W DOC AIRBUS | AMM A320F

Visual Inspection of the Accessory Gearbox (AGB) Sleeve of Line 5 without Special Equipment [CFML]


TASK 72-63-12-210-801-A
Visual Inspection of the Accessory Gearbox (AGB) Sleeve of Line 5 without Special Equipment


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.
ZONE: 400
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)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
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 79-21-05-000-804-A
Removal of the Lubrication Unit
TASK 79-21-05-400-804-A
Installation of the Lubrication Unit
3. Job Set-up
Subtask 72-63-12-941-051-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 WARNING NOTICE(S) in position to tell persons not to operate:
  • The ENG/MODE selector switch, and
  • 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 72-63-12-010-051-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) Remove the splined sleeve assembly (Ref. AMM TASK 79-21-05-000-804).
4. Procedure
Subtask 72-63-12-210-051-A
A. Visual Inspection of the AGB Sleeve of Line 5
   (1) Do a visual inspection of the splined sleeve assembly of AGB Line 5. Refer to the table below for the inspection criteria:
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Examine all areas of the splined sleeve assembly for:


A.Cracks
Not serviceable

B.Missing protective coating
Any amount that does not exceed 5 percent of inner and outer surface area exclusive of splines.

C.Corrosion
Not serviceable

D.Heat discoloration
Accept bright polished steel to straw color.
Accept blue color if discoloration disappears after cleaning.

E.Coked oil deposit
Accept if disappears after cleaning.

2.Examine the splines for:


A.Dents, nicks, burrs
Any amount that is not felt with 0.03 in. (0.76 mm) radius scriber

B.Wear
Any amount that is not felt with 0.03 in. (0.76 mm) radius scriber

C.Scratches
Any amount that is not felt with 0.03 in. (0.76 mm) radius scriber

3.Examine the level cup for:


A.Missing or loose
Not serviceable

5. Close-up
Subtask 72-63-12-410-051-A
A. Close Access
   (1) Install the splined sleeve assembly (Ref. AMM TASK 79-21-05-400-804).
   (2) Make sure that the work area is clean and clear of tools and other items.
   (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 WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 13:14:50 UTC