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Clock Prior to A/C 5331 .................................................................................................. 11-31
Clock A/C 5331 and Later............................................................................................... 11-32
Display Reversionary Panel............................................................................................ 11-33
11-iv For Training Purposes Only
May 03
FLIGHT INSTRUMENTS P I LOT T R A I N I N G GU I D E
Page Intentionally Left Blank
FLIGHT INSTRUMENTS
For Training Purposes Only
May 03
11-1
P I LOT T R A I N I N G GU I D E
CHAPTER 11: FLIGHT INSTRUMENTS Introduction
The flight instruments chapter includes the Electronic Flight Instruments System
(EFIS), Air Data System (ADS), standby instruments, clock and radio altimeter.
Electronic Flight Instrument System (EFIS)
The Electronic Flight Instrument System (EFIS) takes input data from airplane radios,
sensors and control panels and displays the information on four Electronic Flight
Displays (EFDs).
Two of the EFDs function as primary flight displays (PFD), and two EFDs function as
multifunction displays (MFDs).
The color conventions used for the PFD and MFD symbology are:
Electronic Flight Displays
Figure 11-1
White For all scales and on-side FMS sensor data
Green For on-side sensor data (non-FMS)
Yellow For cross-side sensor data and caution information
Magenta For pilot-selectable data
Cyan For secondary information
Red For warnings and failure flags
P604_11_047
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
TOCAGE
CAGE
CLI MB
DI VE
OFF
BRT
059
WX + TRB
UTC 11:01 TAS 0 GS0 TAT15 C
VOR 1 ADF 2
VOR1
YUL
TTG--:--
CRS 012
12.7NM
SAT 15 C
FMS2
LONNA
DTK056
12.2 NM
TTG --:--
33
30
21
S
15
12
6
3
N
E
W
24
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
CYUL
TOC
ALEXS
3
059
N
E
12
25
WX+TRB
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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