
7.2
NU
93.4
575O
115
81
235O
NO TAKEOFF
PARK/EMER BRAKE ON
END
TOTAL FUEL (LBS) 4155O
1.54
146OO 1OOOO 146OO
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
575O
115
81
1.65
CRZ
EPR
I
G
N
START START
I
G
N
ND
STAB
1.54
1.65
73.3
T/O
N1
SYNC
73.3
789
ITT
SYNC
789 DN DN DN
OUT
3O
GEAR
–TRIMS–
NL RUDDER NR
AIL
LWD RWD
7.2
NU
93.4
575O
115
81
235O
NO TAKEOFF
PARK/EMER BRAKE ON
END
7-36 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
ADC REVERSION
IRS ADC ADC IRS
SG 3
EICAS
SG 1 SG 2
PFD 1
ALTN 3
ALTN
ALTN 1
ALTN ALTN
ALTN
NORM
NORM
NORM NORM
NORM
PFD 1 PFD 2
PFD 2
ALTN 2 ALTN
NORM
GX_07_040
PILOT’S
SELECTED
ADC
COPILOT’S
SELECTED
ADC
PFD1 SOURCE
ANNUNCIATION
PFD2 SOURCE
ANNUNCIATION
ADC1 ADC1 ADC1 ADC1
ADC1 ADC2
ADC2 ADC1 ADC2 ADC1
ADC2 ADC2 ADC2 ADC2
ADC1 ADC3 ADC3
ADC2 ADC3 ADC2 ADC3
ADC3 ADC3 ADC3 ADC3
ADC3 ADC1 ADC3 ADC1
ADC3 ADC2 ADC3
ADC Switches
Used to select
reversion on
appropriate ADC.
PFD ANNUNCIATION
Pilot’s Side
Normally fed as follows:
•ADC 1 – if reverted then
• ADC 3 if reverted then
• ADC 2
–
Copilot’s Side
Normally fed as follows:
• ADC 2 if reverted then
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庞巴迪挑战者手册5(66)
