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cftsuencjer
OPERATING MANUAL
PSP 601A-6
SECTION 11
FLIGHT INSTRUMENTS
TABLE OF CONTENTS
Page
1 . GENERAL 1
2. PITOT-STATIC SYSTEM AND TEMPERATURE SENSING SYSTEM 1
3. DIGITAL AIR DATA SYSTEM 1
4. ELECTRONIC FLIGHT INSTRUMENT SYSTEM 2
LIST OF ILLUSTRATIONS
Figure
Number Title Page
1 Pi t o t - S t a t i c System - Schematic 3
2 Pi t o t - S t a t i c System - Components 4
3 Pitot-Static System - Standby Indicators 5
4 DADS - Simplified Block. Diagram 6
5 DADS - Mach/Airspeed Indicators and Altimeters 7
6 DADS - Vertical Speed Indicators and Associated AFCS Advisory Display 8
7 DADS - EFIS EADI Air Data Displays (2 Sheets) 9
8 DADS - EFIS Instrument Remote Controllers 11
9 EFIS - Simplified Block Diagram 12
10 EFIS - EADI Normal Displays 13
11 EFIS - EADI Failure Warning Annunciators (2 Sheets) 14
12 EFIS - EADI Category 2 Annunciator 16
13 EFIS - EADI Comparison Monitor Annunciators 17
14 EFIS - EADI Reversionary Source Annunciators 18
11-CONTENTS
Page 1
Apr 02/87
Fi gure
Number
16
17
18
19
20
21
22
23
24
25
26
27
28
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
EFIS
OPERATING WIMWL
PSP601A-6
Title Page
EHSI Full Compass Mode 19
EHSI ARC Mode 20
EHSI MAP Mode 21
EHSI Weather Radar Display 22
EHSI Failure Warning Annunciators 23
EHSI Comparison Monitor Annunciator 24
EHSI Reversionary Source Annunciators 25
Composite Display 26
MFD MAP Mode 27
MFD PLAN Mode 28
Display Controller 29
Instrument Remote Controllers 30
MFD Controller 31
Remote Switch/Lights 32
11-
Page 2
Apr 02/87
OPERATING MANUAL
PSP 601A-6
SECTION 11
FLIGHT INSTRUMENTS
GENERAL
The flight instrument systems consist of the pi tot-static system, the
temperature sensing system, the digital air data system, the electronic flight
instrument system and the vertical gyros.
PITOT-STATIC SYSTEM AND TEMPERATURE SENSING SYSTEM (Figures 1, 2 and 3)
The pi tot-static system provides the pi tot and static pressures required to
operate the digital air data computers No- 1 and No. 2 (DADC 1 and DADC 2) and
the standby pneumatic airspeed indicator (ASI). Static pressure is provided to
operate the standby pneumatic altimeter (ALT), and the cabin pressure indicator
(CPI). The pi tot-static system consists of the pilot's and copilot's
pi tot-static heads, the left and right static ports, and the pilot's and
copilot's STATIC PRESSURE SELECTOR valves. A dual temperature-sensing probe,
located on the right side of the forward fuselage, provides a
total-air-temperature (TAT) input to DADC 1 and DADC 2. The pi tot tubes,
static ports and temperature probe contain anti-icing heater elements that are
controlled from the A.D.S. HEATER CONT. panel.
For a description of the CPI, refer to Section 2.
DIGITAL AIR DATA SYSTEM (Figures 4 through 9)
The digital air data system provides the flight guidance computers and control
systems with altitude hold, airspeed programming, vertical speed and Mach
control information. The digital air data system also provides altitude
alerting and reporting and indications of altitude, airspeed, vertical speed,
true airspeed, static air temperature and total air temperature.
