W DOC AIRBUS | AMM A320F

Repairs of the Combustion Case Assembly [CFMB]


TASK 72-41-00-300-002-A
Repairs of the Combustion Case 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
ABRASIVE STONE
No specific
AR
ACCESS PLATFORM 1M(3 FT)
No specific
AR
FILE - FINE
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2189)
durite G422
(Material No.CP2191)
durite G421
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 70-51-00-230-002-A
Fluorescent-Penetrant Inspection-Portable-Water Washable
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-B
Closing of the Fan Cowl Doors
TASK 78-30-00-081-041-B
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-B
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-B
Closing of the Thrust Reverser Doors
3. Job Set-up
Subtask 72-41-00-941-053-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 72-41-00-010-055-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
   (2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (4) Put the ACCESS PLATFORM 1M(3 FT) in position.
Subtask 72-41-00-040-053-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 72-41-00-010-057-A ** ON A/C NOT FOR ALL
D. Open the thrust reverser doors: (Ref. AMM TASK 78-36-00-010-040)
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure
Subtask 72-41-00-350-051-A ** ON A/C NOT FOR ALL
A. Blend the part
CAUTION: DO NOT PERMIT THE REMOVED MATERIAL, TOOLS, OR CONSUMABLES TO FALL INTO THE COMBUSTION CASE. ENGINE DAMAGE CAN OCCUR.
   (1) Blend the part with a FILE - FINE, durite G422 (Material No.CP2189) or durite G421 (Material No.CP2191) or ABRASIVE STONE. Remove as small an amount of the parent metal as possible.
Subtask 72-41-00-230-053-A ** ON A/C NOT FOR ALL
B. Do a fluorescent penetrant inspection of all the blend areas. No cracks are permitted. (Ref. AMM TASK 70-51-00-230-002)
5. Close-up
Subtask 72-41-00-410-055-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the thrust reverser doors: (Ref. AMM TASK 78-36-00-410-040).
   (3) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (4) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 72-41-00-440-053-A ** ON A/C NOT FOR ALL
B. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 72-41-00-410-057-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors: (Ref. AMM TASK 71-13-00-410-040)
   (2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (4) Remove the access platform(s).
   (5) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:42:36 UTC