Instrument Failures and GPS/INS Failures
T-45C TS & ADV BIFP-09; IUT BIFP-05
PROGRESS CHECK
Question 3 — 1.8.1.7.1.2
What is the most vital step in the ADI failure
procedure?
a) Use the standby attitude indicator and maintain
aircraft control.
b) Reset the ADI erect switch.
c) Watch for possible progressive failure.
d) Check the electrical system.
Answer: a
Question 4 —1.8.1.7.10.2
Which of the following steps apply when the turn
and slip indicator fails?
a) Use the ADI bank indices for rudder trim reference.
b) Use the angle-of-bank and airspeed for turn rate
reference.
c) Check the ADI for correct indications.
d) Be aware of possible electrical problems.
Answer: b
VI. Pitot static malfunctions 1.8.1.7.3.2
Sg 6, fr 2
INSTRUMENT FAILURES
A. Pitot static system malfunction affects all
* GINA failure
* Standby attitude indicator
primary and standby driven indications:
failure
*
MFD failure
* AOA indicator failure
*
HSI failure
* Radar altimeter failure
*
ADI failure
* VOR failure
1.
Airspeed, TAS, Mach
*
Turn and slip
* TACAN bearing/DME
indicator failure
failure
*
Pitot static
* ILS glideslope failure
malfunctions
2.
Barometric altitude
*
Airspeed indicator * ILS localizer failure
failure
*
Barometric
* ILS marker beacon failure
altimeter failure
3.
Standby VSI (vertical speed on ADI is
*
Vertical speed
* Flight with partial panel
indication failure
generated by GINA accelerometer)
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