A320 hyd g+y sys lo pr summary

[Fixu]

Good afternoon dear colleagues

Anybody aware of the differences regarding G/A Thrust in the Dual HYD Summary?

several msn from my current outfit state
THR LVR : TOGA THEN MCT

others dont… cant find any explanation in our books.

any ideas or references?

thx
fixu

[vilas]

Originally Posted by Fixu

Good afternoon dear colleagues

Anybody aware of the differences regarding G/A Thrust in the Dual HYD Summary?

several msn from my current outfit state
THR LVR : TOGA THEN MCT

others dont… cant find any explanation in our books.

any ideas or references?

thx
fixu

what's given in QRH is the correct one. Only for aircraft fitted with soft GA it says TOGA and then MCT.

[Fixu]

Thanks Vilas 👍👍

[Fixu]

To my surprise the Soft Go Around is listed as not installed in the FCOM GEN AC CONFIGURATION SUMMARY and in the IF INSTALLED TABLE for the respective tails.

Thx

[lurkio]

I'm looking at a QRH for an aircraft not fitted with GA Soft and the summary still says TOGA then MCT.

[vilas]

Originally Posted by lurkio

I'm looking at a QRH for an aircraft not fitted with GA Soft and the summary still says TOGA then MCT.

Then there's something wrong with your QRH because I checked with not one three different aircraft. MCT only comes with OEI, with both engines operating it will flash a message THR LVR to climb because it's neither climb power not cruise thrust.

[BRAKES HOT]

My theory is that this is a NEO vs CEO thing, for control ability, or rather, not running out of control authority during the pitch up manouver. I have no references to back this up however. Does this pattern fit your fleet?

[vilas]

Originally Posted by BRAKES HOT

My theory is that this is a NEO vs CEO thing, for control ability, or rather, not running out of control authority during the pitch up manouver. I have no references to back this up however. Does this pattern fit your fleet?

No. even CEOs with soft go around function have the same write up. THR LVR TOGA then MCT.