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Page Title: Figure 4–7. Engine Power Controls
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(6)   Engine Power Controls
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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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Figure   4–8. Engine Indicator Controllers

TM 1-1520-238-T-4 4–8 4–2. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (cont) 4–2 (d)   Grip Control Collar. A grip control (CHOP) collar switch is installed inside the chop collars on the pilot and CPG collective sticks. The CHOP collar is spring–loaded in the aft position. (e)   Turbine Speed Control Unit. The turbine speed control unit is located at the forward outboard side of the aft avionics bay. This unit has a rpm adjustment screw, an electrical connector, and two internal potentiometers (one for each engine). M58-079 LOAD  DEMAND  SPINDLE  (LDS) (INPUTS  FROM  COLLECTIVE SERVOCYLINDER  OF HYDRAULIC  SYSTEM) CONTROL  CABLE SPINDLE  GEARBOX RPM ADJUSTMENT INCREASE DECREASE HYDRO-MECHANICAL UNIT  (HMU) GRIP  CONTROL  COLLAR HMU  SHAFT TURBINE   SPEED   CONTROL POWER  AVAILABLE  SPINDLE  (PAS) (INPUTS  FROM  PILOT  AND CPG  POWER  LEVERS) COLLECTIVE   STICK Figure   4–7. Engine Power Controls (7)   Engine Indicator Controllers. The major components of the engine indicator controllers (fig. 4–8) are the fuel pressure switch and the oil pressure transmitter. (a)   Fuel Pressure Switch. Fuel pressure switch is an electro–mechanical device that monitors low engine fuel pressure. (b)   Oil Pressure Transmitter. The oil pressure transmitter is an electro–mechanical device.

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