W DOC AIRBUS | AMM A320F

Removal of the Stage 1 Booster Vane Assembly [CFMI]


TASK 72-21-00-000-004-A
Removal of the Stage 1 Booster Vane Assembly


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)
856A1130
1
TOOL SET - JACK SCREW
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 72-21-00-000-001-A
Removal of the Spinner Front Cone
TASK 72-21-00-000-002-A
Removal of the Spinner Rear Cone
TASK 72-21-00-000-003-A
Removal of the Fan Rotor Blades
TASK 72-23-00-000-007-A
Removal of the Splitter Fairing
3. Job Set-up
Subtask 72-21-00-941-063-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).
4. Procedure
Subtask 72-21-00-010-050-A ** ON A/C NOT FOR ALL
A. Preparation for Removal of the Stage 1 Booster Vane Assembly.
   (1) Remove the spinner front cone (Ref. AMM TASK 72-21-00-000-001).
   (2) Remove the spinner rear cone (Ref. AMM TASK 72-21-00-000-002).
   (3) Remove all the fan blades (Ref. AMM TASK 72-21-00-000-003).
   (4) Remove the splitter fairing (Ref. AMM TASK 72-23-00-000-007).
Subtask 72-21-00-020-051-A ** ON A/C NOT FOR ALL
B. Removal of the Stage 1 Booster Vane Assembly.
   (1) Remove the 24 bolts that secure the stage 1 vane assembly to the stage 2 vane assembly.
   (2) Move apart stage 1 vane assembly from the stage 2 vane assembly, using jackscrews, P13, from the 856A1130 TOOL SET - JACK SCREW, on the equally spaced threaded holes located on the rear flange of the stage 1 vane assembly.
[Rev.10 from 2021] 2026.04.02 06:33:39 UTC