W DOC AIRBUS | AMM A320F

Return to Operation After a Storage Period

TASK 10-30-00-554-005-A
Return to Operation After a Storage 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: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
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).
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. Reason for the Job
This procedure gives the instructions necessary for the return-to-operation of the aircraft after a storage 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 storage period.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
2
ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE
No specific
1
ACCESS PLATFORM 4M (13 FT)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
3
SPATULA - NON METALLIC
No specific
AR
WARNING NOTICE(S)
98D27403500000
2
PITCH TRIM CONTROL LOCKING
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
98D27903500000
2
PIN-SIDE STICK LOCKING
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.02ABA1)
Phosphate Ester Hydraulic Fluid-General Power - -
(Material No.03GBC1)
Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. -
(Material No.03HBD9)
Synthetic Ester base Grease-General Purpose Low Temp -
(Material No.05RAB9)
Adhesive Film Tape-- Aluminium Foil -
(Material No.05RNN1)
Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv -
(Material No.12AGC2)
Corrosion Preventive Compound-- Soft Film System
(Material No.14HMB1)
Film-- Waterproof Barrier -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
197CB, 197EB, 198CB, 312AR
 D. 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 10-30-00-280-802-A
Checklist for the Return to Operation After a Storage Period
TASK 12-13-27-612-002-A
Replenish PCU Gearbox to Confirm Fluid Level
TASK 12-13-27-612-003-A
Oil Replenishment of the Slat PCU Gearbox
TASK 12-13-27-612-005-A
Drain and Refill Flap Actuator Assemblies with Semi-fluid
TASK 12-13-80-600-011-B
Drain and Replenish Oil System and Inspection of Starter Magnetic chip Detector
TASK 12-13-80-610-001-A
Drain and Replenish Oil System
TASK 12-13-80-610-001-C
Drain and Replenish Oil System
TASK 12-14-32-614-001-A
Nitrogen Filling of the Tires
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 12-22-27-640-003-A
Lubricate THS Actuator Ball Screw Nut
TASK 12-22-27-640-004-A
Lubricate all Carriage Rollers on all Flap Tracks
TASK 12-22-27-640-005-A
Lubricate Spoiler No 1 to 5 Actuator Attachments
TASK 12-22-27-640-006-A
Lubricate all Track Rollers and Pinions
TASK 12-22-27-640-007-A
Lubrication of THS Mechanical Control Chains and Rear Cable (Area of Tension Regulator) with Grease Mat.
TASK 12-22-27-640-008-A
Remove Flap Rotary Actuators Assemblies For Regreasing
TASK 12-22-27-640-803-A
Lubrication of Elevator Servocontrol Rod Eye End Bearing
TASK 12-22-27-640-804-A
Lubrication of Rudder Servocontrol Rod Eye End Bearing
TASK 12-22-27-640-805-A
Lubrication of THS Mechanical Control Chains and Rear Cable (Area of Tension Regulator) with Grease Mat.
TASK 12-22-32-640-001-A
Lubrication of Main Landing Gear and Doors
TASK 12-22-32-640-002-A
Lubrication of Nose Landing Gear and Doors
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 12-22-53-640-001-A
Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004 (or Grease Mat. No. 03HBD9)
TASK 12-22-53-640-002-A
Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-037 (or Grease Mat. No. 03GBC1)
TASK 12-22-55-640-001-A
Lubrication of Rudder Hinge Bearing No. 6 with Grease Mat. No. 04-004 (or Grease Mat. No. 03HBD9)
TASK 12-22-55-640-002-A
Lubrication of Rudder Hinge Bearing No. 6 with Grease MAT. No. 04-037 (or Grease MAT. No. 03GBC1)
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 12-32-29-281-001-A
Analyze Hydraulic Fluid
TASK 20-24-11-100-001-A
Cleaning and Protection of the Cables
TASK 20-24-12-200-001-A
Check of the Control Cables
TASK 20-24-12-200-003-A
Inspection of the Pulleys
TASK 21-21-41-920-002-A