The digital air data system consists of two complete systems with two digital
air data computers, DADC 1 and DADC 2. The DADCs receive total pi tot-static
pressures from the pi tot-static system, and temperature signals from the
total-air-temperature probe. Other inputs to the DADCs are from the BARO
control on the barometric altitude indicator, the copilot's ALT SEL control on
the electronic flight instrument system (EFIS) remote controller, and flap
position information from the flap control unit. From these inputs, the DADCs
compute and generate output signals for the following systems or components:
Pilot's and copilot's Mach/airspeed indicators (MASI)
Pilot's and copilot's altimeters
SECTION 11
Page 1
Apr 02/87
ctvanenaer
OPERATING MANUAL
PSP 601A-6
Pilots and copilot's vertical speed indicators (VSI)
Pilots and copilot's electronic flight instrument system (EFIS)
Automatic flight control system (AFCS)
Aural warning system
Flight management system (FMS)
ATC transponder system
Master caution and warning system
The AFCS advisory display panel displays static-air-temperature (SAT), total
air temperature (TAT) and true airspeed (TAS).
The digital air data system consists of two digital air data computers, two
Mach/airspeed indicators, two altimeters, two vertical speed indicators and a
dual TAT probe.
ELECTRONIC FLIGHT INSTRUMENT SYSTEM (Figures 9 through 28)
The electronic flight instrument system (EFIS) converts inputs from the
aircraft sensors, long-range navigation (LRN) and short-range navigation (SRN)
systems into video signals for display on electronic display units.
The EFIS comprises three subsystems: the pilot's display system, the copilot's
display system and the multifunction display (MFD) system.
The pilot's and copilot's display systems are identical, each using two
electronic display units to provide conventional attitude director and
horizontal situation information, using a display controller, an instrument
remote controller and a symbol generator. In addition to the conventional
displays, the electronic attitude director indicator (EADI) and electronic
horizontal situation indicator (EHSI) provide a number of other displays such
as IAS/Mach, map and weather radar displays, selectable from the display
controllers. The display controllers also provide for navigation source
selection and bearing source selection. The pilot's and copilot's instrument
remote controllers provide for control of the flight director related displays
on the EADI and EHSIThe
MFD system provides additional long-range mapping information, checklists
and weather radar displays (refer to Section 11). The MFS system can also
serve as a back-up system for either the pilot's or copilot's display system.
The MFD controller provides for selection and control of the MFD formats,
modes, waypoint designators and back-up modes.
SECTION 11
Page 2
Apr 02/87
OPERATING MANUAL
PSP 601A-6
LEGEND
PILOTS
PITOT-STATIC
HEAD
PITOT PRESSURE UNE
STATIC PRESSURE LINE COPILOTS
PITOT-STATIC
HEAD
晻?
?
01
ALT. STATIC SOURCE SW.
PILOTS SIOE CONSOLE
DRAIN =<D>-fi
DRAIN
DADC1
SI DRAIN S2 DRAIN
CENTRE INSTRUMENT PANEL
P2
V
COPILOTS
SIDE PANEL
anttp
MANIFOLD S-_
limit
DRAIN
??
STATIC
PORT
S3
STATIC
PORT
S3
atttittratintituiiii
ALT. STATIC SOURCE SW.
COPILOTS SIDE CONSOLE
?O DRAIN
DADC2
DRAIN
Pi tot-Static System - Schematic
Figure 1
SECTION 11
Page 3
Apr 02/87
OPERATING MANUAL
PSP G01A-6
f: IK'.
PITOT HEAT FAIL ANNUNCIATOR
Indicates a failure of the on-side pitot-static tube
heater.
O
HTR FAIL SWTTCrVUGHT
Indicates a static port, angie-ofattack
<AOA> vane and/or totahairtemperture
(TAT) probe heater
failure.
PWR ? METER SELECT SWITCH
Turns on heater elements (when set to any
position except HTRS OFF) for the static ports,
the pitot-static tubes, the angje-of-attack (AOA)
vanes, and the total-air-temperature (TAT) probe.
The switch also selects the current readings
indicated by the % HTR CURRENT meter.
% HTR CURRENT METER
Indicates the percentage of current
drawn by the heater selected by the
PWR B METER SELECT switch.
SAFETY GUARD REMOVED
FOR CLARITY
PILOTS AND COPILOTS SELECTOR VALVES
STATIC TUBE - The on-side cfigrtaJ air data
computer receives static pressure inputs from the
primary source.
ALTERNATE SOURCE - The on-side dgrtai air
data computer receives stauc pressure from the
secondary (alternate) source.
