W DOC AIRBUS | AMM A320F

Installation of the Acoustical Panels Attachment Screw Locking [CFMI]


TASK 72-23-00-400-045-A
Installation of the Acoustical Panels Attachment Screw Locking


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the Job
This procedure gives the information to lock an acoustical panel when the panel cup inspected is pierced by screw head. This procedure applies to any acoustical panel screws: fwd, mid and aft. Panels with damaged cups re-installed per this procedure will have to be changed at first shop visit opportunity.
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)
No specific
Torque wrench: range to between 75 and 66 lbf.in (0.85 and 0.75 m.daN ) T
No specific
Torque wrench: range to between 93 and 84 lbf.in (1.05 and 0.95 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2101)
graphite grease
(Material No.CP2242)
RTV 732
(Material No.CP2266)
RTV 102
(Material No.CP2431)
RTV 730
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-000-040-A
Removal of the Power Plant
TASK 71-00-00-000-040-A-01
Removal of the Power Plant with the Engine Positioner TWW 75E
TASK 71-00-00-000-040-A-03
Removal of the Power Plant with Jacxson Tool
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 72-23-00-400-042-A
Installation of the Acoustical Panels Attachment Screw/Nut Locking
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A
Closing of the Thrust Reverser Doors
SPM 702111
ESM 722302300008
3. Job Set-up
Subtask 72-23-00-941-104-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 72-23-00-010-130-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
   (2) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (3) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (4) Put an ACCESS PLATFORM 1M(3 FT) in position.
Subtask 72-23-00-040-075-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 72-23-00-010-131-A ** ON A/C NOT FOR ALL
D. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040):
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure
Subtask 72-23-00-420-071-A ** ON A/C NOT FOR ALL
A. Locking of Acoustical Panels
CAUTION: COATING SCREWS IS MANDATORY.
   (1) If panel cup(s) found pierced, do the procedure that follows:
     (a) Remove the bolt.
     (b) Clean all damaged cups SPM 702111.
     (c) Fill all damaged cups with RTV 732 (Material No.CP2242) or RTV 102 (Material No.CP2266) or RTV 730 (Material No.CP2431) .
NOTE: You must install the screw, with only a light layer of graphite grease (Material No.CP2101) , a short time after you apply the RTV (before polymerisation).
   (2) Apply a layer of graphite grease (Material No.CP2101) to the threads of all the screws that attach acoustical panels.
   (3) Re-install the acoustical panels and screws.
CAUTION: DO NOT EXCEED THE SPEED OF 200 RPM TO APPROACH ALL ACOUSTICAL PANEL SCREWS BY USING PNEUMATIC OR ELECTRICAL SCREW DRIVERS.
   (4) Measure the self locking nut torque of each nut when you start to tighten the screws.
NOTE: Make sure that the screws are not damaged, replace them if necessary.
     (a) If the self locking nut torque is less than 4.5 lbf.in (0.05 m.daN) (Ref. AMM TASK 72-23-00-400-042).
     (b) If the self locking nut torque is between 4.5 lbf.in (0.05 m.daN) and 31 lbf.in (0.35 m.daN), TORQUE the screws of fwd and mid panels to between 93 and 84 lbf.in (1.05 and 0.95 m.daN ) T and TORQUE the screws of aft panels to between 75 and 66 lbf.in (0.85 and 0.75 m.daN ) T.
     (c) If the self locking nut torque is more than 31 lbf.in (0.35 m.daN), but less than 49 lbf.in (0.55 m.daN), TORQUE the screws at the running torque value and add 44 lbf.in (0.50 m.daN).
     (d) If the self locking nut torque is more than 49 lbf.in (0.55 m.daN), remove the engine (
Ref. AMM TASK 71-00-00-000-040) and do the engine shop repair procedure to replace the self locking nut ESM 722302300008.
5. Close-up
Subtask 72-23-00-410-123-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) Close the thrust reverser doors (Ref. AMM TASK 78-36-00-410-040):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 72-23-00-440-069-A ** ON A/C NOT FOR ALL
B. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 72-23-00-410-124-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors: (Ref. AMM TASK 71-13-00-410-040)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.02 06:33:42 UTC