DISCARD FILTER ELEMENTS OF RECIRCULATION SYSTEM
TASK 21-26-00-710-001-A
Operational Check of the Avionics Equipment Ventilation-System via MCDU
TASK 21-26-00-710-001-A-01
Operational Check of the Avionics Equipment Ventilation (without the CFDS)
TASK 21-28-00-720-003-A
Functional Test of the FWD Cargo-Compartment Ventilation-System
TASK 21-28-00-720-004-A
Functional Test of the AFT Cargo-Compartment Ventilation-System
TASK 23-61-00-200-001-A
Resistance Check from the Tip to the Retainer and Bonding Check from the Retainer to the Aircraft Structure
TASK 23-71-35-400-001-A
Installation of the Cockpit Voice Recorder (CVR)
TASK 24-21-00-550-001-A
Preservation/Storage/Depreservation of the Integrated Drive Generator (IDG)
TASK 24-21-00-550-002-A
Preservation/Storage/Depreservation of the Integrated Drive Generator (IDG)
TASK 24-21-00-550-803-A
Preservation/Storage/Depreservation of the Integrated Drive Generator (IDG)
TASK 24-21-00-600-040-A
Preservation/Storage/Depreservation of the Integrated Drive Generator (IDG)
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 25-65-32-400-001-A
Installation of the Portable Emergency Locator Transmitter (ELT)
TASK 25-65-35-400-001-A
Installation of the Emergency Locator Transmitter (ELT)
TASK 26-12-00-710-001-A
Operational Check of Loop/Squib
TASK 26-21-00-710-002-A
Operational Check of Engine-Bottle Low-Pressure Indicating-Circuit
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 26-21-41-400-001-A
Installation of the Engine Fire-Extinguisher Bottle
TASK 26-21-41-400-001-E
Installation of the Engine Fire-Extinguisher Bottle
TASK 26-22-00-210-001-A
Detailed Inspection of Distribution Piping
TASK 26-22-00-710-001-A
Operational Test of the APU Fire-Extinguishing Loop/Squib
TASK 26-22-00-710-003-A
Operational Check of Low Pressure Indicating Circuit
TASK 26-22-41-400-001-A
Installation of the Fire Extinguisher Bottle
TASK 26-23-00-200-001-A
Check of Fire-Extinguishing Lines for Leakage and Obstruction
TASK 26-23-00-200-004-A
Check of the Fire Extinguishing Lines of the Two Fire Extinguisher Bottles for Leakage and Blockage
TASK 26-23-00-710-001-A
Operational Test of the Cargo-Compartment Fire-Extinguishing System
TASK 26-23-41-400-004-A
Installation of the Cargo Fire-Extinguisher Bottle
TASK 26-23-41-400-004-B
Installation of the Cargo Fire-Extinguisher Bottle
TASK 26-23-42-400-001-A
Installation of the Cargo Fire-Extinguisher Bottle
TASK 26-24-00-210-001-A
Inspection/Check of the Portable Fire Extinguishers
TASK 26-25-00-200-005-A
Visual Check of Fire Extinguisher Bottle Pressure Reading
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 27-00-00-080-001-A
Removal of the Pitch-Trim Control Locking Tool (98D27403500000)
TASK 27-00-00-480-001-A
Installation of the Pitch-Trim Control Locking Tool (98D27403500000)
TASK 27-14-00-710-001-A
Operational Test of the Aileron and Hydraulic Actuation
TASK 27-24-00-710-002-A
Operational Test of the Rudder Servocontrols with Individual Hydraulic System
TASK 27-34-00-710-001-A
Operational Test of the Elevator and Hydraulic Actuation
TASK 27-44-00-710-002-A
Operational Test of the Trimmable Horizontal Stabilizer Actuator with the Individual Hydraulic Systems
TASK 27-44-51-210-004-A
Check Oil Level of THS Actuator Gearbox
TASK 27-50-00-866-008-A
Extension of the Flaps on the Ground
TASK 27-50-00-866-008-A-01
Extension of the Flaps/Slats on the Ground
TASK 27-50-00-866-009-A
Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01
Retraction of the Flaps/Slats on the Ground
TASK 27-54-00-200-001-A
Detailed Visual Inspection of the Transmission Assembly
TASK 27-54-00-710-002-A
Operational Test of the Flap and Slat Systems
TASK 27-54-49-000-008-A
Removal of the Flap Track 1 to 4 Actuators
TASK 27-54-49-400-005-A
Installation of the Flap Track 1 to 4 Actuators
TASK 27-64-00-710-001-A
Operational Test of the Spoiler Hydraulic Actuation
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 27-84-00-200-001-A