Pitot-Statlc System - Components
Figure 2
SECTION 11
Page 4
Apr 02/87
BARO
CONTROL
OPERATING MANUAL
PSP 601A-6
STANDBY AIRSPEED
INDICATOR
ALTITUDE
POINTER
ALTITUDE
INDICATOR
BARO
INDICATOR
CENTRE INSTRUMENT PANEL
Pi tot-Static System - Standby Indicators
Figure 3
SECTION 11
Page 5
Apr 02/87
OPERATING MANUAL
PSP 601A-6
ATC1
PfTOT-STATIC
INPUTS
[FLAP
.CONTROL
UNIT
FLAP
POSITION
COPILOTS INSTRUMENT
REMOTE CONTROLLER
ALTSEL
TAT
AFCS ADVISORY
DISPLAY
ALTITUDE
REPORTING
DADC1
MACH/AIRSPEED
ALTTTUDE/BARO CORRECTION
TO MASTER CAUTION
AND WARNING SYSTEM
VERTICAL SPEED
PiLOT S
MACH/AIRSPEED
INDICATOR
PILOTS
ALTIMETER
PILOTS
VERTICAL
SPEED
INDICATOR
ALTITUDE ALERT/OVERSPEED
PILOTS EADI
K ASCB
ALTSEL
TAT
{ PROBE
TAT
FLAP POSITION
PfTOT-STATIC
INPUTS
DADC2
2EL/ TO FMS, EFIS
IRS AND AFCS
AURAL
WARNING
SYSTEM
MACH/AIRSPEED
ALTITUDE ALERT/OVERSPEED
COPILOTS
MACH/AIRSPEED
INDICATOR
^ TO MASTER CAUTION
^ AND WARNING SYSTEM
COPILOTS
ALTIMETER
COPILOTS
VERTICAL
SPEED
INOICATCP.
COPILOTS EADI
ALTITUDE
REPORTING
ATC2
DADS - Simplified Block Diagram
Figure 4
SECTION 11
Page 6
Apr 02/87
MACH COUNTER
VMO POINTER
AIRSPEED
POINTER
MEMORY INDEX
POINTER (YELLOW)
POINTBl
BARO SET KNOB
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ctianentjer
OPERATING MANUAL
PSP 601A-6
MACH/AIRSPEED INDICATOR
BARO COUNTERS
ALTIMETER
MEMORY INDEX
POINTER (WHITE)
FAILURE
WARNING FLAG
MEMORY INDEX
POINTER (RED)
MEMORY INDEX
POINTER (GREEN)
ALTITUDE ALERT
ANNUNCIATOR
FAILURE WARNING
FLAG
ALTITUDE
COUNTER
PILOTS AND COPILOT'S INSTRUMENT PANELS
DADS - Mach/Airspeed Indicators and Altimeters
Figure 5
SECTION 11
Page 7
Apr 02/87
OPERATING MANUAL
PSP 601A-6
VERTICAL SPEED INDICATOR
POINTER
FAILURE
WARNING
FLAG
PILOTS AND COPILOrS INSTRUMENT PANELS
SAT DISPLAY
Displays SAT in < t Celsius.
TAT DISPLAY
Displays TAT in degrees
Celsius.
TAS DISPLAY
Displays TAS in knots.
BRT CONTROL
Controls the overall display
brightness.
CENTRE INSTRUMENT PANEL
DADS - Vertical Speed Indicators and
Associated AFCS Advisory Display
Figure 6
SECTION 11
Page 8
Apr 02/87
ctianenefer
OPERATING MANUAL
PSP 601A-6
IAS ACCELERATION TREND VECTOR
Indicates the air a aft IAS trend based
on acceleration. Displayed in magenta
and inhibited below GO knots.
IAS/MACH REFERENCE BUG
Indicates the IAS or Mach reference
selected on the pilot's instrument
remote controller. Displayed in cyan.
MACH DISPLAY
Displays Mach number at or above
0.45 Mach. Display is removed below
0.40 Mach. Resolution is 0.002 Mach.
The colour of the Mach display is the
same as described for the IAS display.
FMS SPEED BUG
indicates the FMS reference speed
when the flight director VNAV mode is
selected. Displayed in magenta.
