W DOC AIRBUS | AMM A320F

Return to Operation After a Parking Period

TASK 10-30-00-554-804-A
Return to Operation After a Parking Period

WARNING: BEFORE YOU OPEN AN AIRCRAFT DOOR, MAKE SURE THAT THE CABIN IS NOT PRESSURIZED. TO DO THIS, MAKE SURE THAT: - THE AIR CONDITIONING GROUND-CART IS NOT CONNECTED TO THE AIRCRAFT, AND - THE FORWARD AVIONICS-COMPARTMENT ACCESS-DOOR 811 IS OPEN. IF THERE IS REMAINING PRESSURE IN THE AIRCRAFT, THE DOOR CAN OPEN WITH A SUDDEN FORCE. THIS CAN CAUSE INJURY TO YOU OR KILL YOU, AND/OR CAUSE DAMAGE TO THE AIRCRAFT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
WARNING: DO NOT USE THE EMERGENCY LIGHTS TO ILLUMINATE THE CABIN DURING MAINTENANCE. IF YOU USE THE EMERGENCY LIGHTS DURING MAINTENANCE, YOU CAN DECREASE THE LIFE OF THE EPSU BATTERIES AND THEIR INTERNAL VOLTAGE. IF THE INTERNAL VOLTAGE OF THE EPSU BATTERIES IS TOO LOW WHEN YOU CHARGE THEM, THERE IS A RISK OF EXPLOSION.
CAUTION: DURING STORAGE OR PARKING PERIODS, DO NOT STOP OR CHANGE THE MAINTENANCE PROGRAM UNLESS IT WAS AGREED BY THE LOCAL AUTHORITIES. THE MAINTENANCE CALENDAR CLOCK CONTINUES DURING THESE PERIODS. IF YOU DO THE AMM STORAGE OR PARKING PROCEDURES CORRECTLY, AND IF YOU HAVE THE AGREEMENT OF THE LOCAL AUTHORITIES, IT IS NOT NECESSARY TO DO ALL THE SCHEDULED MAINTENANCE TASKS (SUCH AS MPD TASKS) IMMEDIATELY DURING THE STORAGE/PARKING PERIOD. YOU CAN WAIT UNTIL THE END OF THE PERIOD. BUT YOU MUST DO THEM ALL BEFORE THE NEXT FLIGHT.
CAUTION: DURING THIS PROCEDURE:
  • MAKE SURE THAT THE LANDING GEAR GROUND SAFETIES, LOCKING DEVICES AND WHEEL CHOCKS ARE IN POSITION.
  • KEEP THE ACCESS PLATFORM AT A SUFFICIENT DISTANCE FROM THE AIRCRAFT (IN WIND, SHOCK ABSORBER REBOUND CAN CAUSE MOVEMENT OF THE AIRCRAFT).
1. Reason for the Job
This procedure gives the instructions necessary for the return-to-operation of the aircraft after a parking period.
You must complete the return-to-operation procedure at a time, when the aircraft will fly in the 24 hours that follow unless specified differently by the applicable national authority regulations.
If the return-to-operation procedure is immediately followed by large maintenance operations, the aircraft must fly immediately after the signature of the Certificate of Release to Service (CRS) document. During maintenance, it is necessary to find and use an applicable preservation procedure.
It is necessary to do a flight to reset a parking period.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE
No specific
1
SPATULA - NON METALLIC
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.05RAB9)
Adhesive Film Tape-- Aluminium Foil -
(Material No.05RNN1)
Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv -
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 10-11-00-555-013-A
Installation of the Aircraft Protection Equipment
TASK 10-11-00-555-014-A
Removal of the Aircraft Protection Equipment
TASK 10-30-00-280-803-A
Checklist for the Return to Operation After a Parking Period
TASK 12-14-32-200-001-A
Inspection of the MLG Shock Absorbers before Flight
TASK 12-14-32-200-002-A
Check of the NLG Shock Absorber Bottoming
TASK 12-14-32-614-003-A
Functional Check of MLG Shock Absorber Charge Pressure
TASK 12-14-32-614-004-A
Check of the NLG Shock Absorber Charge-Pressure
TASK 12-21-11-615-002-A
External Cleaning
TASK 12-22-52-640-017-A
Lubrication of the Forward or Aft Cargo-Compartment Door-Seal
TASK 12-22-52-640-018-A
Lubrication of the Bulk Cargo-Compartment Door-Seal
TASK 12-31-12-660-002-A
De-Icing of the Aircraft in Power-Off Condition
TASK 12-31-21-660-001-A
Cold Weather Maintenance - Air Conditioning
TASK 12-31-23-554-801-A
Cold Weather Maintenance - Aircraft Return to Service at very low outside temperatures - Communications
TASK 12-31-24-660-001-A
Cold Weather Maintenance - Electrical Power
TASK 12-31-25-660-001-A
Cold Weather Maintenance - Equipment/Furnishings
TASK 12-31-27-660-001-A
Cold Weather Maintenance - Flight Controls
TASK 12-31-28-660-001-A
Cold Weather Maintenance - Fuel
TASK 12-31-31-660-001-A
Cold Weather Maintenance - Indicating/Recording systems and Navigation
TASK 12-31-32-660-001-A
Cold Weather Maintenance - Landing Gear
TASK 12-31-35-660-001-A
Cold Weather Conditions - Maintenance of the Oxygen System
TASK 12-31-38-660-001-A
Cold Weather Maintenance - Water/Waste
TASK 12-31-49-660-001-A
Cold Weather Maintenance - Auxiliary Power Unit
