W DOC AIRBUS | AMM A320F

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


TASK 72-22-40-210-801-A
Visual Inspection of the Low Pressure Compressor (LPC) Shaft


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 Low Pressure Compressor (LPC) shaft.
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. Referenced Information
REFERENCE
DESIGNATION
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 72-22-40-941-050-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).
   (3) Put an ACCESS PLATFORM 1M(3 FT) in position.
   (4) Install a MAT - PROTECTIVE in the lower half of the inlet cowl.
4. Procedure
Subtask 72-22-40-210-050-A
A. Visual Inspection of Low Pressure Compressor (LPC) Shaft
   (1) Remove the front spinner (Ref. AMM TASK 72-21-40-000-801).
   (2) Do a visual inspection of the LPC shaft (1):

Table 601: Visual inspection of all non-painted areas

INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
Dents
Any number up to:
- 0.004 in. (0.10 mm) in depth
- 0.020 in. (0.51 mm) in length.

Nicks
Any number up to:
- 0.004 in. (0.10 mm) in depth
- 0.020 in. (0.51 mm) in length.

Scratches
Any number up to:
- 0.004 in. (0.10 mm) in depth
- 0.020 in. (0.51 mm) in length.

Corrosion, pitting
Not serviceable.

Cracks
Not serviceable.

Metal loss
Not serviceable.

Table 602: Visual inspection of all painted areas

INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
Nicks, dents, scratches,
bent, worn, torn thread
Any amount if parent material not
affected.

Corrosion, pitting
Not serviceable.

Cracks
Not serviceable.

Metal loss
Not serviceable.

Missing paint
Any amount if there is a
minimum thickness of 0.00138 in. (0.04 mm)
remaining.

Peeling, blistering,
wear (bending)
Not serviceable.


Table 603: Visual inspection of dimension M, forward anti-rotation lugs
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
Fretting
Any amount, if dimension M is
between 0.09744 in. (2.47 mm)
and 0.10846 in. (2.75 mm).

Table 604: Visual inspection of dimension N, forward anti-rotation lugs

INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
Nicks, dents, scratches
Any number, if dimension N is
between 0.0791 in. (2.01 mm)
and 0.0843 in. (2.14 mm).

Table 605: Visual inspection of area A, forward anti-rotation lugs

INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
Nicks, dents, scratches
Any number up to:
- 0.004 in. (0.10 mm) in depth
- 0.020 in. (0.51 mm) in length.

Missing paint
Any amount.

   (3) Install the front spinner (Ref. AMM TASK 72-21-40-400-801).
5. Close-up
Subtask 72-22-40-942-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the MAT - PROTECTIVE.
   (3) Remove the access platform(s).
   (4) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:52:14 UTC