IAS/MACK REFERENCE DISPLAY
Provides a readout of the lAS/Mach
reference bug with respect to the
PILOTS AND COPILOT'S INSTRUMENT PANEL
DADS - EFIS EADI Air Data Displays
Figure 7 (Sheet 1)
SECTION 11
Page 9
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IAS COMPARISON MONITOR
ANNUNCIATOR
Rashes (amber) for 10 seconds and
then comes on steady to indicate a 5
knots or more difference between tne
on-side and cross-side (AS sources, for
greater than 2 seconds. The IAS
comparison monitor function is
inhibited at SO knots or less.
VMO INDICATOR
Indicates the aircraft maximum
operating velocity (VMO}. Displayed in
red.
AoLl. DISPLAY
Ots&toys the selected amurfe for the
flight atrector A 5 ?L mode, nartge &
from 0 to 60,000 feet, selectable in 100
foot increments.
When the on-side EHSI and DADC are
coupled to the master flight guidance
computer, the Display and surrounding
box are displayed in cyan. When the
cross-side EHSI and DADC are coupled
to the master FGC. the surrounding
box is changed to yellow.
IAS DISPLAY AND SCALE
The IAS display and scale provide an
indication of the IAS from 40 to 450
knots. Below 40 knots the IAS display
is removed.
When the IAS data source is on-side
the IAS display is green. When the
source is cross-side, the cSsptay is
yeBow. When the IAS exceeds the
rafetence IAS. in the fSght director
FLC or VFLC modes, by ?5 knots.
the display is amber. When the IAS
exceeds VMO. as indicated by the
VMO indicator, the olspiay is red.
Whan the IAS acceleration trend
vector exceeds the VMO, the display is
smber.
IAS REVISION ANNUNCIATOR
Indicates a cross-side transfer of IAS
data. An amber boxed XIAS is
displayed on the receiving side and an
amber boxed green IAS is displayed on
the transferring side
NOTES
1 When IAS data from the coupled-side DADC is not
vafid, an IAS related displays are removed and a
ted boxed IAS annunciation is displayed.
2 When the altitude preselect "function faSs the ASEL
display is removed and a red boxed ASEL is
displayed.
DADS - EFIS EADI Air Data Displays
Figure 7 (Sheet 2)
SECTION 11
Page 10
Apr 02/87
OPERATING MANUAL
PSP 601A-6
PILOT'S INSTRUMENT REMOTE CONTROLLER
IAS/MACH PUSH CHG CONTROL/
SWITCH
Rotating the IAS/MACH PUSH
CHG control/switch causes the IAS
or Mach references displayed on the
pilot's and copilot's EADls, to
change. Pressing the IAS/MACH
PUSH CHG control/switch causes
the IAS reference to change to a
Mach reference and vice versa. The
push-to-change function is inhibited
when the aircraft is on the ground.
GLARESHIELD (PILOT'S SIDE)
ALT SEL CONTROL
Rotating the ALT SEL control
causes the ASEL displays, on the
pilot's and copilot's EADls to
change.
COPILOTS INSTRUMENT REMOTE CONTROLLER
GLARESHIELD (COPILOTS SIDE)
DADS - EFIS Instrument Remote Controllers
Figure 8
SECTION 11
Page 11
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IRS1
DME:
NAV 1 -
ADF1
PILOT'S
SIDE
EADI
CENTRE
EHSi
DISPLAY CONTROLLER
Q O ?O
PILOTS
SYMBOL
SENERATORl
IRS1 -
DME1-
NAV1-
ADF1 -
WXINSTRUMENT
REMOTE
CONTROLLER
MFD
MFD CONTROLLER
00O甇D
皁g??
