INS STORED HEADING ALIGNMENT

MISSION CONTROL PANEL SWITCHES (BE- FORE TAXIING)

OVERSPEED GOVERNORS AND RUDDER BOOST - TM-1-1510-223-CL_65

TM-1-1510-223-CL Army Model RC-12 Manual
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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.

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