Detailed Visual Inspection of the Slat Transmission System
TASK 28-11-00-280-002-A
Structural Fuel Tank Leaks - General Information
TASK 28-23-00-720-001-A
Operational Check of Crossfeed Valve Using Individual Motors and Check Fuel Flow in "Open" and Fuel Shut Off in "Closed" Positions
TASK 28-24-00-710-002-A
Operational Test of the ENG 1(2) LP Fuel Valve
TASK 28-29-00-710-001-A
Operational Test of the APU Low Pressure Fuel Valve using each individual Motor in turn
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 29-10-00-210-002-A
Check Clogging Indicators on Return, Case Drain, Ground Servicing, HP Delivery, HP Bleed Air and LP Bleed Air, Water Separator Filters and Reservoir Pressurization Filter
TASK 29-10-00-710-001-A
Operational Check of Hydraulic Fire Shut Off Valves and Associated Indicating System
TASK 29-10-00-864-001-A
Depressurize the Green Hydraulic System
TASK 29-10-00-864-002-A
Depressurize the Yellow Hydraulic System
TASK 29-10-00-864-003-A
Depressurize the Blue Hydraulic System
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 30-42-00-710-001-A
Operational Test of the Windshield Anti-Icing and Defogging
TASK 30-45-00-440-002-A
Reactivation of the Rain Repellent System
TASK 30-45-00-720-001-A
Functional Test of the Windshield Rain Protection
TASK 30-45-52-400-002-A
Installation of the Wiper Arm
TASK 30-45-53-400-001-A
Installation of the Wiper Blade
TASK 31-21-00-750-002-A
Procedure to Set the Clock
TASK 31-33-55-400-002-A
Installation of the Digital Flight Data Recorder (DFDR)
TASK 31-35-22-400-001-A
Installation of the Printer
TASK 31-39-33-400-801-A
Installation of the Cockpit Voice and Data Recorder (CVDR) and the Umbrella Panels
TASK 32-11-00-200-001-A
General Visual Inspection of the Main Landing Gear
TASK 32-21-00-200-002-A
General Visual Inspection of the Nose Landing Gear
TASK 32-31-00-720-002-A
Functional Test of the Normal Extension and Retraction of the Landing Gear
TASK 32-33-00-720-001-A
Functional Check of Free-Fall Extension
TASK 32-40-00-200-001-A
Inspection/Check of Brake System
TASK 32-41-00-210-002-A
Inspection/Check of the Wheels and Tires
TASK 32-41-11-000-006-A
Removal of the MLG Wheel
TASK 32-41-11-400-006-A
Installation of the MLG Wheel
TASK 32-41-12-000-001-A
Removal of the NLG Wheel
TASK 32-41-12-400-001-A
Installation of the NLG Wheel
TASK 32-42-00-710-001-A
Operational Check of the Normal Braking System
TASK 32-43-00-710-001-A
Operational Check of Alternate Braking System
TASK 32-44-11-200-001-A
Functional Check of Parking/Emergency Brake Accumulator by Reading the Charge Pressure on the Accumulator Gauge
TASK 32-45-00-710-001-A
Operational Check of the Parking Brake System
TASK 32-45-00-720-002-A
Functional Check of the Brake Accumulator System with the Parking Brake Applied
TASK 32-46-00-740-005-A
BITE Test of BSCU - Normal Braking TEST
TASK 32-48-51-400-005-A
Installation of the Fan Assy
TASK 32-51-00-720-003-A
Functional Test of the Nose Wheel Steering with the Handwheel
TASK 32-51-00-720-004-A
Functional Test of the Nose Wheel Steering with the Pedals
TASK 33-42-00-600-801-A
Lubrication of the Retractable Landing Lights
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 35-10-00-040-001-A
OXY High Pressure Indication-Direct Reading
TASK 35-12-41-710-001-A
Operational Check of Flight Crew Oxygen System
TASK 35-23-00-710-001-A
Operational Check of Manual Mask Release
TASK 35-30-00-210-006-A
Visual Check of the Tamper Seal/Serviceability Indication of the Protective Breathing Equipment
TASK 35-30-00-220-001-A
Detailed Inspection of Portable Oxygen Mask
TASK 35-32-42-210-001-A
Visual Check of Cylinder Attachments
TASK 35-32-42-210-002-A
Check Connecting Hose, Mask and Pressure on Cylinder Pressure Gauge
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 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 38-32-00-710-002-A
Operational Test of the Waste/Water Drain System
TASK 47-31-34-740-001-A
