Instrument Failures and GPS/INS Failures
T-45C TS & ADV BIFP-09; IUT BIFP-05
2.
Place most appropriate display on
Sg 2, fr 4
remaining MFD and use standby
instruments
STBYSTABTRIM
RUDDERTRIM
NOSEDN
CONTRAUG
R
ALL
L
NOSEUP
RESET
SBI
DISPLAY
FUELCONTR
3.
If momentary loss of all MFDs is
POWER
ENGINE
NORMAL
START
RESET NORM
ORIDE
ON
acceptable, cycle the DISPLAY POWER
MANUAL
OFF
switch to RESET
DISPLAY POWER SWITCH
C. Total (all four) MFD failure
Sg 2, fr 5
1.
Most likely DEU malfunction
2.
Cycle the DISPLAY POWER switch to
RESET
3.
Use standby instruments
4.
All navigation information lost
5.
Only PAR or ASR instrument approach
DEU FAILURE
possible
Sg 2, fr 6
D. Blank, missing, incorrect MFD data
1.
Invalid data is removed from display by
DEU
2.
Incorrect data may be result of input data to
NORMAL ADI AND HSI DISPLAYS
DEU or instructor initiating failure with
training mode
Sg 2, fr 7
SELECTED FAILURE OPTION
COCKPIT IMPACT
VOR
All VOR dataremoved from HSI andHUD
ILS
All ILS dataremoved from HSI, ADI, and HUD
TCN
All TACAN data removed from HSI and HUD
All attitudeand navigationinformation removedfrom HSI, ADI, and
GINA
HUD
True airspeed, Barometric Altitude, Mach Number, and wind direction
SADS
and speed removed from displays
LMFD
Opposite cockpitleft MFD blank
Opposite cockpitrightMFD blank
RMFD
HUD display blank
HUD
ADI attitude frozen
ADI FRZ
ADI and HSI heading frozen
HSI FRZ
TRAINING MODE––FAILURE
IMPLICATIONS
Page 9-8
(4-01) Original
Previous Page
