T-45C TS, ADV, & IUT CO-02
Engine Start and Poststart
1.
The initial selection of DATA formats will
default to the waypoint data format,
subsequent selections of DATA will return
to the last selected sub-level data format
2.
System alignment begins when the
batteries are turned on and alignment is
normally completed within four minutes. So
the system should be aligned by the time
you call up the aircraft display during the
poststart checks
3.
The legends on aircraft data page: ALGN
is the elapsed alignment time. QUAL in the
alignment quality in km per hour [the
minimum QUAL number is 00.59] GPS SAT
is the number of satellites tracked by the
system
D. NATOPS step 12. Stabilator trim - CHECK
BOTH DIRECTIONS: The stabilator trim
indicator will only depict trim position with no
forces on the stick. While checking or setting
the trim for takeoff or catapult launch, it is
important that both pilots not exert longitudinal
forces on the stick
E. NATOPS step 14. Standby attitude indicator -
PULL TO ERECT: Power should be applied for
at least one minute before caging the standby
attitude indicator (AI) Pulling the caging knob,
cages the indicator. Rotating the knob adjusts
the pitch of the miniature aircraft. Pulling the
caging knob and rotating it clockwise locks the
gyro. Don't lock the standby gyro during flight
F. NATOPS step 18. BIT display - NOTE DEGD:
(IFF, YDS and VCR will display DEGD if they
are set to OFF or are in standby)
The possible BIT legends are:
1.
GO - proper system operating and dual
1553 bus communications
(10-99) Original
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