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used to scroll through data.
Selections made by pressing
BRT+ key to move cursor up,
then pressing ENTER key to
activate selection.
Selections made by pressing
DIM -- key to move cursor down,
then pressing ENTER key to
activate selection.
The CLR key used to back out
of sub--modes.
CLR BRT + DIM --
ENTER 0
1 2
4 5
7 8
HGS Test Menu Page
Vol. 1 12--70--13
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual
CSP A--013
MASTER
Head---up Guidance System --- Test Mode Selections
Figure 12---70---6 Sheet 2
LEG #1 A/C ID #7002
ENTER LEG #
EFFECT
APPCH WARN
FAULT
ADC1 SELCT ALT
HGS HCP/90
APM NO AIII CAP
REF MACH
APM APCH WARN
NO AIII CAP
25 FAULTS
Applicable
Airplane
Tail Number
Scroll
Indicators
Scrolling / Clear :
BRT+ key used to move
cursor up,
DIM -- key used to move
cursor down,
CLR key used to back out of
sub--modes.
Fault Effects Column
Indicates effect of
corresponding recorded fault
(located on adjacent line).
Indication can be blank (no
effect), or a loss of category IIIa
capability (NO AIII CAP) or
fault resulted in an approach
warning (APPCH WARN)
Recorded Faults Column
Identifies failure and
failed unit.
Total Number Faults for this Leg
(Max 126 faults per leg)
Enter Leg
Number Prompt
/ Readout
Used along with
HGS control Panel
to enter a specific
leg number.
Recorded Faults Page
Used to gain access to
recorded fault data for current
flight leg or one of the
preceding legs (max 127 legs
stored in memory)
Table format used to display
fault information.
Leg Number
Indicator
Range is from #1
hru #127,
progressing from
current leg (#1)
backwards thru
previous legs.
INVALID
INAC
INVALID
ADC2
REV 56, Jan 31/03
Vol. 1 12--70--14
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual MASTER
CSP A--013
Head --- up Guidance System --- Test Mode Selections
Figure 12---70---6 Sheet 3
EXISTING FAULTS
ACTIVE FAULT
HGS REF G/S
HGS RUNWAY/ELEV
W/S VALID
HGS OHU/60
APM MARKERS
8 FAULTS
Scrolling / Clear :
BRT+ key used to move
cursor up,
DIM -- key used to move
cursor down,
CLR key used to back out of
sub--modes.
Existing Faults Page
Indicates faults detected
within the last 2 seconds.
Table format used to display
fault information.
Total Number Faults Detected
(last 2 seconds)
(Max 256 faults)
Scroll
Indicators
Recorded Faults Column
Identifies failure and failed unit.
ACT
STBY
ELV
G/S
FAULT CLR BRT + DIM --
HGS Control Panel (1)
Center Pedestal
Fault Lamp
(amber)
Fault Code / Messages
LED panel indicates
corresponding fault code /
system message:
HC 10 thru HC 57 (Computer)
OHU 60 thru OHU 68
(Overhead Unit)
DEU 70 thru DEU 78 (Display
Electronics Unit)
HC 88 (System in Test Mode)
HC89 (Vector Generator in
Test Mode)
HCP 90 thru HCP 98 (Control
Panel Fault)
Combiner B1 (Combiner not
aligned)
FAIL
INAC
FAIL
FAIL
FAIL
GPW1
Vol. 1 12--70--15
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual
CSP A--013
MASTER
Head---up Guidance System --- Test Mode Selections
Figure 12---70---6 Sheet 4
SENSOR MENU
RAA
HGS
ANA
GPWS
SWITCH
>
Inertial Reference
System Units
Air Data
Computer Units
Integrated
Avionics
Processor
System
DME 1
Transceiver
VHF
Navigation
Receivers
Traffic Alert &
Collision Avoidance
System
Radio Altimeter
Units
Analog
Equipment
Ground
Proximity
Warning
System
Thrust Lever
Take--off /
Go--around
Switches
IRU/AHRS
ADC
IAPS
DME
VHF
TCAS
Sensor Menu Page
Used to gain access to HGS
data for corresponding airplane
system or equipment.
HGS Control Panel
Data Entry Readout
Runway elevation,
Glideslope angle.
Menu Page Selections:
BRT+ key used to move
　
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