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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
Honeywell
WX
ET
NO BEARING
RA 9 . 8NM +13
TA4 . 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
TCAS MENU
EMER
TERR
MAP
PLAN
NAV
APT
NORM ABN
SKP
RCL
PAG
ENT
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
SPD FMS MAN
CRS 1 CRS 2
PUSH DCT PUSH DCT
HDG ALT
DN
UP
P
I
T
C
H
Honeywell
FD AP FD
CPL
YD
FLC NAV HDG BANK VNAV ALT
APR VS
BC
PUSH CHG PUSH SYNC
RADAR LSS TILT
TST
FP
GMAP
CLR
TST
SBY OFF
WX RCT SBY LX
PULL
ACT
+
–
GAIN
MIN MAX
PULL
VAR
TRB STAB TGT SECT
OFF
RADAR LSS TILT
TST
FP
GMAP
CLR
TST
SBY OFF
WX RCT SBY LX
PULL
ACT
+
–
GAIN
MIN MAX
PULL
VAR
TRB STAB TGT SECT
OFF
TCAS MENU
EMER
TERR
MAP
PLAN
NAV
APT
NORM ABN
SKP
RCL
PAG
ENT
FMS 1 FMS 2
STAT
HYD
AC
ELEC
BLEED
AIR
COND
DC
ELEC
FUEL
FLT
CTRL
SCROLL
EICAS
SYSTEMS SELECT
NORM
MFD 1 MFD 2
IRS 1 IRS 3 IRS 2
NAV NAV NAV
ALN ALN ALN
OFF OFF OFF
ATT ATT ATT
MINIMUMS
RAD BARO IN Hpa
NAV SRC BARO SET
BRG V/L FMS BRG
HSI
Honeywell
PUSH STD
MINIMUMS
RAD BARO IN Hpa
NAV SRC BARO SET
BRG V/L FMS BRG
HSI
Honeywell
PUSH STD
For Training Purposes Only
Sept 04
7-65
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
DESCRIPTION
PITOT-STATIC SYSTEM
Three pitot-static (PS) systems designated PS1, PS2, and PS3 and a standby PS source
are provided to supply variable pressure inputs to the 3 Air Data Computers (ADC),
the standby instruments and to the Mach transducer. Use and distribution of these
pitot-static probes is as follows (refer to “Pitot-Static Schematic” on page 7-66):
Three Total Air Temperature (TAT) probes are provided to supply temperature input to
the ADCs. Ice protection is provided by electric heating elements for the PS probes
and TAT probes. Please refer to Chapter 3, ANTI-ICE SYSTEMS.
PRESSURE SOURCE FROM TO
P1 Pitot/Static Probe No. 1 MADC No. 1
P2 Pitot/Static Probe No. 2 MADC No. 2
P3 Pitot/Static Probe No. 3 MADC No. 3
Ps Standby Pitot/Static Probe Standby Instruments / Mach Transducer
S1/S2 Pitot/Static Probe No. 1 and Standby MADC No. 1
S1/S2 Pitot/Static Probe No. 2 and No. 3 MADC No. 2
S1/S2 Pitot/Static Probe No. 3 and No. 2 MADC No. 3
S1/S2 Standby Pitot/Static Probe and No. 1 Standby Instruments / Mach Transducer
TOP
VIEW
PS 3 PS 2
PS 1 PS
Standby
TAT 2
TAT 3 PS2
TAT 3
PS
Standby
ENGINE INLET
TAT 1/2
Probe
PS3
PS1 TAT1
GX_07_038
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
7-66 For Training Purposes Only
Sept 04
PITOT-STATIC SCHEMATIC
GX_07_039
p
p p
s2
s2 s2
s1
s1
p
s2
s1
s1
MADC
NO. 1
MADC
NO. 3
MACH
TRANSDUCER
VALVE
P3
LOWER
LEFT
P1
UPPER
LEFT
P2
LOWER
RIGHT
P/S
STDBY
UPPER
RIGHT
MADC
NO. 2
STANDBY ALTIMETER /
AIRSPEED INDICATOR
MACH
TRANSDUCER
LOWER
MANIFOLD
UPPER
MANIFOLD
DRAINS DRAINS
DRAINS
DRAINS
S IN
S
OUT
　
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