TASK 12-31-51-660-001-A
Cold Weather Maintenance - Structure
TASK 12-31-52-660-001-A
Cold Weather Maintenance - Doors
TASK 12-31-71-660-001-A
Cold Weather Maintenance - Power Plant
TASK 12-31-71-660-802-A
Cold Weather Maintenance - Power Plant
TASK 12-32-28-281-001-A
Drain Water Content
TASK 12-32-28-281-003-A
Sample Fuel for Microbiological Contamination Analysis
TASK 12-32-28-281-005-A
Operate Water Drain Valves in Installed ACT(S) to Drain Accumulated Water
TASK 24-38-00-550-801-A
On-wing Preservation/Return to Service of the Batteries
TASK 24-38-51-280-802-A
Removal of the Battery for Check in Workshop
TASK 24-38-51-400-001-A
Installation of the Battery
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 26-21-00-720-003-A-01
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-21-00-720-003-B-01
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-21-00-720-003-C
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-21-00-720-003-C-01
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-21-00-720-003-C-02
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-21-00-720-802-A
Check Distribution Piping to Detect Leakage and Obstruction
TASK 26-24-00-210-001-A
Inspection/Check of the Portable Fire Extinguishers
TASK 26-25-00-200-002-A
Detailed Inspection of Lavatory Fire Extinguisher for Signs of Leakage/Discharge
TASK 26-25-41-400-001-A
Installation of the Fire Extinguisher Bottle
TASK 26-25-41-400-802-A
Installation of the Fire Extinguisher Bottle of Lavatory A
TASK 26-25-41-400-804-A
Installation of the Fire Extinguisher Bottle of Lavatory DS/ES/HS
TASK 26-25-41-400-805-A
Installation of the Fire Extinguisher Bottle of Lavatory WC/FS/GS
TASK 28-11-00-280-002-A
Structural Fuel Tank Leaks - General Information
TASK 29-10-00-200-001-A
Check Fluid Level on Reservoir Indicators
TASK 29-10-00-200-008-A
Check Nitrogen Charge Pressure on Hydraulic Power Accumulators
TASK 29-22-00-860-008-A
Removal of the Safety Device of the Ram Air Turbine
TASK 29-30-00-200-002-A
Check of the Reservoir Quantity Indication on the ECAM Display Unit
TASK 30-11-00-710-001-A
Operational Test of the Wing Ice-Protection System
TASK 30-21-00-710-002-A
Operational Check of the Engine-Air-Intake Ice-Protection System (with the Engines in operation)
TASK 30-31-00-720-001-A
Functional Check of the Insulation Resistance of the Pitot Probe Heater
TASK 30-45-00-720-002-A
Functional Test of the Rain Repellent System (with the Air Compressor)
TASK 30-45-00-720-002-B
Functional Test of the Rain Repellent System (with the Air Conditioning System)
TASK 31-35-00-710-001-A
Operational Test of the Printer
TASK 31-35-22-400-001-A
Installation of the Printer
TASK 32-41-00-210-002-A
Inspection/Check of the Wheels and Tires
TASK 32-41-00-210-003-A
Functional Check of Tire Pressures
TASK 32-44-11-200-001-A
Functional Check of Parking/Emergency Brake Accumulator by Reading the Charge Pressure on the Accumulator Gauge
TASK 33-51-00-710-001-A
Operational Check of Emergency Power Supply Units by BITE-Check
TASK 33-51-00-710-006-A
Operational Test of Emergency Lights not with CIDS
TASK 33-51-00-710-009-A
Check of all the Cabin Lights and Signs for Correct Illumination and Correct Installation
TASK 33-51-38-400-001-A
Installation of the Emergency Power Supply Unit (EPSU)
TASK 33-51-38-400-002-A
Installation of the Battery of the Emergency Power Supply Unit (EPSU)
TASK 34-10-00-170-001-A
Flushing of the Total Pressure Lines
TASK 34-10-00-170-002-A
Flushing of the Principal Static Pressure Lines
TASK 34-10-00-170-003-A
Draining and Flushing of Standby Pneumatic Circuits
TASK 34-11-15-200-001-A
Inspection/Check of the Pitot Probe
TASK 34-11-16-200-001-A
Inspection of the Static Port and Standby Static Port
TASK 34-11-18-200-002-A
Inspection/Check of the TAT Sensor
TASK 34-11-19-200-001-A
Inspection of the Angle Of Attack (AOA) Sensor
TASK 34-22-25-170-001-A
Draining and Flushing of Standby Pneumatic Circuits
TASK 36-11-00-710-003-A
Operational Test of the Bleed Air System
TASK 36-11-00-710-802-A
Operational Test of the Bleed Air System
TASK 36-11-00-710-804-A
Operational Test of the Bleed Air System with the APU running and the Engines at Idle
TASK 36-11-00-710-806-A
Operational Test of the Bleed Air System with the APU running and the Engines at Idle
TASK 38-10-00-670-002-A
Disinfection of Potable Water System and Discard of Water Filter Elements, if Installed
