W DOC AIRBUS | AMM A320F

Inspection of the Bleed Air Cold Flow Path after Hail and Bird Strike


TASK 36-11-00-200-002-A
Inspection of the Bleed Air Cold Flow Path after Hail and Bird Strike


WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
WARNING: PUT A WARNING NOTICE ON THE HIGH PRESSURE GROUND POWER CONNECTIONS TO TELL PERSONS NOT TO OPERATE THE PNEUMATIC SYSTEM.
CAUTION: USE A SECOND WRENCH TO APPLY COUNTER TORQUE TO THE UNION ON THE VALVE WHEN YOU CONNECT THE HP SENSE TUBE.
FIN: 9HA1 ** ON A/C NOT FOR ALL
FIN: 9HA2 ** ON A/C NOT FOR ALL
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
SAFETY CLIP - CIRCUIT BREAKER
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 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 36-11-44-000-001-A
Removal of the Bleed-Air Precooler Exchanger Inlet
TASK 36-11-44-200-001-A
Visual Inspection of the Bleed-Air Precooler-Exchanger Inlet
TASK 36-11-44-400-001-A
Installation of the Bleed-Air Precooler Exchanger Inlet
TASK 36-11-54-000-001-A
Removal of the Fan Air Valve
TASK 36-11-54-400-001-A
Installation of the Fan Air Valve
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-040-A
Closing of the Fan Cowl Doors
TASK 71-13-00-410-040-B
Closing of the Fan Cowl Doors
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-081-041-B
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for 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
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
TASK 78-36-00-010-040-B
Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A
Closing of the Thrust Reverser Doors
TASK 78-36-00-410-040-B
Closing of the Thrust Reverser Doors
3. Job Set-up
Subtask 36-11-00-861-081-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-00-941-094-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (2) On the AIR COND control panel 30VU:
  • make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on)
  • make sure that the APU BLEED pushbutton switch is released (the ON legend is off)
  • put a WARNING NOTICE(S) to tell persons not to operate the pneumatic system.
   (3) On the ENG control panel 115VU:
  • put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).
   (4) On the HP ground connector:
  • Put a WARNING NOTICE(S) to tell persons not to pressurize the pneumatic system.
   (5) On the ENG section of the maintenance panel 50VU:
  • make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off
  • put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 36-11-00-865-078-A ** ON A/C NOT FOR ALL
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-00-010-080-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-059-A ** ON A/C NOT FOR ALL
E. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 36-11-00-010-081-A ** ON A/C NOT FOR ALL
F. 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.
Subtask 36-11-00-010-080-B ** ON A/C NOT FOR ALL
G. Get Access
   (1) Open the fan cowls (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 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-059-B ** ON A/C NOT FOR ALL
H. 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 36-11-00-010-081-B ** ON A/C NOT FOR ALL
I. 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 36-11-00-210-054-A ** ON A/C NOT FOR ALL
A. Inspection of the Bleed Air Cold Flow Path after Hail and Bird Strike
   (1) Inspection of the elbow duct (1) for cracks, dents and damage.
NOTE: The damage limits are given in Duct and Fuel Pipe Repair Manual (Ref. DFPRM 51-12-00-200-801-A01).
     (a) If you find cracks, dents or damage on the elbow duct (1):
       1 Replace the elbow duct (1).
   (2) Inspection of the ducts for cracks, dents and damage.
NOTE: The damage limits are given in Duct and Fuel Pipe Repair Manual (Ref. DFPRM 51-12-00-200-801-A01).
   (3) Inspection of the Fan Air Valve (FAV) (2):
F Inspection of the Fan Air Valve ** ON A/C NOT FOR ALL
     (a) If there are cracks, marks and/or distortion (specially in the area that conn ect the FAV (2) with the ducts):
       1 Replace the FAV (2) (Ref. AMM TASK 36-11-54-000-001) (Ref. AMM TASK 36-11-54-400-001).
   (4) Inspection of the exchanger inlet (3) (Ref. AMM TASK 36-11-44-200-001).
     (a) If you found damage in the exchanger inlet (3):
       1 Replace the exchanger inlet (Ref. AMM TASK 36-11-44-000-001) (Ref. AMM TASK 36-11-44-400-001).
5. Close-up
Subtask 36-11-00-865-079-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-00-410-080-A ** ON A/C NOT FOR ALL
B. 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 36-11-00-440-060-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 36-11-00-410-079-A ** ON A/C NOT FOR ALL
D. 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 access platform(s).
   (3) Remove the WARNING NOTICE(S).
Subtask 36-11-00-410-080-B ** ON A/C NOT FOR ALL
E. 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 36-11-00-440-060-B ** ON A/C NOT FOR ALL
F. Activate the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).
Subtask 36-11-00-410-079-B ** ON A/C NOT FOR ALL
G. Close Access
   (1) Close the fan cowls (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 WARNING NOTICE(S).
   (3) Remove the access platform(s).
Subtask 36-11-00-862-076-A ** ON A/C NOT FOR ALL
H. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 04:00:51 UTC