TM 1-1510-223-CL
P-23
INS STORED HEADING ALIGNMENT
NOTE
Perform only if a stored heading shutdown
was completed and the aircraft has not
been moved. Only one stored heading
alignment can be done between full align-
ments.
1.
#1 and #2 3Ø inverters – RESET/ON.
2.
BUS CROSS TIE switch – AUTO.
3.
INS mode switch – NAV.
4.
INS SETUP page – Enter alignment coordi-
nates.
5.
After reaching align state zero select auto-
mixing mode.
MISSION CONTROL PANEL SWITCHES (EN-
GINE RUNUP)
After receiving clearance from IPF, set as instructed:
1.
ANT SEL – As required.
2.
ANT STEERING – As required.
3.
DATA LINK HV switch – ON.
4.
Mission equipment caution/advisory annun-
ciator panel – Check for no power fault lights.
5.
ANT SEL and ANT STEERING switches –
AUTO.
AUTOFEATHER/AUTO IGNITION
1.
AUTO IGNITION switches – ARM.
2.
POWER levers – Approximately 25% torque.
