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Page Title: Figure 4–3. Engine Anti–Ice Subsystem
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4–2. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (cont)
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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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(2)   Engine Anti–Ice Subsystem

TM 1-1520-238-T-4 4–4 4–2. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (cont) 4–2 (d)   Cooling Doors. The cooling doors are movable vane type doors that open when the engines are shutdown. They are located at the bottom on both the right and left hand nacelles. (e)   Cooling Door Actuator. The cooling door actuator, a pneumatic piston with an internal spring, opens and closes the cooling door. (f)   Fixed Louvers. The fixed louvers are fixed air scoops that are angled forward with a honeycomb filter in the vents. NGB  FAIRING (HEATER  BLANKET  IN  FAIRING) BLEED  AIR  TUBE ANTI-ICE  VALVE SWITCH THERMOSTATIC BLEED  AIR  TUBE M58-069 Figure   4–3. Engine Anti–Ice Subsystem

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