W DOC AIRBUS | AMM A320F

Blending of the Stage 1 Booster Vane Assembly [CFMB]


TASK 72-21-00-320-004-A
Blending 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
ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE
No specific
AR
FILE - SMOOTH
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2189)
durite G422
(Material No.CP2191)
durite G421
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 70-51-00-230-002-A
Fluorescent-Penetrant Inspection-Portable-Water Washable
TASK 72-21-00-000-007-A
Removal of the Fan Rotor Blades
TASK 72-21-00-400-007-A
Installation of the Fan Rotor Blades
3. Job Set-up
Subtask 72-21-00-941-076-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) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position.
4. Procedure
Subtask 72-21-00-020-074-A ** ON A/C NOT FOR ALL
A. Remove the Fan rotor blades (Ref. AMM TASK 72-21-00-000-007).
Subtask 72-21-00-220-055-A ** ON A/C NOT FOR ALL
B. Check for dimensions and location of defects on edge and compare with repair limits.
Subtask 72-21-00-320-053-A ** ON A/C NOT FOR ALL
C. Perform blending of defects using a FILE - SMOOTH or strips of durite G422 (Material No.CP2189) or durite G421 (Material No.CP2191) , used dry.
   (1) Remove a minimum of 0.01 in. (0.25 mm) of base metal in addition to depth of defect.
Subtask 72-21-00-230-053-A ** ON A/C NOT FOR ALL
D. Fluorescent penetrant inspect reworked area (Ref. AMM TASK 70-51-00-230-002). No crack is allowed.
5. Close-up
Subtask 72-21-00-420-078-A ** ON A/C NOT FOR ALL
A. Install the fan rotor blades (Ref. AMM TASK 72-21-00-400-007).
Subtask 72-21-00-869-071-A ** ON A/C NOT FOR ALL
B. Make sure that the work area is clean and clear of tools and other items.
Subtask 72-21-00-942-070-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Remove the access platform(s).
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 12:59:45 UTC