W DOC AIRBUS | AMM A320F

Removal of the Stage 1 Booster Vane Assembly [CFMB]


TASK 72-21-00-000-008-A
Removal of the Stage 1 Booster Vane Assembly


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
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 72-21-00-000-005-A
Removal of the Spinner Front Cone
TASK 72-21-00-000-006-A
Removal of the Spinner Rear Cone
TASK 72-21-00-000-007-A
Removal of the Fan Rotor Blades
TASK 72-23-00-000-028-A
Removal of the Splitter Fairing
3. Job Set-up
Subtask 72-21-00-941-070-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 72-21-00-020-071-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 72-21-00-000-005).
   (2) Remove the spinner rear cone (Ref. AMM TASK 72-21-00-000-006).
   (3) Remove all the fan blades (Ref. AMM TASK 72-21-00-000-007).
   (4) Remove the splitter fairing (Ref. AMM TASK 72-23-00-000-028).
Subtask 72-21-00-020-066-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 booster vane assembly to the stage 2 booster vane assembly.
   (2) Move apart the stage 1 booster vane assembly from the stage 2 booster vane assembly, using jackscrews, P13, from the 856A1130 TOOL SET - JACK SCREW (856A1130G02/G06/G10), on the equally spaced threaded holes located on the rear flange of the stage 1 booster vane assembly.
[Rev.10 from 2021] 2026.04.01 12:59:45 UTC