PILOT ENGINE CONTROL PANEL

Governor Switches : The pilot or gunner GOV switches AUTO position, permits the overspeed governor to automatically control fuel metering and engine speeds ( N1 and N2 ). The EMER position permits the pilot and gunner to manually control the engine rpm. The governor circuit is powered by the dc essential bus and protected by the GOV CONTR circuit breaker.
Fuel Switch : The pilot FUEL switch,  FUEL position energizes the forward and aft boost pumps, opens the fuel shutoff valve, and completes the ignition and start fuel circuit. The aft fuel boost pump circuit is powered by the dc essential bus. The other circuits are protected by the START RLY, IGN SOL, FUEL/OIL VALVE, FUEL BOOST FWD, and FUEL BOOST AFT circuit breakers.
Engine Oil Bypass Switch : The pilot ENG OIL BYP switch, AUTO position permits the oil to automatically bypass the oil cooler when the oil tank is approximately 3.8 quarts low. The OFF position deactivates the automatic bypass feature causing the oil to pass through the oil cooler regardless of the oil tank level. The switch circuit is powered by the dc essential bus and protected by the FUEL OIL VALVE circuit breaker.
Engine Deice : The pilot ENG DEICE switch is placed in the DEICE position. This action causes the hot air solenoid valve to route engine bleed air to the engine air inlet.  A rise in the turbine gas temperature (TGT) will occur when the pilot or gunner ENG DEICE switch is in the DEICE position.  De-ice operation will become continuous if the hot air solenoid valve (ENG DEICE) circuit fails or if ENG DEICE circuit breaker is out (extended).
RPM Warning Switch : The pilot RPM switch, OFF position prevents audio warning from functioning for engine starting when the audio might be objectionable. The switch automatically resets to WARNING position when the engine and rotor reach normal rpm.
Hydraulic Test Switch : The pilot HYD TEST switch is used to test the No.1 and No.2 hydraulic systems. Holding the switch in the SYS 1 position will cause the No.1 system to be the only system supplying hydraulic pressure. Similar action occurs when the switch is held in the SYS 2 position.
Force Trim Switch : Placing the FORCE TRIM switch in the FORCE TRIM position will induce artificial feel into the systems. Depressing the cyclic stick force trim switch will cause the magnetic brake and force gradient to be repositioned to correspond to the positions of the cyclic stick and pedals thus providing trim. The system is powered by the dc essential bus and protected by the FORCE TRIM circuit breaker.

 

Return to The Cockpit ( Pilots Station )
Return to Attack Helicopter Home Page