MFD
SYMBOL
GENERATOR
ASCB
COPILOTS
SIDE
e~L>:
K>桲^A V
EHSI
DISPLAY CONTROLLER
n M i i n
Q O O O
IRS 2
DME 2
NAV2
AOF2
RA
COPILOTS
SYMBOL
GENERATOR
IRS 2
OME2
NAV2
ADF2
RA
WX
TO/FROM FMS 1 AND FMS 2
IRS 1 AND IRS 2. AFCS 1
AND AFCS 2 AND DADS 1
AND DADS 2
INSTRUMENT REMOTE
CONTROLLER
EFIS - Simplified Block Diagram
Figure 9
SECTION 11
Page 12
Apr 02/87
OPERATING MANUAL
PSP 601A-6
FLIGHT DIRECTOR
MODE ANNUNCIATORS
DECISION
HEIGHT
ANNUNCIATOR
ROLL
SCALE
VMO
INDICATOR
FLIGHT
DIRECTOR
COMMAND
CUE
IAS DISPLAY
IAS ACCEL
TREND
VECTOR
IAS SCALE
FMS SPEED
BUG
IAS/MACH
REFERBSICE
BUG
MACH
DISPLAY
MARKER
BEACON
ANNUNCIATOR
AUTOPILOT
ANNUNCIATOR
ALTITUDE PRESELECT
DISPLAY
VERTICAL TRACK
ALERT ANNUNCIATOR
VERTICAL NAVIGATION
POINTER
GUDESLOPE
POINTER
AIRCRAFT SYMBOL
LOCALIZER
POINTER/
RISING
RUNWAY
RADIO
ALTITUDE
DISPLAY
DECISION
HEIGHT
DISPLAY
INCLINOMETER
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EADI Normal Displays
Figure 10
SECTION 11
Page 13
Apr 02/87
OPERATING MANUAL
PSP 601A-6
ATTITUDE
FAILURE
ANNUNCIATOR
ATTITUDE FAILURE
FLIGHT
DIRECTOR
FAILURE
ANNUNCIATOR
FLIGHT DIRECTOR FAILURE
PILOTS AND COPILOT'S INSTRUMENT PANELS
EFIS - EADI Failure Warning Annunciators
Figure 11 (Sheet 1)
SECTION 11
Page 14
Apr 02/87
cftanerujer
OPERATING MANUAL
PSP 601A-6
IAS FAILURE
ANNUNCIATOR
LOCALIZER
FAILURE
ANNUNCIATOR
ASEL FAILURE
ANNUNCIATOR
CROSS-SIDE
DATA FAILURE
ANNUNCIATOR
GLIDESLOPE
FAILURE
ANNUNCIATOR
RADIO
ALTITUDE
FAILURE
ANNUNCIATOR
IAS, ALTITUDE PRESELECT. CROSS-SIDE DATA.
GLIDESLOPE. VERTICAL NAVIGATION, RADIO
ALTITUDE AND LOCALIZER FAILURES
SYMBOL
GENERATOR
INTERNAL
FAILURE
ANNUNCIATOR
SYMBOL GENERATOR INTERNAL FAILURE
EFIS - EADI Failure Warning Annunciators
Figure 11 (Sheet 2)
SECTION 11
Page 15
Apr 02/87
OPERATING MANUAL
PSP 601A-6
CAT 2 INVALID
ANNUNCIATOR
FOOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EADI Category 2 Annunciator
Figure 12
SECTION 11
Page 16
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IAS
COMPARISON
MONITOR
ANNUNCIATOR
LOCALIZER
COMPARISON
MONITOR
ANNUNQATOR
ATTITUDE
COMPARISON
MONITOR
ANNUNCIATOR
GLIDESLOPE
COMPARISON
MONITOR
ANNUNCIATOR
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EADI Comparison Monitor Annunciators
Figure 13
SECTION 11
Page 17
Apr 02/87
OPERATING MANUAL
PS? 601A-6
IAS REVERSION
ANNUNCIATOR
SG REVERSION
ANNUNCIATOR
IRS REVERSION
ANNUNCIATOR
PILOTS AND COPILOT'S INSTRUMENT PANELS
EFIS - EADI Reversionary Source Annunciators
Figure 14
SECTION 11
Page 18
Apr 02/87
ctvanenaer
OPERATING MANUAL
PSP601A-6
WIND
VECTOR
DISPLAY
HEADING
SELECT BUG
FORE
LUBBER
LINE
HEADING
SOURCE
ANNUNCIATOR
COURSE SELECTS
DESIRED TRACK
DISPLAY
BEARING
POINTS?
