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W AOAsymbolcomes on whenthe airplane is within 2degrees ofstick shaker.
(20) FlightDirectorGuidance Cue, The guidance cue representslateraland verticalattitude commands requiredfor the selectedlow visibilityapproachandlanding:
W DuringCategory I or II operations, displayeduntil80feetAGL,and
W DuringCategory IIIaoperations, displayeduntiltouchdown
W AnF/Dflagis usedto indicateflightdirector failure.
(21)
FlightModeAnnunciations, Lateral armed/ capturedand vertical mode annunciations are provided. Autopilot statusindications andmistrimindications (aileron,elevatorand rudder)are provided.
(22)
Autopilot,Yaw Damper&Mistrim Indications, Ayaw damper messageis providedtoindicatethattheyaw damperis disengaged. Mistrimflags(elevator, aileron andruddertrims)are providedto indicateout-
of-
trim conditions.
NOTE
HGSentryoflanding runwayelevation isto bemade prior to anytypeoflanding usingthe HGS.
Flight Crew Operating Manual MASTER
CSP A-
013
Vol. 1
12-
70-
6
FLIGHT INSTRUMENTS
REV56,Jan 31/03
Head-
Up Guidance System
OVERHEAD PANEL
ACT 1 2 3
H G S STBY ELV HGS 4 7 5 8 6 9
G/S
ENTER 0 TEST
FAULT CLR BRT+ DIM -
Combiner Brightness Control
Used to adjust brightness
of holographic image.
Push in for automatic
control.
Pull out and rotate
clockwise for manual
control.
HGS SystemFigure 12 ---70 ---1
Flight Crew Operating Manual MASTER CSP A-
013 Vol. 1
12-
70-
7
FLIGHT INSTRUMENTS
Head-
Up Guidance System REV 56, Jan 31/03
T
URB
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