A320 Avionic cooling logic
Hi all
Regarding Avionic cooling on A320 fleet
The FCOMS says
CLOSED CONFIGURATION (Flight and ground)
Flight phase
The threshold is
+35c and increasing
+32c and decreasing
Ground phase
The threshold is
+12c and increasing
+9c and decreasing
INTERMEDIATE CONFIGURATION (Inflight only)
The threshold is
+35c and increasing
+32c and decreasing
OPEN CONFIGURATION (On ground only)
The threshold is
+12c and increasing
+9c and decreasing
I do understand that the 3 degrees split is for the computer not to go crazy.
I am trying to visualize the above logic, any idea to simplify this ?
Highly appreciate your knowledge sharing.
Last edited by b767300; 24th Jun 2014 at 07:17.