TASK 38-12-00-710-001-A
Operational Test of the Potable Water-Distribution System (with the APU)
TASK 38-12-00-710-002-A
Operational Test of the Potable Water-Distribution System (with a Ground Air-Supply Cart)
TASK 38-31-00-710-009-A
Operational Test of the Toilet Unit
TASK 49-20-00-600-002-A
Preservation/Storage/Return-to-Service of the APU (APS 3200)
TASK 49-20-00-600-803-A
APU Preservation / Storage / Return to Service (131-9(A))
TASK 51-74-11-300-001-A
Repair of Corroded Areas
TASK 52-10-00-010-001-A
Opening of the Passenger/Crew Door
TASK 52-10-00-410-001-A
Closing of the Passenger/Crew Door
TASK 52-21-11-000-001-A
Removal of the Emergency Exit Hatch
TASK 52-21-11-400-001-A
Installation of the Emergency Exit Hatch
TASK 52-22-00-010-001-A
Opening of the Emergency Exit Doors from the Passenger Compartment
TASK 52-22-00-010-002-A
Opening of the Emergency Exit Doors from the Outside
TASK 52-22-00-410-001-A
Closing of the Emergency Exit Doors from the Passenger Compartment
TASK 52-22-00-410-002-A
Closing of the Emergency Exit Doors from the Outside
TASK 52-30-00-860-001-A
Open the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-002-A
Close the FWD or Aft Cargo-Compartment Door with the Yellow Electric Pump
TASK 52-30-00-860-006-A
Open the Bulk Cargo-Compartment Door
TASK 52-30-00-860-008-A
Close the Bulk Cargo-Compartment Door
TASK 52-41-00-010-002-A
Open the Avionics Compartment Doors for Access
TASK 52-41-00-410-002-A
Close the Avionics Compartment Doors after Access
TASK 54-50-00-200-002-A
Flow Check of Individual Drain Lines of Pylon System
TASK 54-50-00-200-803-A
Operational Check of Pylon Drainage System in Zone C
TASK 56-12-11-400-001-A
Installation of the Sliding Windows
TASK 56-12-11-400-001-A-02
Installation of the Sliding Windows
TASK 71-00-00-550-011-A
Depreservation of Installed Engine
TASK 71-00-00-630-802-A
Depreservation of the Engine
TASK 71-00-00-700-014-B
Cold Weather Operation Procedure
TASK 72-00-00-600-027-A
Depreservation
TASK 72-00-00-600-028-A
Depreservation
TASK 25-64-00-00
FIRST AID EQUIPMENT - DESCRIPTION AND OPERATION
TASK 54-50-00-00
PYLONS - DESCRIPTION AND OPERATION
TASK 54-50-00-00-13
PYLONS - DESCRIPTION AND OPERATION
TASK 54-50-00-00-21
PYLONS - DESCRIPTION AND OPERATION
3. Job Set-up
Subtask 10-30-00-660-053-A ** ON A/C NOT FOR ALL
A. Cold Weather Conditions
   (1) If the aircraft is in cold weather conditions during the return-to-operation of the aircraft, do the cold-weather maintenance procedures.
     (a) It is not necessary to do all the steps given in the cold-weather maintenance procedures. Use your experience and your knowledge of the local weather conditions to do only the necessary steps for the inspections and/or tests:
Subtask 10-30-00-660-053-B ** ON A/C NOT FOR ALL
A. Cold Weather Conditions
   (1) If the aircraft is in cold weather conditions during the return-to-operation of the aircraft, do the cold-weather maintenance procedures.
     (a) It is not necessary to do all the steps given in the cold-weather maintenance procedures. Use your experience and your knowledge of the local weather conditions to do only the necessary steps for the inspections and/or tests:
Subtask 10-30-00-660-053-D ** ON A/C NOT FOR ALL
A. Cold Weather Conditions
   (1) If the aircraft is in cold weather conditions during the return-to-operation of the aircraft, do the cold-weather maintenance procedures.
     (a) It is not necessary to do all the steps given in the cold-weather maintenance procedures. Use your experience and your knowledge of the local weather conditions to do only the necessary steps for the inspections and/or tests:
Subtask 10-30-00-941-059-A
B. Safety Precautions
   (1) Put the ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position near the aircraft.
   (2) Open forward avionics-compartment access-door 811 (Ref. AMM TASK 52-41-00-010-002).
NOTE: This step is done to remove the remaining pressure in the cabin.
   (3) Put the WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the systems while you prepare the aircraft for operation again.
Subtask 10-30-00-860-062-A
C. Aircraft Maintenance Configuration
   (1) Return to service of Emergency Power Supply Units (EPSU):
     (a) If the EPSUs disconnection method was selected at the entry into parking, connect all the EPSUs batteries (Ref. AMM TASK 33-51-38-400-001).