NO. 1
NAVIGATION*
SOURCE
ANNUNCIATOR
COURSE
PRESELECT
SOURCE
ANNUNCIATOR
BEARING
POINTER
SOURCE
ANNUNCIATOR
COURSE
DEVIATION 8AR
FMS FMS
MESSAGE DRIFT
ANNUNCIATOR BUG
TARGET ALERT
ANNUNCIATOR
DISTANCE
DISPLAY
WAYPOINT/DME RECIPROCAL
IDENTIFIER COURSE
PRESELECT
POINTER
RECIPROCAL
COURSE
POINTER
COURSE
昉RESELECT
POINTER
GLIDESLOPE
POINTER
COURSE
SELECT/DESIRED TRACK
POINTER
?TO-FROM
POINTER
"AIRCRAFT
SYMBOL
COURSE PRESELECT
DEVIATION BAR
TIME-TO-GO
DISPLAY
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI Full Compass Mode
Figure 15
SECTION 11
Page 19
Apr 02/87
OPERATING MANUAL
PSP 601A-6
PARTIAL
HEADING DIAL
COURSE/DESIRED
TRACK DISPLAY
OFF SCALE
ARROW
NAV SOURCE
ANNUNCIATOR
COURSE
PRESELECT
ANNUNCIATOR
BEARING
POINTER
SOURCE
ANNUNCIATOR
DISTANCE
DISPLAY
WIND
VECTOR
DISPLAY
COURSE
SELECT/
DESIRED
TRACK
POINTER
FORE HEADING FMS
LUBBER SOURCE MESSAGE
UNE ANNUNCIATOR ANNUNCIATOR
TARGET ALERT
ANNUNCIATOR
HEADING
SELECT
DISPLAY
HEADING
SELECT BUG
FMS DRIFT
BUG
COURSE
PRESELECT
POINTER
GUDESLOPE
POINTER
COURSE
PRESELECT
DEVIATION BAR
GROUND
SPEED
DISPLAY
WAYPOINT/DME
IDENTIFIER
BEARING
POINTS
NO. 1
COURSE AIRCRAFT TO/FR
DEVIATION SYMBOL ANNUNCIATOR
BAR
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI ARC Mode
Figure 16
SECTION 11
Page 20
ApT 02/87
ctiauenejer
COURSE
SELECT
DISPLAY
VOR STATION
SYMBOL
SELECTED
COURSE UNE
OPERATING MANUAL
PSP 601A-6
SELECTED BEARING NO. 2
DISPLAY
CROSS-TRACK
DISTANCE DlSP! * v
VOR NAVIGATION SOURCE
VOR BEARING
WAYPOINTS
STATION SYMBOLOGY
VOR ONLY - O ?MS ONLY)
VOR/DME- ?
DME ONLY -<? (FMS ONLY)
CROSS-TRACK
DISTANCE DISPLAY
FMS NAVIGATION SOURCE
WAYPOINT
LEG
TO WAYPOINT
IDENTIFIER
WAYPOINT
FLIGHT LEVEL
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI MAP Mode
Figure 17
SECTION 11
Page 21
Apr 02/87
MODS
ANNUNCIATOR
OPERATING MANUAL
PSP 601A-6
ALERT
ANNUNCIATOR
RANGE RING
WX RETURN
DISPLAY
RANGE
ANNUNCIATOR
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI Weather Radar Display
Figure 18
SECTION 11
Page 22
Apr 02/87
OPERATING MANUAL
PS? 601A-6
IRS FAILURE
ANNUNCIATOR
/ t
IOI
CRS
349
^ \
V
o ?
R -=-?
1 r
.xXM'i'/'/,.
HDG
340
v?
