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Inertial Reference System Units
Air Data Computer Units
IntegratedAvionics Processor System
DME 1
Transceiver
VHF
Navigation Receivers
Traffic Alert & Collision Avoidance System Sensor Menu Page
Used to gain access to HGS
data for correspondingairplane system or equipment.
SENSORMENU
IRU/AHRS ADC IAPS DME
Radio Altimeter Units
HGS Control Panel Data Entry Readout
Runway elevation, Glideslopeangle.
AnalogEquipment
ANA
GPWS
SWITCH
Ground ProximityWarning System
Thrust Lever Take-
off / Go-
around Switches
Menu Page Selections:
BRT+ key usedto move
cursor up, thenENTERkey used
toactivate selection.
DIM -
key usedto move
cursor down, thenENTERkey
usedto activate selection.
CLRkey usedto back out of
sub-
modes.
Head ---up Guidance System ---Test Mode Selections
Figure 12 ---70 ---6 Sheet 4
Flight Crew Operating Manual MASTER
CSP A-
013
FLIGHT INSTRUMENTS Head-
Up Guidance System Vol. 1 12-
70-
16
REV 56, Jan 31/03
Airplane Identification Page
Used to tagHGS computer
andallfault records with
airplanetail/ ident number.
New Airplane Tail or Ident Number Field
When ENTERNEW ID is selected, ELEV readout on HGS controlpanelwillindicate ID. Keypadis then usedto input 5-
digit number. ENTER is then usedto store number in memory.
Scrolling / Clear :
BRT+ key usedto move
cursor up,
DIM -
key usedto move
cursor down,
CLRkey usedto back out of sub-
modes.
Head ---up Guidance System ---Test Mode Selections
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