Instrument Failures and GPS/INS Failures
T-45C TS & ADV BIFP-09; IUT BIFP-05
3.
AV BIT and GINA degraded on BIT display
4.
Use standby VSI
5.
Altitude display more sensitive, refer to
standby altimeter
D. Erroneous GINA data
Sg 1, fr 8
1.
Erroneous GINA velocity data may be
displayed with no failure indication
2.
Cross-check standby instruments
D
N
OFF
3.
Cross-check wind, ground speed, ground
FORECAST WINDS 175 AT 05 KNOTS
track marker, ghost velocity vector with
ERRONEOUS GINA DATA
forecast winds
II.
MFD failure
Sg 2, fr 2
INSTRUMENT FAILURES
A. Single MFD failure
* GINA failure
* Standby attitude indicator
failure
*
MFD failure
* AOA indicator failure
1.
Turn MFD CONT and BRT knobs full
*
HSI failure
* Radar altimeter failure
*
ADI failure
* VOR failure
clockwise
*
Turn and slip
* TACAN bearing/DME
indicator failure
failure
*
Pitot static
* ILS glideslope failure
malfunctions
2.
Raster scan visible MFD electronically
*
Airspeed indicator * ILS localizer failure
failure
functional
*
Barometric
* ILS marker beacon failure
altimeter failure
*
Vertical speed
* Flight with partial panel
indication failure
3.
No raster scan MFD failed
Sg 2, fr 3
4.
Place most appropriate display on
remaining MFD and use standby
instruments
5.
If momentary loss of all MFDs is
acceptable, cycle the DISPLAY POWER
switch to RESET
B. Right or left (both cockpits) MFD failure
1.
SINGLE MFD FAILURE
(4-01) Original
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