ir
DME ?',/? s ?\ \
^
180
RNE I
TTG
34.5
o
V^z J
X^LS
HEADING FAILURE
NAV SOURCE
FAILURE
ANNUNCIATOR
/Z
N j
Q MAG
V
HDG
340 = >
GLIDESLOPE
FAILURE
ANNUNCIATOR
NAVIGATION SOURCE AND GUDESLOPE
FAILURE
PILOT'S AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI Failure Warning Annunciators
Figure 19
SECTION 11
Page 23
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IRS HEADING
COMPARISON
MONITOR ANNUNCIATOR
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI Comparison Monitor Annunciator
Figure 20
SECTION 11
Page 24
Apr 02/87
OPERATING MANUAL
PSP 601A-6
SG REVERSION
ANNUNCIATOR
IRS REVERSION
ANNUNCIATOR
PILOT'S AND COPILOTS INSTRUMENT PANELS
EFIS - EHSI Reversionary Source Annunciators
Figure 21
SECTION 11
Page 25
Apr 02/87
OPERATING MANUAL
PS? 601A-6
COURSE SELECT/
DESIRED TRACK
DISPLAY
NAVIGATION
SOURCE
ANNUNCIATOR $
TO/!=R
A*NEL,rrtClATC=:
COURSE
DEVIATION COURSE
POINTER SELECT/DESIRED
TRACK
POINTER
GLIDESLOPE
POINTER
HEADING SELECT
DISPLAY
HEADING SELECT
BUG
MOTE
PILOTS AND COPILOTS INSTRUMENT PANELS
The composite cfisptey is a reversionary mode, used to provide both
essential attitude cfirector and horumiuri situation information on one
display, in the event that an electrooic OBptoy unit fafls.
EFIS - Composite Display
Figure 22
SECTION 11
Page 26
Apr 02/87
OPERATING MANUAL
PSP 601A-6
DISTANCE AND COURSE
TO DESIGNATOR
HEADING
DIAL
LUBBER
LINE
TUNED
VOR/DME
NAVIGATION
SOURCE ANNUNCIATOR
VOR/DME
NAVAID SYMBOL
^ ^ VOR/DME
^ ^ D M E ONLY
O VORONLY
AIRPORT
IDENTIFIER
RANGE
RING
DESIRED
TRACK
LINE
WEATHER
RADAR
MODE
DESIGNATOR
LATITUDE/
LONGITUDE
DISPLAY
TGT/VAR
ANNUNCIATOR
AIRCRAFT SYMBOL
-TO** WAYPOINT
DISPLAY
ETA TTG
IN OR IN
GMT HR:MN
DISTANCE
T O T O '
WAYPOINT
DISPLAY
DESIGNATOR
DISPLACEMENT LINE
CROSS-TRACK
DEVIATION
DISPLAY
CENTRE INSTRUMENT PANEL
EFIS - MFD MAP Mode
Figure 23
SECTION 11
Page 27
Apr 02/87
OPERATING MANUAL
PSP 601A-6
DISTANCE AND COURSE
TO DESIGNATOR
AIRCRAFT
SYMBOL
TUNED
VOR/DME
SELECTED
NAV SOURCE
MAG
ANNUNCIATOR
-NORTH-UP*
IDENTIFIER
DISPLACEMENT
LINE
DESIGNATOR
RANGE
AIRPORT
ANNUNCIATOR
WEATHER
RADAR
MODE
TGT/VAR
ANNUNCIATOR
TO" WAYPOINT
DESIGNATOR
LATITUDE/
LONGITUDE
DISPLAY
ETA TTG
IN OR IN
GMT HRrMN
RANGE
RING
WAYPOINT DISTANCE TO
T O " WAYPOINT
CENTRE INSTRUMENT PANEL
EFIS - MFD PLAN Mode
Figure 24
SECTION 11
Page 28
Apr 02/87
cttanenefer
OPERATING MANUAL
PSP 601A-6
GSPD/TTG PUSHBUTTON
Alternately selects ground
speed (GS) or time-to-go (TTG)
for display. /<
WX PUSHBUTTON
Selects weather radar returns
for display in partial compass
format.
MAP PUSHBUTTON
Selects display of active
waypornts and VOR/DME
ground station positions on
partial compass display.
ET PUSHBUTTON
Selects elapsed time display
instead of GS/TTG display.
V/L PUSHBUTTON
Selects between the on-side
and cross-side SRN systems
(see note).
FULL/ARC PUSHBUTTON
Selects full compass (360
degrees of heading} or partial
compass (90 degrees of
heading) format for display.
BRG O KNOB
Selects the bearing source for
the No. 1 bearing pointer on
the EHSl.
ADl DIM (OUTER) CONTROL
Adjusts the brightness of the
EAOI display. When set to OFF.
the EHSl displays a composite
EAOI and EHSl.
FMS PUSHBUTTON
Selects between the on-side
and cross-side LRN system
(FMS).
BRG O KNOB
Selects the bearing source for
the No. 2 bearing pointer on
the EHSl.
