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Abnormal Conditions
In the event of a DCP failure, a red boxed DCP shows on the affected PFD. To allow
selection of the operating DCP, a reversionary selector switch is provided on the
reversionary panel. This switch has three positions, NORM, 1, or 2. In the NORM
position, each DCP controls its own MFD. In either the 1 or the 2 position, the
remaining DCP controls the display on both MFDs.
FLIGHT INSTRUMENTS
For Training Purposes Only
May 03
11-53
P I LOT T R A I N I N G GU I D E
Display Reversionary Panel
Figure 11-33
VFE (45 FLAPS)
VFE (30 FLAPS)
VFE (20 FLAPS)
VA (MANEUVERING)
(AT SEA LEVEL 48,200LB)
(AT 20,000FT 26,000LB)
VNO (BELOW 8,000FT)
VNO (8,000 TO 22,150 FT)
AIRSPEED LIMITS - (INDICATED SPEEDS)
MMO (22,150FT TO 26,570FT)
VMO (26,570FT TO 30,990FT)
MMO (30,990FT TO 41,000FT)
VLO (EXT) (L/G EXTENSION)
VLO (RET) (L/G RETRACTION)
VLE (L/G EXTENDED)
189
197
231
248
187
300
348
0.78
318
0.85
197
197
250
PULL
PULLTOCAGE
CAGE
CLI MB
DI VE
OFF
BRT
BRT
BRT
0.0
0.0
0.0
0.0
180 180
N1
ITT
N2
STAB
- TRIM -
NU
ND
5.0
RUDDER
AIL
LWD RWD
NL NR
FF (PPH)
OIL PRESS
OIL TEMP
FAN VIB
0 4050
8100
0.0
33
0
0
0
- FUEL (LBS) - TOTAL
0
0
33
0.0
4050
DN DN DN
- GEAR - - FLAPS - 20
R ENG OIL PRESS
L ENG OIL PRESS
L WSHLD HEAT
L WINDOW HEAT
INBD BRAKE PRESS
R WSHLD HEAT
R WINDOW HEAT
OUTBD BRAKE PRESS
R PROBE HEAT OFF
L PROBE HEAT OFF
HYD 3 LO PRESS
BRT
CABIN TEMP
BLEED PRESS
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
47
23
0
36 35
1820
100
0
0.0
APU
100 323
RPM EGT
R FUEL PUMP ON
L FUEL PUMP ON
DOOR CLOSED
PARKING BRAKE ON
PROX SYS FAULT
FDR FAIL
SPOILERS
15
2 000
2
3
4
ALT
0
7 3
2
1
4
9
6 2992
5
1014
400
350
300 250
200
150
100
60
KTS
IAS
FEET
X 1000
CABIN
ALTITUDE
0
4
2
6
8
10
20
30
45
BRT
BRT
80
60
20
00
20
10
10
20
300
200
100
100
000
8000
4
RA2
IRS2
ADC2
DCP2
TERM
VOR1
TRU
NO FLIGHT PLAN
TCAS
OFF
29.92 IN
2400M
GS
RA
TO
LOC 1
DR TO
ALTS
FMS1
12
DTK 333
.7
YUL
NM
4
4
2
2
1
1
2500M
200
N
33
15
12
E
6
3
0
3000
40
VT 150
V2 133
VR 121
V1 113
ADF2
0FT
2
1
VFE (45 FLAPS)
VFE (30 FLAPS)
VFE (20 FLAPS)
VA (MANEUVERING)
(AT SEA LEVEL 48,200LB)
(AT 20,000FT 26,000LB)
VNO (BELOW 8,000FT)
VNO (8,000 TO 22,150 FT)
AIRSPEED LIMITS - (INDICATED SPEEDS)
MMO (22,150FT TO 26,570FT)
VMO (26,570FT TO 30,990FT)
MMO (30,990FT TO 41,000FT)
VLO (EXT) (L/G EXTENSION)
VLO (RET) (L/G RETRACTION)
VLE (L/G EXTENDED)
189
197
231
248
187
300
348
0.78
318
0.85
197
197
250
80
60
20
00
20
10
10
20
300
200
100
100
000
8000
4
RA2
IRS2
ADC2
DCP2
VOR1
TRU
TCAS
OFF
29.92 IN
2400M
GS
RA
TO
LOC 1
DR TO
ALTS
4
4
2
2
1
1
2500M
200
0
3000
40
VT 150
V2 133
VR 121
V1 113
ADF2
0FT
2
1
FMS2
12
DTK 056
.2
LONNA
NM
TERM
N
33
15
12
E
6
3
CABIN TEMP
BLEED PRESS
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
47
23
0
36 35
1820
100
0
0.0
APU
100 323
RPM EGT
R FUEL PUMP ON
　
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本文鏈接地址：龐巴迪挑戰者604機組操作手冊 CL_604-FLIGHT_INSTRUMENTS(23)