BITE Test of the IGGS with Bleed Air
TASK 47-31-34-740-001-A-01
BITE Test of the IGGS without Bleed Air
TASK 49-11-11-400-003-A
Installation of the Power Plant (APU) (APS 3200)
TASK 49-11-11-400-004-A
Installation of the Power Plant (APU) (131-9(A))
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 53-00-00-210-001-A
Remove and Detailed Inspection of Piston Type Drain Valves in Lower Fuselage Shell
TASK 53-39-00-210-001-A
Operational Check of Rubber Flap Drain Valve Holes in Pressure Floor from MLG Bay
TASK 53-59-00-210-001-A
Operational Check of Single Drain Pipe Aft of FR70 from Outside
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 55-13-11-000-001-A
Remove/Open of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
TASK 55-13-11-400-001-A
Install/Close of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
TASK 55-13-11-560-001-A
Preparation for Installation
TASK 55-33-13-010-002-A
Opening/Removal of the Trailing Edge Access-Panels of the Vertical Stabilizer
TASK 55-33-13-410-002-A
Closing/Installation of the Trailing Edge Access-Panels of the Vertical Stabilizer
TASK 56-12-11-200-001-A
Inspection of the Sliding Windows
TASK 56-12-11-220-002-A
Check of the Sliding Windows
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 71-00-00-400-040-A
Installation of the Power Plant
TASK 71-00-00-400-040-A-01
Installation of the Power Plant with the Engine Positioner TWW 75E
TASK 71-00-00-400-040-A-03
Installation of the Power Plant with Jacxson Tool
TASK 71-00-00-400-042-A
Installation of the Power Plant
TASK 71-00-00-400-042-A-01
Installation of the Power Plant with the Engine Positioner TWW 75E (MIAG)
TASK 71-00-00-400-042-A-03
Installation of the Power Plant with Jacxson Tool
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 71-00-00-710-003-A
Engine Automatic Start
TASK 71-00-00-710-003-B
Engine Automatic Start
TASK 71-00-00-710-004-A
Engine Manual Start
TASK 71-00-00-710-004-B
Engine Manual Start
TASK 71-00-00-710-006-A
Minimum Idle Check
TASK 71-00-00-710-006-B
Minimum Idle Check
TASK 71-00-00-710-012-B
Test No.3 : Idle Leak Check
TASK 71-00-00-710-018-A
Discontinued Start, Restart and Shutdown Procedures
TASK 71-00-00-710-028-A
Engine Shutdown
TASK 71-00-00-710-028-B
Engine Shutdown
TASK 71-00-00-710-043-A
Normal Engine Automatic-Start Procedure
TASK 71-00-00-710-047-A
Normal Engine Manual-Start Procedure
TASK 71-00-00-720-811-A
Test No. 3A - Idle Power Test
TASK 71-00-00-860-814-A
Shutdown of the Engine
TASK 71-00-20-400-040-A
Installation of the Power Plant
TASK 71-00-20-400-040-A-01
Installation of the Power Plant with the Engine Positioner TWW 75E (MIAG)
TASK 71-00-51-400-802-A
Installation of the Power Plant (Bootstrap Method)
TASK 71-00-51-400-802-A-01
Installation of the Power Plant (JacXson Method)
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 10-30-00-660-052-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 10-30-00-660-052-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 10-30-00-660-052-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 10-30-00-941-053-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 10-30-00-615-057-A
C. Removal of the Film Protection
   (1) If installed, remove the Film-- Waterproof Barrier - (Material No.14HMB1) from the cockpit and passenger seats.
   (2) Remove the protection from the carpets of the cabin aisles, cockpit and galley areas.
   (3) Remove all the Film-- Waterproof Barrier - (Material No.14HMB1) and the Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) or Adhesive Film Tape-Surface protection PVC film coated Pressure sensitive acrylic-based adhesiv - (Material No.05RNN1) .
     (a) If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
       1 Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
       2 Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
Do not remove the aircraft protective equipment from the engines, APU, probes and sensors at this step.
