W DOC AIRBUS | AMM A320F

Visual Inspection of the Low Pressure Compressor (LPC) Cover [CFML]


TASK 72-21-22-200-801-A
Visual Inspection of the Low Pressure Compressor (LPC) Cover


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
1. Reason for the Job
This procedure gives criteria for visual inspection of the Low Pressure Compressor (LPC) cover.
NOTE: The inspection criteria below are applicable after removal of high metal.
NOTE: You can use equivalent alternatives for standard tools, equipment and consumable materials.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 1M(3 FT)
No specific
1
MAT - PROTECTIVE
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-803-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-803-A
Closing of the Fan Cowl Doors
TASK 72-21-40-000-801-A
Removal of the Front Spinner
TASK 72-21-40-400-801-A
Installation of the Front Spinner
3. Job Set-up
Subtask 72-21-22-941-050-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position not less than five minutes before you do this procedure.
     (c) Put a WARNING NOTICE(S) in position to tell persons not to operate:
  • The ENG/MODE selector switch
  • The ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 72-21-22-010-050-A
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (2) Put an ACCESS PLATFORM 1M(3 FT) in position.
   (3) Install a MAT - PROTECTIVE in the inlet cowl.
Subtask 72-21-22-010-051-A
C. Get Access
   (1) Remove the front spinner (Ref. AMM TASK 72-21-40-000-801).
4. Procedure
Subtask 72-21-22-210-050-A
A. Visual Inspection of Low Pressure Compressor (LPC) Cover (1)

Look for
MAXIMUM SERVICEABLE LIMITS
1.Visual inspection of all areas
A.Dents
Any amount up to:
  • 0.0098 in. (0.25 mm) in depth
  • 0.098 in. (2.49 mm) in length.
B.Nicks
Any amount up to:
  • 0.0098 in. (0.25 mm) in depth
  • 0.098 in. (2.49 mm) in length.
C.Scratches
Any amount up to:
  • 0.0098 in. (0.25 mm) in depth
  • 0.098 in. (2.49 mm) in length.
2.Visual inspection of area B, seal groove
A.Nicks, dents, scratches
Not serviceable.
3.Visual inspection of diameter E
A.Fretting
Any amount, if diameter E is between 5.60 in. (142.24 mm) and 5.6016 in. (142.28 mm).
B.Pitting
Not serviceable.
4.Visual Inspection of Area F, anti-rotation tang/lug
A.Peening and wear
Any amount, if the dimension J is between 0.378 in. (9.60 mm) and 0.386 in. (9.80 mm).
B.Breaking and distortion
Not serviceable.
5.Visual Inspection of Dimension G, anti-rotation tang/lug
A.Wear
Any amount, if the dimension G is between 0.154 in. (3.91 mm) and 0.161 in. (4.09 mm).
6.Visual inspection of area L, thread
A.Nicks, dents, scratches, bent, worn, torn thread
Not serviceable.
5. Close-up
Subtask 72-21-22-410-051-A
A. Install the front spinner (Ref. AMM TASK 72-21-40-400-801).
Subtask 72-21-22-410-050-A
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the MAT - PROTECTIVE from the inlet cowl.
   (3) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL 448AR
   (4) Remove the access platform(s).
   (5) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:51:49 UTC