DB's SY 737 Engine Flashcards
ENGINE START switches - OFF
- Normal position
- Both igniters are activated when Start Levers in IDLE and:
• Uncommanded rapid decrease in N2 or
• N2 is 50%-57%
• In flight - N2 is between idle and 5%
Engine Start Switches - GRD
- Opens start valve
- Closes engine bleed valve
- Ground Starts - Arms selected igniter (when start lever moved to IDLE)
- Air Starts - Arms both igniters (when start lever moved to IDLE)
- Releases to OFF at start valve cutout (56%)
ENGINE START switch - CONT
- Provides ignition to selected igniters (with engine on and start levers in IDLE)
- In flight - Provides ignition to both igniters when N2 is below idle with start lever in IDLE.
ENGINE START Switches - FLT
Both igniters activated (when start lever in IDLE)
REVERSER lights - ON
One or more of the following:
- Isolation valve or thrust reverser control valve is not in commanded position
- At least one thrust reverser sleeve not in commanded state
- Auto-restow circuit has been activated
- Synchro shaft lock circuitry failed
ENGINE CONTROL lights - ON
Non-dispatchable fault in the Engine Control system
When are the ENGINE CONTROL lights active?
- Engine is operating and
- Airplane is on the ground and
• Below 80 prior to takeoff or
• 30 secs after touchdown
EEC Switches - lights illuminated
- ON only
- ALTN and ON
- ALTN only
- Normal control mode
- EEC automatically in (soft) alternative mode or manually in hard alt mode by retarding thrust levers idle (not by pressing EEC switch)
- EEC manually selected to (hard) alternate mode by pressing EEC switch
What type of engines are installed?
CFM56-7B
What does soft alternate mode on the EEC do for us?
The EEC uses the last valid fight conditions to define engine parameters which allows the mode change to occur with no immediate change in engine thrust.
What does hard alternate mode in the EEC do for us?
The EEC reverts to alternate mode (factory presets) thrust schedule. Hard alternate mode thrust is always equal to or greater than normal mode thrust for the same lever position.
How does a loss of either DEU affect our engines?
Loss of either DEU results in a loss of signal to both EECs, which reverts both EECs to alternate mode to prevent the engines from operating on a single source of data.
How does the EEC actually control the speed of the engine?
The EEC compares commanded N1 to actual N1 and adjusts fuel through the HMU to achieve the commanded N1.
At what N2 speed does the starter normally cutout?
56%
During an engine start, what does a flashing white box around the EGT indicate?
Impending hot start or a compressor stall has occurred