W DOC AIRBUS | AMM A320F

Inspection of Forward Acoustical Panels [CFMB]


TASK 72-23-00-280-005-A
Inspection of Forward 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)-ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 72-23-00-000-009-A
Removal of the Forward Acoustical Panels of the Fan
TASK 72-23-00-300-044-A
Repair of Forward, Mid and Aft Acoustical Panels when Unbonded Cup
TASK 72-23-00-400-009-A
Installation of the Forward Acoustical Panels of the Fan
3. Job Set-up
Subtask 72-23-00-941-090-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).
   (4) Put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).
   (5) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position at the front of the engine.
4. Procedure
Subtask 72-23-00-350-058-A ** ON A/C NOT FOR ALL
A. Inspection of FWD Acoustical Panels
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.FWD acoustical panels


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

B.Pierced cups caused by screw head.
Not serviceable
Replace and bond the cups (Ref. AMM TASK 72-23-00-300-044)
C.Unbonded cups.
Not serviceable
Repair the panel (Ref. AMM TASK 72-23-00-300-044) and re-install the panel immediately (Ref. AMM TASK 72-23-00-400-009). Panel must be repaired at next shop visit.
D.Missing cups.
Not serviceable
Replace the panel (Ref. AMM TASK 72-23-00-000-009) and (Ref. AMM TASK 72-23-00-400-009).
E.Missing insert thread
No limits

F.Missing panel
Not serviceable

G.Loose bolts
Not serviceable
Tighten bolts
H.Local collapse of panel inner surface
No limits

J.Subsurface linear impressions or wrinkles
No limits
Serviceable criteria applied on new parts
K.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
L.Defects in the protective coating (initial Tedlar film, or paint) such as:


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


(1)Superficial defects (dents, nicks, tears, impacts 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.
(2)Defects (tears, cracks, punctures) through the skin
Not serviceable
Replace panel(s) (Ref. AMM TASK 72-23-00-000-009) and (Ref. AMM TASK 72-23-00-400-009).
5. Close-up
Subtask 72-23-00-410-103-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 12:59:48 UTC