W DOC AIRBUS | AMM A320F

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


TASK 36-11-00-200-802-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.
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
437AL, 438AR, 447AL, 448AR
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 36-11-44-000-802-A
Removal of the Bleed-Air Precooler-Exchanger Cold-Inlet
TASK 36-11-44-200-802-A
Visual Inspection of the Bleed-Air Precooler-Exchanger Inlet
TASK 36-11-44-400-802-A
Installation of the Bleed-Air Precooler-Exchanger Cold-Inlet
TASK 36-11-54-000-802-A
Removal of the Fan Air-Valve Actuator
TASK 36-11-54-000-803-A
Removal of the Fan Air Valve (FAV)
TASK 36-11-54-400-802-A
Installation of the Fan Air-Valve Actuator
TASK 36-11-54-400-803-A
Installation of the Fan Air Valve (FAV)
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-805-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-802-A
Closing of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 36-11-00-861-144-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 36-11-00-941-143-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 36-11-00-865-130-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 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-00-010-179-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-802):
     (a) For ENGINE-1 (1000EM1)
437AL 438AR.
     (b) For ENGINE-2 (1000EM2)
447AL 448AR.
   (2) Put the ACCESS PLATFORM 1M(3 FT) in position below the engine.
Subtask 36-11-00-040-120-A ** ON A/C NOT FOR ALL
E. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-040-805).
Subtask 36-11-00-010-180-A ** ON A/C NOT FOR ALL
F. Get Access
   (1) Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
4. Procedure
Subtask 36-11-00-210-057-A ** ON A/C NOT FOR ALL
A. Inspection of the Bleed Air Cold Flow Path after Hail and Bird Strike
   (1) Do an 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):
  • Replace the elbow duct (1).
   (2) Do an 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) Do an inspection of the fan air valve body 7120HM1 (7120HM2):
     (a) If there are cracks, marks and/or distortion (specially in the area that connect the fan air valve body (2) with the ducts):
   (4) Do an inspection of the fan air valve actuator 9HA1 (9HA2):
     (a) If there are cracks, marks and/or distortion:
   (5) Do an inspection of the exchanger inlet (3) (Ref. AMM TASK 36-11-44-200-802).
     (a) If you find damage in the exchanger inlet (3):
5. Close-up
Subtask 36-11-00-865-131-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 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-00-410-168-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 78-36-00-410-802):
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
Subtask 36-11-00-440-105-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-440-805).
Subtask 36-11-00-410-169-A ** ON A/C NOT FOR ALL
D. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (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 36-11-00-862-127-A ** ON A/C NOT FOR ALL
E. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 04:00:52 UTC