NOTE: For EPSUs connection, only the steps related to the connection of EPSUs in the EPSU installation task are necessary.
     (b) If the EPSUs batteries removal method was selected at the entry into parking, install all the EPSUs batteries (Ref. AMM TASK 33-51-38-400-002).
   (2) Return to service of the batteries:
     (a) If method 1 (off-wing preservation) was selected:
       1 Install and connect batteries 2PB1 and 2PB2 (Ref. AMM TASK 24-38-51-400-001).
       2 Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
or
     (b) If method 2 (on-wing preservation) was selected:
       1 If battery Saft Part Number (P/N) 2758 is installed:
         a If you did the last regular check of the battery more than 6 months ago:
         b If you did the last regular check of the battery less than 6 months ago, do the return to service of the battery (Ref. AMM TASK 24-38-00-550-801).
NOTE: The energization of the aircraft electrical circuits is done in the (Ref. AMM TASK 24-38-00-550-801).
       2 If battery Saft P/N 416526 is installed, do the return to service of the battery (Ref. AMM TASK 24-38-00-550-801).
NOTE: The energization of the aircraft electrical circuits is done in the (Ref. AMM TASK 24-38-00-550-801).
   (3) On the CABIN PRESS section of panel 25VU:
  • Make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).
  • Release the DITCHING pushbutton switch (the ON legend goes off) to open the avionics ventilation skin-valves and the outflow valve.
   (4) Remove the WARNING NOTICE(S) from the ELEC section of panel 35VU.
   (5) If the first aid kits and the medical/doctors kit were removed during the cold-weather maintenance procedures:
     (a) Remove the WARNING NOTICE(S) installed at the removal of the first aid kits and the medical/doctors kit.
NOTE: For the location of the first aid kits and the medical/doctors kit (Ref. AMM D/O 25-64-00-00).
     (b) Install the first aid kits and the medical/doctors kit in the aircraft.
   (6) Return to service of the Electronic Module Assemblies (EMA) of the airbag system of the passenger seats:
NOTE: This step is only applicable to the ”AMSAFE” supplier EMA Part Number (P/N) 511959-XXX-XX, 513766-XXX-XX and 514518-XXX-XX.
     (a) If the aircraft parking period was less than 1 month, do the operational check of the airbag system by EMA Push-to-Test (PTT) procedure (Ref. AMM D/O 25-21-00-71).
     (b) If the aircraft parking period was more than 1 month:
       1 If these EMAs were removed, install them (Ref. AMM D/O 25-21-58-40).
       2 If these EMAs stay connected, do the operational check of the airbag system by EMA PTT procedure (Ref. AMM D/O 25-21-00-71).
4. Procedure
Subtask 10-30-00-210-082-A
A. General Visual Inspection (GVI)
   (1) Do a GVI of the airframe to find the Foreign Object Damage (FOD), bird nests, fluid leakage (hydraulic fluid, fuel or oil) from:
     (a) The top and bottom surfaces of the wings
     (b) The external surfaces of the fuselage
     (c) The center wing box in the lower fuselage
     (d) The landing gears
     (e) The horizontal and vertical stabilizers
     (f) The external skin, door frames and external handles of:
  • The passenger/crew doors
  • The cargo doors.
     (g) The drains in the lower fuselage.
   (2) If you find corrosion, remove it (Ref. AMM TASK 51-74-11-300-001).
   (3) If necessary, clean the aircraft externally (Ref. AMM TASK 12-21-11-615-002).
Subtask 10-30-00-210-086-A ** ON A/C NOT FOR ALL
B. Check of the Pylons Drains
CAUTION: WHEN YOU REMOVE THE ALUMINIUM-FOIL ADHESIVE FILM-TAPE 05RAB9, BE CAREFUL NOT TO CAUSE DAMAGE TO THE PAINT. THIS TAPE HAS A HIGH ADHESION CAPACITY.
   (1) If the aircraft parking period was less than 15 days:
     (a) Remove the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) from the engine drain masts and the pylons drains.
NOTE: For the location of the pylons drains (Ref. AMM D/O 54-50-00-00).
       1 If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
         a Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
         b Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
     (b) If the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) were not installed on the engine drain masts and the pylons drains at the entry into the parking period:
   (2) If the aircraft parking period was more than or equal to 15 days:
     (a) If installed, remove the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) from the engine drain masts and the pylons drains.
NOTE: For the location of the pylons drains (Ref. AMM D/O 54-50-00-00).
       1 If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
         a Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
         b Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
     (b) Do a check of the drains on the pylons (Ref. AMM TASK 54-50-00-200-002).
Subtask 10-30-00-210-086-C ** ON A/C NOT FOR ALL
B. Check of the Pylons Drains
CAUTION: WHEN YOU REMOVE THE ALUMINIUM-FOIL ADHESIVE FILM-TAPE 05RAB9, BE CAREFUL NOT TO CAUSE DAMAGE TO THE PAINT. THIS TAPE HAS A HIGH ADHESION CAPACITY.
