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In a turn the up-going wing causes a
- de-stabilizing effect due to increased AoA.
- de-stabilizing effect due to decreased AoA.
- stabilizing effect due to decreased AoA.
Why the aoa decrease?
When resetting the CSD on the ground, the engine should be
- rotating at idle.
- stationary.
- rotating at Nsync.
but while connecting IDG the N2 should be rotating.
The CSD or IDG speed governor setting
- is not allowed to be adjusted.
- is adjusted with the engine stationary.
- is adjusted with the engine running.
b737 AMM:
E. Adjust the CSD Output Speed
SUBTASK 24-11-11-215-039-001
WARNING: MAKE SURE THE ENGINES ARE STOPPED WHEN YOU ADJUST THE CSD. THE
CSD ADJUSTMENT PUTS MAINTENANCE PERSONS IN THE DANGEROUS ZONE
THAT IS AROUND THE ENGINE INLET. ENGINE SUCTION CAN CAUSE INJURY TO
PERSONS.
(1) Make sure that the engine is stopped (PAGEBLOCK 71-00-00/201)...............
If the TAS of an aircraft increases, the CSU will
- increase the blade angle to provide constant RPM.
- decrease the blade angle to provide constant RPM.
- change the blade angle to provide constant RPM.
Why?
Which of the graphs shown is given by the equation y = x^2 + 3?

- a
- b
- c
can someone explain this to me