W DOC AIRBUS | AMM A320F

Removal of the Centerbody [CFMI]


TASK 78-11-12-000-040-A
Removal of the Centerbody


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 72-56-00-210-001-A
Inspection/Check of the Turbine Frame Assembly
TASK 78-11-11-000-040-A
Removal of the Core Nozzle Assembly
3. Job Set-up
Subtask 78-11-12-941-054-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 78-11-12-010-053-A ** ON A/C NOT FOR ALL
B. Remove the core nozzle (Ref. AMM TASK 78-11-11-000-040).
4. Procedure
Subtask 78-11-12-020-052-A ** ON A/C NOT FOR ALL
A. Removal of the Centerbody
   (1) Remove nuts (10) and washers (15) attaching centerbody to engine. Discard nuts.
NOTE: If any anomaly occurs when removing nuts (loosing or broken stud), (Ref. AMM TASK 72-56-00-210-001) for serviceability or repair.
   (2) Remove centerbody (30) from engine.
[Rev.10 from 2021] 2026.04.01 12:59:05 UTC