W DOC AIRBUS | AMM A320F

Borescope Inspection of the Common Nozzle Assembly Fireproof Bulkhead (Engine/CNA installed) [IAE]


TASK 78-10-00-200-014-A
Borescope Inspection of the Common Nozzle Assembly Fireproof Bulkhead (Engine/CNA installed)


1. Reason for the Job
Refer to the MPD TASK: 781000-I3
BORESCOPE INSPECTION OF THE COMMON NOZZLE ASSEMBLY FIREPROOF BULKHEAD (ENGINE/CNA INSTALLED)
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT)
No specific
AR
BORESCOPE SET
No specific
AR
WARNING NOTICE(S)
 B. 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
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-32-00-010-010-A
Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A
Closing of the Thrust Reverser Halves
3. Job Set-up
Subtask 78-10-00-941-054-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 78-10-00-010-058-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowls doors (Ref. AMM TASK 71-13-00-010-010):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Put the ACCESS PLATFORM 2M (6 FT) in position.
Subtask 78-10-00-040-054-A ** ON A/C NOT FOR ALL
C. Deactivate the Thrust Reverser
WARNING: MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
   (1) Deactivate the thrust reverser Hydraulic Control Unit (HCU) (Ref. AMM TASK 78-30-00-040-012).
Subtask 78-10-00-010-059-A ** ON A/C NOT FOR ALL
D. Open the Thrust Reverser Halves (Ref. AMM TASK 78-32-00-010-010):
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR
4. Procedure
Subtask 78-10-00-210-054-A ** ON A/C NOT FOR ALL
A. Examine the Common Nozzle Assembly
F Mixed Exhaust System ** ON A/C NOT FOR ALL
   (1) Use a BORESCOPE SET to do an inspection. Put the boroscope between the CNA and the pylon, aft the engine.
   (2) Examine the upper support strut (CN4) and the fireproof bulkhead for any obvious damage, cracks or loose or missing fasteners. If damage is found, contact Goodrich for disposition.
5. Close-up
Subtask 78-10-00-410-058-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 halves (Ref. AMM TASK 78-32-00-410-010):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 78-10-00-440-054-A ** ON A/C NOT FOR ALL
B. Activate the Thrust Reverser Hydraulic Control Unit (Ref. AMM TASK 78-30-00-440-012).
Subtask 78-10-00-410-059-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowls doors (Ref. AMM TASK 71-13-00-410-010):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:26:59 UTC