W DOC AIRBUS | AMM A320F

Procedure After Volcanic Ash Environment Operation (131-9(A))


TASK 49-00-00-200-809-A
Procedure After Volcanic Ash Environment Operation (131-9(A))


WARNING: DO NOT BREATHE VOLCANIC ASH. DO NOT GET VOLCANIC ASH IN YOUR EYES. PUT ON PROTECTIVE CLOTHES, EYE GOGGLES AND A RESPIRATOR MASK. MAKE SURE THAT THE RESPIRATOR MASK CAN REMOVE VOLCANIC ASH FROM THE AIR. VOLCANIC ASH CAN CAUSE EYE IRRITATION AND INJURY TO THE RESPIRATORY SYSTEM.
CAUTION: YOU MUST EXAMINE THE ENGINE VERY CAREFULLY AFTER FLIGHT THROUGH VOLCANIC ASH OR SAND. THE INGESTION OF MUCH VOLCANIC ASH OR SAND INTO THE ENGINE CAN CAUSE OPERATIONAL PROBLEMS AND UNSATISFACTORY ENGINE PERFORMANCE. IF YOU DO NOT OBEY THE STEPS THAT FOLLOW, AN IN-FLIGHT SHUTDOWN CAN OCCUR.
CAUTION: IF THERE IS DRY SAND/DUST, DO NOT USE FLUIDS TO REMOVE THE SAND/DUST. IF THERE IS LAYER OF SAND/DUST ON THE AIRCRAFT SURFACES, REMOVE THE SAND/DUST WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE SAND/DUST AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN.
1. Reason for the Job
This procedure is in agreement with EASA Safety Information Bulletin 2010-17 and ICAO Volcanic Ash Contingency Plan EUR Doc 019.
NOTE: APU operations in or through known volcanic ash laden environments should be prevented because of the high potential for maintenance issues. The long term effects of exposure to the volcanic ash are unknown and may manifest themselves hundreds of hours after exposure. If aircraft is in contact with ash environments contact Honeywell Aerospace Technical Support at +1 855-808-6500 US & Canada (Toll Free) or +1 602-365-6500 International, or mail to: AeroTechSupport@Honeywell.com
NOTE: If the volcanic ash contamination occurred when the aircraft was on ground with applicable protection by covers and blankets (Ref. AMM 10-11-00), and if there is no ash behind the covers, the inspections specified hereafter are not necessary
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
BLOWING EQUIPMENT - DRY AIR
No specific
1
PROBE - NON METALLIC, FLEXIBLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
VACUUM CLEANER
No specific
1
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
315AL, 316AR
 D. 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 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 26-22-00-210-001-A
Detailed Inspection of Distribution Piping
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 31-36-00-740-010-A
Printout of the Stored Reports
TASK 49-00-00-710-010-A
Operational Test of the APU
TASK 49-16-00-200-002-A
Detailed Inspection of APU Air Intake, Diffuser Elbow, Seals and Felt Metal
TASK 49-32-41-920-001-A
Replacement of the Fuel Filter (131-9(A))
TASK 49-52-51-000-002-A
Removal of the Cooling Fan (131-9(A))
TASK 49-52-51-400-002-A
Installation of the Cooling Fan (131-9(A))
TASK 49-81-41-000-003-A
Removal of the Exhaust Muffler (131-9(A))
TASK 49-81-41-400-003-A
Installation of the Exhaust Muffler (131-9(A))
TASK 49-91-00-740-001-A
Read CFDS for APU CLASS 3 Fault(s) of APU OIL DIFF PRESSURE SWITCH (P9) and GENERATOR SCAV DIFFERENTIAL PRESSURE SWITCH (P5) (131-9(A))
TASK 49-91-41-200-002-A
Remove and Discard Oil Filter Elements (131-9(A))
TASK 49-91-44-000-004-A
Removal of the Oil Cooler (131-9(A))
TASK 49-91-44-400-004-A
Installation of the Oil Cooler (131-9(A))
TASK 52-41-00-010-001-A
Open the APU Doors for Access
TASK 52-41-00-410-001-A
Close the APU Doors after Access
3. Job Set-up
Subtask 49-00-00-860-192-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) On the panel 25VU, press the APU MASTER SW pushbutton switch then make sure that the APU air intake flap has moved to the fully open position.
   (3) Put a WARNING NOTICE(S) in the cockpit to tell persons not to start the APU.
   (4) Make sure that the hydraulic systems are depressurized
(Ref. AMM TASK 29-00-00-864-001).
Subtask 49-00-00-865-189-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
Subtask 49-00-00-010-101-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the APU access doors 315AL and 316AR.
   (2) Open the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-010-001).
   (3) Set the light SW 11LJ to the ON position.
4. Procedure
Subtask 49-00-00-280-054-A ** ON A/C NOT FOR ALL
A. Procedure After Volcanic Ash Environment Operation
CAUTION: IF THERE IS DRY ASH, DO NOT USE FLUIDS TO REMOVE THE ASH. IF THERE IS A LAYER OF ASH ON THE AIRCRAFT SURFACES, REMOVE THE ASH WITH A VACUUM CLEANER (OR, IF YOU CANNOT USE A VACUUM CLEANER, USE AN AIR BLOWER, A SOFT CLOTH OR A HAND BRUSH). FLUIDS CAN MIX WITH THE ASH AND MAKE A PASTE THAT CAN CAUSE EROSION/ABRASION. THIS PASTE CAN GO INTO AREAS THAT ARE NOT EASY TO CLEAN.
