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AVIONICS FLIGHT CHECKS-continued - TM-1-1510-223-MTF0133
Up
TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
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Inertial navigation system
TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
(1) Fly aircraft to test altitude.
(2) ALT switch-indicator (flight director mode
selector) - Press on.
(3) Verify that the aircraft maintains the
altitude being flown at the time the ALT
hold switch was pressed.
i.
Check  autopilot  indicated
airspeed
hold
function as follows:
(1) Fly aircraft to test airspeed.
(2) IAS switch-indicator (flight director mode
selector) - Press on.
(3) Aircraft should maintain airspeed that was
being flown at the time IAS hold switch
was pressed.
j.
Check roll command function of autopilot as
follows:
(1) TURN control knob (autopilot controller) -
Turn to L and R and verify that autopilot
turns aircraft left or right respectively.
* 2. Slaved compass systems - Check that systems
agree with known magnetic headings
within ±2°and within 3°of each other.
* 3. Inertial Navigation System Flight Test - Perform as
follows:
Demonstrate satisfactory performance by flying over
three known checkpoints, and comparing the inertial
present position readouts with the coordinates of the
checkpoints. Establish a
4-9

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