   (1) If the aircraft parking period was less than 15 days:
     (a) Remove the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) from the engine drain masts and the pylons drains.
NOTE: For the location of the pylons drains (Ref. AMM D/O 54-50-00-00).
       1 If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
         a Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
         b Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
     (b) If the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) were not installed on the engine drain masts and the pylons drains at the entry into the parking period:
   (2) If the aircraft parking period was more than or equal to 15 days:
     (a) If installed, remove the FINE NYLON NETTING and the Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) or Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) from the engine drain masts and the pylons drains.
NOTE: For the location of the pylons drains (Ref. AMM D/O 54-50-00-00).
       1 If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
         a Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
         b Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
     (b) Do a check of the drains on the pylons (Ref. AMM TASK 54-50-00-200-803).
Subtask 10-30-00-420-074-A
C. Installation of the Removed Equipment
   (1) If the portable fire-extinguisher bottles were removed, install them.
   (2) If the lavatory fire-extinguisher bottles were removed, install them (Ref. AMM TASK 26-25-41-400-001) (Ref. AMM TASK 26-25-41-400-802) (Ref. AMM TASK 26-25-41-400-803) (Ref. AMM TASK 26-25-41-400-805) (Ref. AMM D/O 26-25-41-40).
   (3) Printer:
     (a) If the printer was removed, install it (Ref. AMM TASK 31-35-22-400-001).
     (b) If you let the printer installed and if the Outside Air Temperature (OAT) is more than or equal to 30 DEG.C (86 DEG.F) and if the outside air humidity is more than or equal to 80% during the parking period:
  • Make sure that the circuit breaker 6TW is closed.
  • Let the aircraft energized for 30 minutes.
  • Do an operational test of the printer (Ref. AMM TASK 31-35-00-710-001).
Subtask 10-30-00-210-091-A ** ON A/C NOT FOR ALL
D. Inspection of the Fire Protection System
   (1) If the lavatory fire-extinguisher bottles were not removed during the parking period, do a check of the pressure of the lavatory fire-extinguisher bottles for signs of leakage/discharge (Ref. AMM TASK 26-25-00-200-002).
   (2) If the portable fire-extinguisher bottles were not removed during the parking period, do a check of all the portable fire-extinguisher bottles (Ref. AMM TASK 26-24-00-210-001).
   (3) If the aircraft parking period was more than 1 month, do a check of the engine fire-extinguishing distribution-piping (Ref. AMM TASK 26-21-00-720-003).
Subtask 10-30-00-210-091-B ** ON A/C NOT FOR ALL
D. Inspection of the Fire Protection System
   (1) If the lavatory fire-extinguisher bottles were not removed during the parking period, do a check of the pressure of the lavatory fire-extinguisher bottles for signs of leakage/discharge (Ref. AMM TASK 26-25-00-200-002).
   (2) If the portable fire-extinguisher bottles were not removed during the parking period, do a check of all the portable fire-extinguisher bottles (Ref. AMM TASK 26-24-00-210-001).
   (3) If the aircraft parking period was more than 1 month, do a check of the engine fire-extinguishing distribution-piping (Ref. AMM TASK 26-21-00-720-802).
Subtask 10-30-00-210-081-A
E. Inspection of the Landing Gears
   (1) Do an inspection of the MLG shock absorbers before flight (Ref. AMM TASK 12-14-32-200-001).
   (2) Do a check of the NLG shock absorber bottoming (Ref. AMM TASK 12-14-32-200-002).
   (3) Do a check of the tire pressure (Ref. AMM TASK 32-41-00-210-003).
   (4) If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Do a check of the tire and wheel condition (Ref. AMM TASK 32-41-00-210-002).
     (b) Make sure that the charge pressure of the landing-gear shock absorbers is correct:
Subtask 10-30-00-210-083-A
F. Inspection of the Hydraulic System
   (1) If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Do a check of the hydraulic-reservoir fluid level:
       1 If the hydraulic fluid level is low:
       2 If the hydraulic fluid level is too high:
Subtask 10-30-00-670-055-A
G. Disinfection of the Potable Water System (PWS)
   (1) The parking period is completed and the aircraft can return-to-service:
   (2) The parking period is not completed and extended with a non-revenue flight:
  • If the PWS is not used during the non-revenue flight, it is not necessary to do the disinfection of the PWS.
Subtask 10-30-00-710-168-A
H. Operational Test of the Water/Waste Systems
   (1) The parking period is completed and the aircraft can return-to-service:
     (a) If the aircraft was parked for more than 1 month:
       1 Do the operational test of the potable water-distribution system (Ref. AMM TASK 38-12-00-710-001) or (Ref. AMM TASK 38-12-00-710-002).
       2 Do the operational test of the toilet unit (Ref. AMM TASK 38-31-00-710-009).
   (2) The parking period is not completed and extended with a non-revenue flight:
     (a) If the PWS is not used during the non-revenue flight, it is not necessary to do the operational test of the potable water-distribution system.
     (b) If the toilet system is not used during the non-revenue flight, it is not necessary to do the operational test of the toilet unit.
