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SECTION  I. EQUIPMENT DESCRIPTION AND DATA
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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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Figure   7–1. Primary Hydraulic System Major Component Location

TM 1-1520-238-T-5 Change 6 7–3 7–2. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (cont) 7–2 (4)   Primary GSE Panel. The primary GSE panel, located on the aft equipment bay deck outboard of the utility manifold, provides connections for external hydraulic application and for servicing the primary and utility reservoirs with fluid. The fluid is filtered by a 45 micron screen filter (ADF) or a 5 micron cartridge filter element (ADG). (5)   Longitudinal Servocylinder. The longitudinal servocylinder, located on the left transmission deck in front and to the right of the main transmission, converts mechanical inputs during normal operation, or electrical inputs during digital automatic stabilization equipment backup control system (DASE BUCS) operation, into hydraulic pressure outputs which are sent to the main rotor swashplate. (6)   Lateral Servocylinder. The lateral servocylinder, located on the transmission deck in front and to the left of the main transmission, converts mechanical inputs during normal operation, or electrical inputs during DASE BUCS operation, into hydraulic pressure outputs which are sent to the main rotor swashplate. (7)   Collective Servocylinder. The collective servocylinder, located on the transmission deck in front of the main transmission, converts mechanical inputs during normal operation, or electrical inputs during DASE BUCS operation, into hydraulic pressure outputs which are sent to the main rotor swashplate. (8)   Directional Servocylinder. The directional servocylinder, located on the top of the tail rotor gearbox, converts mechanical inputs during normal operation, or electrical inputs during DASE BUCS operation, into hydraulic pressure outputs which are sent to the tail rotor swashplate.

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