   (1) Examine APU air inlet and exhaust ducts for ash contamination (Ref. AMM TASK 49-16-00-200-002). If you find contamination:
     (a) Clean the Air Intake System. Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , VACUUM CLEANER and BLOWING EQUIPMENT - DRY AIR to remove any ash that could be ingested.
   (2) Examine the Exhaust Muffler. If you find contamination:
     (a) Remove the exhaust muffler (Ref. AMM TASK 49-81-41-000-003).
     (b) Clean the exhaust muffler with a dry Textile-Lint free Cotton - (Material No.14SBA1) , VACUUM CLEANER and BLOWING EQUIPMENT - DRY AIR to remove any ash that could be ingested.
     (c) Examine the exhaust muffler drain system.
     (d) If you find blockage into the exhaust drain line, use a PROBE - NON METALLIC, FLEXIBLE to make sure that the drain pipe is not blocked. If the drain pipe is blocked, remove the blockage without neither water nor any water based agent. BLOWING EQUIPMENT - DRY AIR is recommended to remove possible blockages.
     (e) Install the exhaust muffler (Ref. AMM TASK 49-81-41-400-003)
   (3) Examine the drain mast for contamination.
     (a) Examine the drain mast and all the drain lines.
     (b) If you find blockage in the drain line, use a PROBE - NON METALLIC, FLEXIBLE to make sure that the drain pipe is not blocked.
     (c) If the drain pipe is blocked, remove the blockage without water or any water based agent. BLOWING EQUIPMENT - DRY AIR is recommended to remove possible blockages.
   (4) Do a general visual inspection of the APU ventilation system and the APU Compartment for contamination. If you find contamination:
     (a) Remove all volcanic ashes from visible and easy access areas of the APU compartment and the APU ventilation system. Use a clean Textile-Lint free Cotton - (Material No.14SBA1) , VACUUM CLEANER and BLOWING EQUIPMENT - DRY AIR to remove any ash that could be ingested in the APU compartment.
   (5) Examine if there is contamination in the Oil cooler:
Print the APU MES/IDLE Report <13>. (Ref. AMM TASK 31-36-00-740-010) and record the Oil Sump Temperature (OTA) parameter shown in APU MES/IDLE Report <13>.
     (a) If OTA is less than 140deg.C (284deg.F), continue operating APU normally.
     (b) If OTA get 140deg.C (284deg.F) or above.
       1 Remove Oil Cooler (Ref. AMM TASK 49-91-44-000-004).
       2 Clean the Oil Cooler with a clean Textile-Lint free Cotton - (Material No.14SBA1) , VACUUM CLEANER and BLOWING EQUIPMENT - DRY AIR to remove all the ashes and dirt found.
       3 Remove the Fan Assembly (Ref. AMM TASK 49-52-51-000-002).
       4 Clean the Fan Assembly and cooling ducts with a clean Textile-Lint free Cotton - (Material No.14SBA1) , VACUUM CLEANER and BLOWING EQUIPMENT - DRY AIR to remove all ashes and dirt found.
       5 Install the Fan Assembly (Ref. AMM TASK 49-52-51-400-002).
       6 Install the Oil Cooler (Ref. AMM TASK 49-91-44-400-004).
   (6) Read CFDS for APU CLASS 3 Fault(s) of APU OIL DIFF PRESSURE SWITCH (P9) and GENERATOR SCAV DIFFERENTIAL PRESSURE SWITCH (P5) (131-9(A)), (Ref. AMM TASK 49-91-00-740-001)
     (a) If necessary, replace the filters. (Ref. AMM TASK 49-91-41-200-002).
NOTE: If A/C operates on a NFL (No Flight Zone) or operates regularly in ash laden environments such as TLZ (Time Limited Zone) it is recommended to replace oil filters and oil every 100 hours of operation.
   (7) Examine the fire extinguisher outlets for contamination (Ref. AMM TASK 26-22-00-210-001)
   (8) If A/C fuel system maintenance is required because of ash contamination then replace the APU fuel filters. (Ref. AMM TASK 49-32-41-920-001)
   (9) Do an operational test (Ref. AMM TASK 49-00-00-710-010) and if the test result is not satisfactory, shutdown the APU and do the troubleshooting provided for the fault/s detected during the operational test.
   (10) Record operation of APU in ash environment in APU logbook.
5. Close-up
Subtask 49-00-00-410-095-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) Set the LIGHT control switch 11LJ to the OFF position.
   (3) Close the APU access doors 315AL and 316AR (Ref. AMM TASK 52-41-00-410-001).
   (4) Remove the access platform(s).
   (5) Remove the WARNING NOTICE(S).
Subtask 49-00-00-865-190-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUAPU/APU/CTL2KDL42
121VUAPU/ECB/SPLY1KDL41
Subtask 49-00-00-860-193-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Put the related hydraulic system in the pressurized configuration (Ref. AMM TASK 29-00-00-864-001).
   (2) De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 01:26:13 UTC