Rigging of slats
 

Hi guys,

I was trying to look up the AMM for the rigging of slats for A320 but I can't seem to find the specific chapter. Can anyone kindly point me in the right direction?

Thanks in advance!

I'm not rated on any Airbus but think if you go to the back end of AMM27, look for slat removal/installation, then follow the closeout which would include adjustment/rigging & the required function/op checks TBCO.

Is this for a college project?

BAe

Take a look at the end of the installation section for each specific slat

ie 27-84-63-400-002 for No 1 slat :ok:

for slat 1 : AMM 27-84-63-820-055
for slat 2 : -64-
for slat 3 : -65-
and so on ...
bon courage.

Thanks everyone! Exactly what I'm looking for. :ok:

Cheers!