WX DIM (INNER) CONTROL
Adjusts the brightness of the
weather radar returns on the
EHSl.
OH/TST (INNER) CONTROL
Rotating the control adjusts the
decision height display on the
EAOI. When pressed activates
the test mode.
HSl DIM (OUTER) CONTROL
Adjusts the brightness of the
EHSl display. When set to OFF.
the EADl displays a composite
EAOI and EHSL
PILOT'S AND COPILOT'S SIDE PANELS
NOTE
SRN systems are the VHF navigation
system and the DME system.
EFIS - Display Controller
Figure 25
SECTION 11
Page 29
Apr 02/87
OPERATING MANUAL
PSP 601A-6
HDG PUSH SYNC PUSHBUTTON
When rooted, moves the heading
bug on the p8ot's EHSl. When
pressed, causes the heading bug to
synchronize to the aircraft heading.
IAS/MACH PUSH CHG CONTROL/
SWITCH
When rotated, adjusts the
lAS/Mach reference on the pilot's
and copilot's EAOis. When pressed.
change the IAS reference to the
Mach reference or vice versa. The
push-to-change function is inhibited
with the aircraft on the ground.
CRS PUSH OCT CONTROL/
SWITCH
When rotated, rnoves the course
select pointer on the associated
EHSl. When pressed, causes the
course pointer to indicate the 2ero
deviation course to the tuned VOR
station. When an FMS source is
selected, rotating the control causes
the preselect course pointer to
move.
ALT SEL CONTROL
When rotated, adjusts the
AScL display on the pilot's
and copilot's EADJs.
HOG PUSH SYNC PUSHBUTTON
When rotated, moves the heading
bug on the copdot's EHSl. When
pressed, causes the heading bug to
synchronize to the aircraft heading.
GlARESHiELD
EFIS - Instrument Remote Controllers
Figure 26
SECTION 11
Page 30
Apr 02/87
OPERATING MANUAL
PSP 601A-6
WX PUSHBUTTON
Selects the weather radar
information for display on the MFD
indicator.
NORM PUSHBUTTON
Selects checklist index page for
display on MFD indicator.
SRC PUSHBUTTON
Selects long range navigation source
for MAP and PLAN modes.
MAP/PLAN PUSHBUTTON
Alternately selects MAP or PLAN
format for MFD indicator display.
VOR PUSHBUTTON
Selects VOR/DME information
for display on MFD indicator.
INC/DEC RNG CONTROL
Increases or decreases the range
display on the MFD indicator.
EMER PUSHBUTTON
Selects emergency checklist index
page for display on MFD indicator.
SKP PUSHBUTTON
Allows skipping of designator or
active lines.
DAT PUSHBUTTON
Allows additional long range
navigation information to be added
to the MAP or PLAN mode display
ENT PUSHBUTTON
Enters designator as a waypotm.
checks off a line or selects an index
line item for display.
RCL PUSHBUTTON
Recalls designator to home position
or recalls lowest numbered skipped
tine in a checklist.
PAG PUSHBUTTON
Advances the page count and places
the active line selection at first line
of the page.
CENTRE PEDESTAL
EFIS - MFD Controller
Figure 27
SECTION 11
Page 31
Apr 02/87
OPERATING MANUAL
PSP 601A-6
COMP WON SWITCH/LIGHT
Comes on (amber) to indicate that a
difference exists between one of the
on-side and cross-side sources. The
out-of -tolerance source is indicated
on the EADl. When pressed, resets
the comparison circuits.
SG REV SWITCH/UGHT
When pressed, selects the cross-side
symbol generator as a back-up when
the on-side symbol generator fafls.
IAS REV SWITCH/LIGHT
When pressed, selects the cross-side
OADC as a back-up IAS source
when the on-side source fails.
IRS REV SWTTCH/UGHT
When pressed, selects the cross-side
IRS as back-up when the on-side
IRS source fails.
FD REV SWITCH/LIGHT
When pressed, selects the cross-side
flight guidance computer (FGC) as a
back-up flight director when the onside
FGC fails.
PILOTS AND COPILOTS INSTRUMENT PANELS
EFIS - Remote Switch/Lights
Figure 28
SECTION 11
Page 32
Apr 02/87

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