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Page Title: Table 7–1. Hydraulic and Pneumatic Systems Controls and Indicators (cont)
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Pilot TAIL WHEEL Lock Panel
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TM-1-1520-238-T-5 Army Model AH-64 Helicopter (NSN 1520-01-106-9519) (EIC: RHA) Manual
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Pilot Emergency Hydraulic Pressure Indicator

TM 1-1520-238-T-5 7–18 7–6. CONTROLS AND INDICATORS (cont) 7–6 Table   7–1. Hydraulic and Pneumatic Systems Controls and Indicators (cont) Pilot Power Quadrant SWITCH/INDICATOR POSITION FUNCTION RTR BK toggle switch OFF Releases rotor brake hydraulic pressure. BRAKE Applies utility system pressure regulated to 337 psi to stop rotor brake disc on main transmission. LOCK Locks rotor brake by trapping 3000 psi pressure between manifold and rotor brake actuator. M68-148 RTR  BK  SWITCH Pilot Power Quadrant

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