Subtask 10-30-00-281-056-A
CAUTION: IF A RESULT OF THE MICROBIOLOGICAL CONTAMINATION TESTS IS HEAVY, YOU MUST REMOVE CONTAMINATION FROM ALL THE TANKS BEFORE THE RETURN TO SERVICE OF THE AIRCRAFT.
I. Protection of the Fuel System from Microbiological Contamination
NOTE: Because microbiological contamination can expand in one tank or expand from tank to tank during routine fuel transfers, tests and protective treatments are necessary for all the fuel tanks.
   (1) Fuel sampling:
Fuel sampling is only applicable if the aircraft parking period was more than 1 month.
(a) If you did a microbiological contamination analysis at each water drain valve in a period of 15 days before the return-to-service of the aircraft:
(b) If you did not do a microbiological contamination analysis at each water drain valve in a period of 15 days before the return-to-service of the aircraft:
  • Do a fuel sampling for microbiological contamination analysis (Ref. AMM TASK 12-32-28-281-003).
    If you did the refueling procedure, do the fuel sampling procedure a minimum of one hour after the end of the refueling procedure.
  • Wait for the results of the contamination analysis and do the steps of (Ref. AMM TASK 12-32-28-281-003) related to these results before the next flight.
   (2) Water draining:
  • Do the water draining procedure a minimum of one hour after the end of the refueling procedure.
   (3) If you found a fuel leak during the GVI of the airframe, (Ref. AMM TASK 28-11-00-280-002).
Subtask 10-30-00-710-164-A
J. EPSU Battery
   (1) If the EPSU batteries removal method was selected at the start of the parking period or if the EPSU batteries stay connected for a period of 7 days or less, no test is necessary.
   (2) If the EPSUs disconnection method was selected at the start of the parking period:
     (a) Let the aircraft energized for a minimum of 30 minutes to recharge the EPSU batteries.
     (b) Do a check of the cabin emergency lights and signs for correct illumination (Ref. AMM TASK 33-51-00-710-009).
     (c) Do a test of the EPSU (Ref. AMM TASK 33-51-00-710-001) or (Ref. AMM TASK 33-51-00-710-006).
Subtask 10-30-00-720-051-A
K. Functional Test of the Rain Repellent System (If Installed)
   (1) If the aircraft parking period was more than 1 month, do the functional test of the rain repellent system (Ref. AMM TASK 30-45-00-720-002).
Subtask 10-30-00-640-050-A ** ON A/C NOT FOR ALL
L. Lubrication of the Cargo Door Seals
NOTE: You can ignore these steps if the inspection of doors was done during the parking periodic ground-checks at 3-month intervals before the non-revenue flight.
   (1) If the aircraft parking period was more than 1 month:
     (a) Lubricate the forward and aft cargo-compartment door-seals (Ref. AMM TASK 12-22-52-640-017).
     (b) If the bulk cargo-compartment door is installed, lubricate the bulk cargo-compartment door-seal (Ref. AMM TASK 12-22-52-640-018).
Subtask 10-30-00-720-050-A ** ON A/C NOT FOR ALL
M. Functional Test of the Doors
NOTE: You can ignore these steps if the Inspection of Doors was done during the PARKING periodic ground checks at 3 month interval before the Non-revenue Flight.
   (1) If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Open and close all the access doors to the pressurized area and make sure that they operate correctly:
Subtask 10-30-00-720-050-B ** ON A/C NOT FOR ALL
M. Functional Test of the Doors
NOTE: You can ignore these steps if the Inspection of Doors was done during the PARKING periodic ground checks at 3 month interval before the Non-revenue Flight.
   (1) If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Open and close all the access doors to the pressurized area and make sure that they operate correctly:
Subtask 10-30-00-720-050-C ** ON A/C NOT FOR ALL
M. Functional Test of the Doors
NOTE: You can ignore these steps if the Inspection of Doors was done during the PARKING periodic ground checks at 3 month interval before the Non-revenue Flight.
   (1) If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Open and close all the access doors to the pressurized area and make sure that they operate correctly:
Subtask 10-30-00-210-094-A
N. Inspection of the Cockpit Windows
   (1) If the aircraft parking period was more than 1 month:
     (a) Do a check of the opening and closing of the sliding windows.
Make sure that:
  • The applied load on the handle is correct,
  • The red indicator is visible on the button of the handle when the sliding window is closed.
NOTE: To check correct opening, closing, locking and to measure the applied load (Ref. AMM TASK 56-12-11-400-001).
Subtask 10-30-00-710-172-A
DELETED
Subtask 10-30-00-630-061-A ** ON A/C NOT FOR ALL
P. De-preservation of the Engines and the APU
NOTE: ATA 10 gives instructions related to the parking, storage, periodic checks and return to operation of the aircraft. These instructions do not include the engine and the APU.
For the parking, storage, periodic checks and return to operation of the engines and the APU, ATA 10 refers to the applicable procedures in the related ATA chapters (7X and 49).
   (1) APU de-preservation:
     (a) Remove the protection equipment from the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the APU open areas.
