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Home > Aviation Maintenance and Training Volume 2 > > HUD Failures
Velocity vectors
Figure 1. Display System Component Locations

Operational Navigation Flight Procedures - index
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T-45C TS, ADV & IUT ONFP-01
Low Level Waypoint Navigation
4.
Above 5,000 ft AGL or id invalid signal received numbers
removed, but "R" remains
Fig 6: Failure
Indications of HUD
5.
Radar altimeter power controlled on the MFD BIT display
Display
III.
HUD Failures
A.
Indications 4.4.5.4.3
1.
At power-up and test
a.
Blank screen after twenty seconds
b.
DEGD BIT status reported on BIT display
2.
In flight
a.
One or more indications missing from display
b.
Blank screen
c.
DEGD BIT status reported on BIT display
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(4-03) Original






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