T-45C TS, ADV & IUT ENG-19
Flight Instruments
(2) When pulled and turned clockwise into a
detent position, cages and locks the gyro
gimbals
(3) When pressed and rotated, adjusts the
aircraft symbol up to 50 (up or down)
NOTE: Do not cage the standby attitude
indicator within 30 seconds after power up
or press with excessive force or repeated
jabbing action.
NOTE: Do not cage and lock the standby
gyro with electric power ON and aircraft in
motion. The action will damage the gyro
b.
Solid color power OFF flag appears if power
supply fails or faults develop within instrument
c.
Bank index indicates roll in 10, 20, 30, 60, and
90 degree increments in both directions
4.
Subsystem interface: requires/receives 28 VDC
essential services bus power
NOTE: The two-inch standby AI provides a
minimum of 9 minutes attitude information after total
power failure.
C.
Standby turn and slip indicator
Sg 8, fr 5
Fig 10: Standby Turn
and Slip Indicator
1.
Location: upper left instrument panel, both cockpits
2.
Function: self-contained gyro driven rate of turn/slip
indicator, with a power warning flag
3.
Controls/switches/indicators
a.
Power off flag appears when power to the
instrument fails
Original (9-98)
Page 19-24
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