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Flight Deck Photos and/or Graphic Representation
ENG Mode Selector
NORM - Continuous ignition A + B is selected when the engine is running and one of the following is met:
FLEX or TO/GA thrust is selected on the ground
TO/GA thrust is selected in flight
ENG ANTI ICE switch is ON
Engine surge or stall occurs in flight
FLAPS lever position is other then "0" in flight
CRANK - The start valve opens provided the ENG MAN START switch is ON and N2 is less than 10%. Ignition is not supplied.
IGN / START - Provides continuous ignition if the ENG MASTER switch is ON and N2 is at idle or greater.
During and automatic start, on airplanes placarded :EXTENDED DRY CRANK", expect ignition and fuel flow 50 seconds
after ENG MASTER switch is selected ON.
On airplanes without the placard, expect ignition and fuel flow between approximately 15% and 20% N2.
During a manual start the HP fuel valve is open and ignition is selected when the ENG MASTER switch is selected ON.
ENG MASTER Switches 1 & 2
ON - LP fuel valve opens, provided the ENG FIRE switch is in. During and automatic start, the HP fuel valve opens,
provided the ENG MODE selector is at IGN/START.
During a manual start, the HP fuel valve opens, provided the ENG MODE selector is at IGN/START and the ENG MAN START switch is ON.
OFF - Closes the HP and LP fuel valves. Resets both channels of the FADEC.
FIRE / FAULT Lights
FIRE Light (Top) - Illuminates when the respective fire warning is activated and during engine fire test.
FAULT Light (Bottom) - Illuminates Amber in the event of an automatic start abort, or a disagreement between the
HP fuel valve position of FADEC channel A and B.