W DOC AIRBUS | AMM A320F

Inspection of Mid Acoustical Panels [CFMB]


TASK 72-23-00-280-006-A
Inspection of Mid Acoustical Panels


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
ACCESS PLATFORM 1M(3 FT)
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 72-00-00-200-025-A
Over-Serviceable-Limit Extensions
TASK 72-00-00-200-025-A-01
Over-Serviceable-Limit Extensions
TASK 72-21-00-000-005-A
Removal of the Spinner Front Cone
TASK 72-21-00-000-006-A
Removal of the Spinner Rear Cone
TASK 72-21-00-000-007-A
Removal of the Fan Rotor Blades
TASK 72-21-00-400-005-A
Installation of the Spinner Front Cone
TASK 72-21-00-400-006-A
Installation of the Spinner Rear Cone
TASK 72-21-00-400-007-A
Installation of the Fan Rotor Blades
TASK 72-23-00-000-025-A
Removal of the Mid Acoustical Panels
TASK 72-23-00-300-044-A
Repair of Forward, Mid and Aft Acoustical Panels when Unbonded Cup
TASK 72-23-00-400-025-A
Installation of the Mid Acoustical Panels
TASK 72-23-00-400-044-A
Installation of Acoustical Panels Attachment Screw Locking
3. Job Set-up
Subtask 72-23-00-941-091-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 72-23-00-010-113-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Put an ACCESS PLATFORM 1M(3 FT) in position at the front of the engine.
   (2) Remove the spinner front cone (Ref. AMM TASK 72-21-00-000-005).
   (3) Remove the spinner rear cone (Ref. AMM TASK 72-21-00-000-006).
   (4) Put a temporary mark on each fan blade from 1 to 36.
   (5) Remove 3 consecutive fan blades (Ref. AMM TASK 72-21-00-000-007).
To compensate for imbalance caused by the removal of 3 blades, it is recommended to remove 3 blades 180-degrees opposite to those removed before.

4. Procedure
Subtask 72-23-00-350-059-A ** ON A/C NOT FOR ALL
A. Inspection of Mid Acoustical Panels
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Leading edge delamination
Not serviceable
Replace panel (Ref. AMM TASK 72-23-00-000-025) and (Ref. AMM TASK 72-23-00-400-025).
2.Inner skin delamination in acoustical area
20 percent of acoustical area
Above 20 percent, replace panel (Ref. AMM TASK 72-23-00-000-025) and (Ref. AMM TASK 72-23-00-400-025).
3.Mid acoustical panel cups


A.Dents, marks, indentations caused by screw head
No limits

B.Pierced cups caused by screw head
No limits
(Ref. AMM TASK 72-23-00-400-044)
C.Unbonded cups
Not serviceable
(Ref. AMM TASK 72-23-00-300-044)
D.Missing cups.
Not serviceable
(Ref. AMM TASK 72-23-00-300-044)
4.Missing panel
Not serviceable

5.Loose bolts
Not serviceable
Tighten bolts.
6.Subsurface linear impressions or wrinkles
No limits
Serviceable criteria applied on new parts.
7.Voids
Five per panel, 2 in. (50.8 mm) apart, 0.12 in. (3 mm) Dia max., 0.012 in. (0.3 mm) max. depth
Serviceable criteria applied on new parts.
8.Defects in the protective coating (initial Tedlar film, or paint) such as:


A.Missing
No limits
Remove the loose material with a sharp blade.
B.Defects (dents, nicks, tears, flaking) that let show the inner skin
No limits
Remove the loose material with a sharp blade.
9.Inner skin defects, such as:


A.Superficial defects (dents, nicks, tears, impact marks) not through the skin
No limits with a total surface area less than 4 square in. (2580 sq mm) per panel
Remove the loose material with a sharp blade.
B.Defects (tears, cracks, punctures) through the skin
Not serviceable
Replace panel(s) (Ref. AMM TASK 72-23-00-000-025) and (Ref. AMM TASK 72-23-00-400-025).
C.Stiffener delamination under panel leading edge
Sound not constant with adjacent area by tap test control. Do the tap test control on the first 0.83 in. (21 mm) area from the leading edge on assembled panels
Replace panel(s) (Ref. AMM TASK 72-23-00-000-025) and (Ref. AMM TASK 72-23-00-400-025).
10.Damper


A.Cracks (if panel removed)
Any amount

B.Disbonded damper (if panel removed)
Any amount not more than 20 percent of the total bonded surface
Replace mid acoustical panels that are not in the limits (Ref. AMM TASK 72-23-00-000-025) and (Ref. AMM TASK 72-23-00-400-025).
Refer to the over-serviceable limit extensions (Ref. AMM TASK 72-00-00-200-025).
5. Close-up
Subtask 72-23-00-410-104-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Install the fan rotor blades at the locations recorded at the removal (Ref. AMM TASK 72-21-00-400-007).
   (2) Install the spinner rear cone (Ref. AMM TASK 72-21-00-400-006).
   (3) Install the spinner front cone (Ref. AMM TASK 72-21-00-400-005).
   (4) Make sure that the work area is clean and clear of tools and other items.
   (5) Remove the ACCESS PLATFORM 1M(3 FT).
   (6) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:41:54 UTC