SPYDER BOLDFACE EXPANDED

Reasons to use Emergency Engine Shutdown

Engine Fire

Engine Disintegration

Visible fluids leaking from engine or pylon area that cannot be stopped

Reasons to discharge agent during Emergency Engine Shutdown, Fire is:

Visible

Indicated

Suspected

WARNING: In min Q, use extreme caution when

applying rudder, structural damage can result from excessive rudder deflections at high speeds

WARNING: Excessive rudder TRIM with the rudder against the stops can result in

Extreme rudder deflection and possible rudder deflection and possible structural damage when the stops are removed.

WARNING: If engine fire is visible or indicated, it is imperative that

the associated hydraulic system be depressurized, to provide FULL isolation of pressurized fluids from the nacelle. The system must remain depressurized until fire is stopped and engine has cooled.On airplanes modified by TCTO-581 (Check Valve): Turn on the applicable PTU if there is no indication of the fire or hydraulic fluid loss. If landing gear extension or retraction is planned, turn on the applicable ATM when an outboard engine has failed, or fire is indicated and there is no indication of hydraulic fluid loss.On airplanes NOT modified by TCTO-581: If an engine fire was extinguished and the associated hydraulic system is intact, the associated PTU and/or ATM may be used for short periods to retract/extend landing gear or recharge emergency brake accumulator after the engine EGT stabilizes below 200C.