W DOC AIRBUS | AMM A320F

Visual Inspection of the Flow Path Panel [CFML]


TASK 72-21-01-210-802-A
Visual Inspection of the Flow Path Panel


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 the criteria for the visual inspection of the flow path panel.
NOTE: The inspection criteria below are applicable after the removal of the 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 72-21-01-000-802-A
Removal of the FlowPath Panel
TASK 72-21-01-400-802-A
Installation of the FlowPath Panel
3. Job Set-up
Subtask 72-21-01-941-057-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 72-21-01-210-051-A
A. Visual Inspection of the Flow Path Panel
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Visual inspection of the visible outer surface (this does not include extracting holes (4), borescope passthrough holes (2) and draining holes (3)):


A.Contact marks
Any number up to 0.0008 in. (0.02 mm) in depth.

B.Dents, Nicks
Any number up to 0.012 in. (0.3 mm) in depth.

C.Scratches
Any number up to 0.012 in. (0.3 mm) in depth.

D.Cracks, tears
Not serviceable
Replace the flow path panel (1) (Ref. AMM TASK 72-21-01-000-802) and (Ref. AMM TASK 72-21-01-400-802).
E.Missing surface coating (sulfuric anodization)
Not more than ten per cent of total surface

F.Erosion of parent metal
Not serviceable
Replace the flow path panel (1) (Ref. AMM TASK 72-21-01-000-802) and (Ref. AMM TASK 72-21-01-400-802).
2.Visual inspection of the extracting holes (4), borescope passthrough holes (2), draining holes (3)


A.Contact marks
Any number

B.Missing surface coating (sulfuric anodization)
Any amount

C.Dents, Nicks
Any number up to 0.012 in. (0.3 mm) in depth.

D.Scratches
Any number up to 0.012 in. (0.3 mm) in depth.

3.Visual examination of the seal (5)


A.Missing material, cutting, wear, folding
Up to 15 percent of the initial length.

B.Missing seal, cutting, wear, folding
Cumulative length up to 15 percent of the circumference (bonded seal more than 114.33 in. (2.90 m)).

C.Disbonding of partial section
Any amount all along the circumference.

D.Disbonding of the total section
Up to 15 percent in cumulative length all (bonded seal more than 114.33 in. (2.90 m)).

4.Visual examination of the central shoulder (6)


A.Cracks, tears
Not serviceable.

B.Missing of surface coating (sulfuric anodization)
Up to 10 percent of the total area.

C.Erosion of parent metal
Not serviceable.

D.Contact marks
Any amount.

E.Nicks, dents
Any number up to 0.0011 in. (0.03 mm) in depth.

F.Scratches
Any number up to 0.0011 in. (0.03 mm) in depth.

5. Close-up
Subtask 72-21-01-410-053-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 from the lower half of the inlet cowl.
   (3) Remove the access platform(s).
   (4) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 13:03:36 UTC