CABIN ALTITUDE or
Rapid Depressurization
Without delay, descend to the lowest safe
altitude or 10,000 feet, whichever is higher
Aborted Engine Start
FUEL CONTROL switch (affected side) . . . CUTOFF
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Motor engine for 30 sec
(when N2 decreases below 20%)
Dual Engine Failure
-FUEL CONTROL switches (both) . . . .
CUTOFF/RUN
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ENGINE FIRE
Severe Damage
Separation
-check fire. . . Rotate to the stop and hold for 1 sec
time start (30 seconds) . . Rotate to other bottle
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-APU selector . . . . . . . . . . . START, then ON
Airspeed Unreliable
Set the following gear up pitch attitude and thrust:
Engine Limit or Surge or Stall
-A/T ARM switch . . . . . . OFF
-Thrust lever (Confirm) . . . . . . . .Retard
(until engine indications stay within limits or the thrust lever is at idle)
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