     (c) Do the applicable APU de-preservation procedure before you start the APU (in relation to the APU preservation procedure that you selected):
   (2) Engine de-preservation:
     (a) Remove all the protection equipment from the probes and sensors, the engines and the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the engine open areas.
     (c) Do the applicable engine de-preservation procedure before you start the engine (in relation to the engine preservation procedure that you selected) (Ref. AMM TASK 71-00-00-630-802).
Subtask 10-30-00-630-061-C ** ON A/C NOT FOR ALL
P. De-preservation of the Engines and the APU
NOTE: ATA 10 gives instructions related to the parking, storage, periodic checks and return to operation of the aircraft. These instructions do not include the engine and the APU.
For the parking, storage, periodic checks and return to operation of the engines and the APU, ATA 10 refers to the applicable procedures in the related ATA chapters (7X and 49).
   (1) APU de-preservation:
     (a) Remove the protection equipment from the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the APU open areas.
     (c) Do the applicable APU de-preservation procedure before you start the APU (in relation to the APU preservation procedure that you selected):
   (2) Engine de-preservation:
     (a) Remove all the protection equipment from the probes and sensors, the engines and the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the engine open areas.
     (c) Do the applicable engine de-preservation procedure before you start the engine (in relation to the engine preservation procedure that you selected) (Ref. AMM TASK 72-00-00-600-028).
Subtask 10-30-00-630-061-E ** ON A/C NOT FOR ALL
P. De-preservation of the Engines and the APU
NOTE: ATA 10 gives instructions related to the parking, storage, periodic checks and return to operation of the aircraft. These instructions do not include the engine and the APU.
For the parking, storage, periodic checks and return to operation of the engines and the APU, ATA 10 refers to the applicable procedures in the related ATA chapters (7X and 49).
   (1) APU de-preservation:
     (a) Remove the protection equipment from the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the APU open areas.
     (c) Do the applicable APU de-preservation procedure before you start the APU (in relation to the APU preservation procedure that you selected):
   (2) Engine de-preservation:
     (a) Remove all the protection equipment from the probes and sensors, the engines and the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the engine open areas.
     (c) Do the applicable engine de-preservation procedure before you start the engine (in relation to the engine preservation procedure that you selected) (Ref. AMM TASK 72-00-00-600-027).
Subtask 10-30-00-630-061-F ** ON A/C NOT FOR ALL
P. De-preservation of the Engines and the APU
NOTE: ATA 10 gives instructions related to the parking, storage, periodic checks and return to operation of the aircraft. These instructions do not include the engine and the APU.
For the parking, storage, periodic checks and return to operation of the engines and the APU, ATA 10 refers to the applicable procedures in the related ATA chapters (7X and 49).
   (1) APU de-preservation:
     (a) Remove the protection equipment from the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the APU open areas.
     (c) Do the applicable APU de-preservation procedure before you start the APU (in relation to the APU preservation procedure that you selected):
   (2) Engine de-preservation:
     (a) Remove all the protection equipment from the probes and sensors, the engines and the APU areas (Ref. AMM TASK 10-11-00-555-014).
     (b) Make sure that there is no FOD in the engine open areas.
     (c) Do the applicable engine de-preservation procedure before you start the engine (in relation to the engine preservation procedure that you selected) (Ref. AMM TASK 71-00-00-550-011).
Subtask 10-30-00-710-165-A ** ON A/C NOT FOR ALL
Q. Operational Tests of the Ice-Protection System and the Bleed Air System
   (1) Ice-protection system
If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Do the operational test of the engine-air-intake ice-protection system (Ref. AMM TASK 30-21-00-710-002).
     (b) Do the operational test of the wing ice-protection system (Ref. AMM TASK 30-11-00-710-001).
   (2) Bleed air system
     (a) If the aircraft was parked for less than or equal to 15 days, no test of the bleed system is necessary.
     (b) If the aircraft was parked for more than 15 days but less than or equal to 30 days, do the operational test of the bleed air system at idle engine rating (Ref. AMM TASK 36-11-00-710-804).
     (c) If the aircraft was parked for more than 30 days, do the operational test of the bleed air system (Ref. AMM TASK 36-11-00-710-802).
Subtask 10-30-00-710-165-C ** ON A/C NOT FOR ALL
Q. Operational Tests of the Ice-Protection System and the Bleed Air System
   (1) Ice-protection system
If the aircraft parking period was more than 1 month, do the steps that follow:
     (a) Do the operational test of the engine-air-intake ice-protection system (Ref. AMM TASK 30-21-00-710-002).
     (b) Do the operational test of the wing ice-protection system (Ref. AMM TASK 30-11-00-710-001).
   (2) Bleed air system
     (a) If the aircraft was parked for less than or equal to 15 days, no test of the bleed system is necessary.
     (b) If the aircraft was parked for more than 15 days but less than or equal to 30 days, do the operational test of the bleed air system at idle engine rating (Ref. AMM TASK 36-11-00-710-806).
     (c) If the aircraft was parked for more than 30 days, do the operational test of the bleed air system (Ref. AMM TASK 36-11-00-710-003).
