Originally Posted by
compressor stall
....just the above post seemed to imply an alpha that would trigger it. The article is ambiguously worded. I don’t remember that in the GS logic diagram but I don’t know everything and always curious...
There may be confusion with some of the words in FCOM regarding Ground Spoiler logic.
The 2.5 degree condition applies when "
Speed brake lever in the retracted position but ground spoilers not armed and:"
"Ground Spoiler Control..
FULL EXTENSION - LANDING PHASE
The ground spoilers will automatically extend when the following conditions are met:- Speed brake lever not in the retracted position or ground spoilers armed and:
- Both main landing gears on ground,
- Both thrust levers at or below Idle position, or Reverse selected on at least one engine (and the other thrust lever below MCT position).
- Speed brake lever in the retracted position but ground spoilers not armed and:
- Both main landing gears on ground,
- Reverse selected on at least one engine (and the other thrust lever below MCTposition).
The ailerons are fully-extended (Aileron Anti Droop@ ), provided one aileron servocontrol is available on each side, when:- The ground spoilers are fully extended
- Flaps are not in clean CONF
- Pitch attitude is lower than 2.5 °
- Flying manually
- In normal law only."