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Page Title: Shaft Driven Compressor (SDC)
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Section  VII. POWER TRAIN SYSTEM

TM 1-1520-238-10 Change 9 2-55 2.39.1   Shaft Driven Compressor (SDC). The SDC is mounted on the main transmission accessory case and uses outside air. The air passes through a particle separa- tor and then through a butterfly-type throttle valve. This valve is closed by a time-delay solenoid when the APU START switch is engaged. The valve remains closed for 60 seconds after the APU START switch is released. The purpose of the time-delay solenoid is to reduce starting loads on the APU during external power starts. It is not ac- tivated during a battery start. The shaft driven compressor will compress air at 3:1 ratio and route it through a surge valve. This valve, mounted on top of the SDC, will open or close  as  necessary  to  keep  SDC  air  pressure  constant with  variable  system  demand.  Pressurized  air  then passes  through  a  spring-operated  check  valve  and  into the PAS manifold. This check valve prevents pressurized air, from sources other than the SDC, from reverse routing back to the SDC. The SDC is lubricated by the main trans- mission accessory oil pump and has its own scavenge. If the SDC oil temperature exceeds 182 °C (360 °F), or if the SDC fails, the pilot SHAFT DRIVEN COMP caution light illuminates. 2.39.2   No. 1 Engine Bleed Air. The No. 1 engine pro- vides an alternative source of pressurized air in case of SDC  failure.  The  engine  compressor  bleed  air  selector valve opens automatically if SDC output falls below 10 psi. Simultaneously,  a  spring-operated  check  valve  opens. When closed, this valve prevents pressurized air from go- ing to the engine compressor when the SDC is operating. Each engine provides bleed air to its engine inlet to pre- vent ice formation and to keep the engine cooling louvers closed while the engine is operating. The bleed air used in these last two instances is independent of the pressurized air system. 2.39.3   External Air Source Receptacles. The recep- tacle for external air source connection (fig 2-46) is on the lower portion of No. 1 engine nacelle. When the air source is  connected  and  operating,  a  normally  closed  check valve to the pressurized air system opens to allow air to pressurize the manifold.

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