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Page Title: Table 3–1. Landing Gear System Controls and Indicators
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3–3. EQUIPMENT DATA
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TM-1-1520-238-T-4 Army Model AH-64 Helicopter (NSN 1520-01-106-9519) (EIC: RHA) Manual
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SECTION  II. THEORY OF OPERATION

TM 1-1520-238-T-4 3–13 3–6. CONTROLS AND INDICATORS 3–6 The landing gear system receives mode selects and remote switch inputs from various controls located in the pilot station (fig. 3–12). Table 3–1 provides a listing of the controls, switches and associated indicators pertaining to the landing gear system along with a description of their function. M58-192A 1. PILOT  TAIL  WHEEL  PANEL 1 Figure  3–12. Pilot Station Table   3–1. Landing Gear System Controls and Indicators Pilot TAIL WHEEL Panel SWITCH/INDICATOR POSITION FUNCTION TAIL WHEEL UNLOCK/ LOCK 2–position switch UNLOCK Energizes electrical circuit to control tail wheel lock solenoid. UNLOCK De–energizes solenoid in tail wheel lock circuit. Advisory Light GREEN Lights when TAIL WHEEL switch is set to UNLOCK.

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