Subtask 10-30-00-210-084-A
R. Inspection of the Probes and the Sensors
   (1) If not already removed, remove all the protection equipment from all the probes and the sensors (Ref. AMM TASK 10-11-00-555-014).
   (2) Do the inspection procedure of the sensors/probes:
   (3) If the aircraft parking period was more than 1 month, do a check of the insulation resistance of the pitot probe heater (Ref. AMM TASK 30-31-00-720-001).
   (4) Install the protection equipment on the probes and the sensors (Ref. AMM TASK 10-11-00-555-013).
NOTE: The protection on the probes and the sensors prevents FOD in the probes and the sensors before the next flight.
Subtask 10-30-00-170-052-A ** ON A/C NOT FOR ALL
S. Flushing of the Air Data System (ADS)
NOTE: You must do the air data flushing at the latest of the return-to-service procedure to decrease the time before the flight and prevents FOD in the air data pipes before the next flight.
   (1) Conditions for flushing
You must only flush the related ADS(s) for which one or more of these conditions apply:
  • The aircraft was in parking for more than 1 month and the last flushing of the ADS occurred more than 1 month.
  • All the probe covers were not installed immediately after the last flushing of the ADS.
  • All the probe covers were not installed immediately after the last flight of the aircraft.
  • There was a report of air data problems during the last flight of the aircraft.
  • The aircraft was operated or parked in very bad weather conditions (dust storm or sand storm or snow storm or heavy rain) or in a atmosphere with haze (foreign material can collect in the lines).
  • A probe cover was not found in position during all the periodic ground check.
  • A probe cover was not found in position at the time of the return to operation.
  • There is water, sand or dust on the static and pitot probes when you remove the protection equipment.
   (2) If one of these conditions occurs, you must flush the related ADS.
     (a) Flush the total pressure line of the Air Data Module (ADM) (Ref. AMM TASK 34-10-00-170-001).
     (b) Flush the static pressure line of the ADM (Ref. AMM TASK 34-10-00-170-002).
     (c) Drain and flush the standby pneumatic circuit of the ADM (Ref. AMM TASK 34-10-00-170-003).
   (3) Install the protection equipment on the probes and the sensors (Ref. AMM TASK 10-11-00-555-013).
NOTE: The protection on the probes and the sensors prevents FOD in the probes and the sensors before the next flight.
Subtask 10-30-00-170-052-B ** ON A/C NOT FOR ALL
S. Flushing of the Air Data System (ADS)
NOTE: You must do the air data flushing at the latest of the return-to-service procedure to decrease the time before the flight and prevents FOD in the air data pipes before the next flight.
   (1) Conditions for flushing
You must only flush the related ADS(s) for which one or more of these conditions apply:
  • The aircraft was in parking for more than 1 month and the last flushing of the ADS occurred more than 1 month.
  • All the probe covers were not installed immediately after the last flushing of the ADS.
  • All the probe covers were not installed immediately after the last flight of the aircraft.
  • There was a report of air data problems during the last flight of the aircraft.
  • The aircraft was operated or parked in very bad weather conditions (dust storm or sand storm or snow storm or heavy rain) or in a atmosphere with haze (foreign material can collect in the lines).
  • A probe cover was not found in position during all the periodic ground check.
  • A probe cover was not found in position at the time of the return to operation.
  • There is water, sand or dust on the static and pitot probes when you remove the protection equipment.
   (2) If one of these conditions occurs, you must flush the related ADS.
     (a) Flush the total pressure line of the Air Data Module (ADM) (Ref. AMM TASK 34-10-00-170-001).
     (b) Flush the static pressure line of the ADM (Ref. AMM TASK 34-10-00-170-002).
     (c) Drain and flush the standby static and standby total pressure-lines of the ADM (Ref. AMM TASK 34-22-25-170-001).
   (3) Install the protection equipment on the probes and the sensors (Ref. AMM TASK 10-11-00-555-013).
NOTE: The protection on the probes and the sensors prevents FOD in the probes and the sensors before the next flight.
5. Close-up
Subtask 10-30-00-280-055-A
A. Checklist
   (1) Do the checklist for the return to operation after a parking period (Ref. AMM TASK 10-30-00-280-803).
Subtask 10-30-00-942-053-B
B. Close-up
   (1) Make sure that the 98D29208246000 SAFETY DEVICE-RAT or 98D29208246001 DEVICE-SAFETY,RAT is removed (Ref. AMM TASK 29-22-00-860-008).
   (2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (3) Remove the WARNING NOTICE(S) from the cockpit.
   (4) Close forward avionics-compartment access-door 811 (Ref. AMM TASK 52-41-00-410-002).
   (5) Make sure that all the access doors and panels opened during this procedure are closed.
   (6) Make sure that all the external connections (external power supply, etc.) are disconnected from the aircraft. This does not include the aircraft grounding (earthing) cable.
   (7) Remove the access platform(s).
   (8) Remove all the fixtures, tools, test and support equipment used during this procedure.
[Rev.10 from 2021] 2026.04.01 04:24:22 UTC
"Aviabrain" 2025