Electronic Engine Control Flashcards

1
Q

ENGINE CONTROL lights

A
  • engine control system is not dispatchable due to faults in the system
  • EEC through the CDS controls this light
  • DO NOT TAKEOFF with this light illuminated or inop
  • does not come on in flight
  • if the EEC detects a fault in-flight, no crew indication is provided
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2
Q

EEC switches

A

ON (white)
- indicates normal control mode is selected
ON (blank)
- EEC has been manually selected to alternate mode (hard alternate mode)
ALTN in view (amber)
- related EEC has automatically switched or manually selected to the alternate mode
- both ON and ALTN in view if the EEC has automatically switched to soft alternate mode

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3
Q

REVERSER lights

A
  • the engine accessory unit (EAU) controls this light
  • illuminates for 10 sec. during a normal T/R stow operation
  • extinguishes if the reverser sleeves are fully stowed and the isolation valve is closed
  • stays on if a T/R control system component fails during the stow
  • if the reverser light illuminates at any other time, a malfunction has occurred
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