4. Procedure
Subtask 10-30-00-210-074-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 top surfaces of the ailerons and spoilers
     (c) The bottom surface of the ailerons
     (d) The nacelles, the leading edge of the nacelles and the pylons
     (e) The external surfaces of the fuselage
     (f) The Center Wing Box (CWB) in the lower fuselage
     (g) The landing gears
     (h) The flight control surfaces
     (i) The leading and trailing edges of the horizontal and vertical stabilizers
     (j) The external skin, door frames and external handles of:
  • The passenger/crew doors
  • The cargo doors
     (k) The toilet areas.
   (2) If you find corrosion, remove it (Ref. AMM TASK 51-74-11-300-001).
   (3) Make sure that:
  • The communication and navigation antennas are correctly installed
  • The static dischargers are correctly installed and in the correct condition (Ref. AMM TASK 23-61-00-200-001).
NOTE: In AMM reference task 23-61-00-200-001, only the steps related to the inspection of the static dischargers are applicable.
   (4) Do a GVI of the avionics compartment to find the FODs, scratches, marks, impacts or deformations, cracks, leaks (oil or hydraulic), paint, markings, fixing and condition of the various mechanisms and elements, pipes, cleanliness, connection of the electrical outlets and seals.
Subtask 10-30-00-420-067-A
B. Aircraft Configuration
   (1) Return to service of the Emergency Power Supply Units (EPSU):
     (a) If the EPSUs disconnection method was selected at the entry into storage, 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 storage, install all the EPSUs batteries (Ref. AMM TASK 33-51-38-400-002)
   (2) Install and connect batteries 2PB1 and 2PB2 (Ref. AMM TASK 24-38-51-400-001).
   (3) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (4) On overhead panel 25VU, on the CABIN PRESS section:
  • Release the DITCHING pushbutton switch (the ON legend goes off) to open the avionics ventilation skin-valves and the outflow valve.
  • Make sure that the avionics ventilation continues to operate correctly.
   (5) Remove the WARNING NOTICE(S) from the ELEC section of panel 35VU.
   (6) Make sure that you have set the clock (Ref. AMM TASK 31-21-00-750-002).
Subtask 10-30-00-615-051-A
C. Cleaning of the Aircraft
   (1) We recommend that you clean the aircraft externally (Ref. AMM TASK 12-21-11-615-002).
Subtask 10-30-00-640-051-A ** ON A/C NOT FOR ALL
D. Lubrication of the Cargo Door Seals
   (1) Lubricate the forward and aft cargo-compartment door-seals (Ref. AMM TASK 12-22-52-640-017).
   (2) If the bulk cargo-compartment door is installed, lubricate the bulk cargo-compartment door-seal (Ref. AMM TASK 12-22-52-640-018).
Subtask 10-30-00-710-118-A
E. Inspection of the Doors
   (1) Open and close all the access doors to the pressurized area and make sure that they operate correctly:
Subtask 10-30-00-210-085-A
F. Inspection of the Cockpit Windows
   (1) Do a check of the sliding windows (Ref. AMM TASK 56-12-11-220-002).
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 area is visible on the button of the handle.
NOTE: To measure the applied load on the handle (Ref. AMM TASK 56-12-11-400-001).
   (2) Do a check of the pressure seal integrity (Ref. AMM TASK 56-12-11-200-001).
   (3) Close the sliding windows.
   (4) Do the operational test with the Window Heat Computer (WHC) calculator to do a check of the integrity of the anti-ice system of the cockpit windows (Ref. AMM TASK 30-42-00-710-001).
Subtask 10-30-00-420-068-A ** ON A/C NOT FOR ALL
G. Installation of the Removed Equipment
   (1) If removed, install the Digital Flight Data Recorder (DFDR) (Ref. AMM TASK 31-33-55-400-002).
   (2) If removed, install the Cockpit Voice Recorder (CVR) (Ref. AMM TASK 23-71-35-400-001).
   (3) If removed, install the debris guard, the impeller and the shroud of the brake fans (Ref. AMM TASK 32-48-51-400-005).
   (4) Fire-extinguishing bottles:
     (a) If removed, install the portable fire-extinguishing bottles.
     (b) If removed, install the fire-extinguisher bottles and cartridges of:
   (5) If removed, install the batteries of:
  • The flashlights and make sure that they operate correctly
  • The megaphones and make sure that they operate correctly.
   (6) Install the Emergency Locator Transmitter (ELT):
   (7) 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.
   (8) If removed, install the wiper blades (Ref. AMM TASK 30-45-53-400-001) and the wiper arms (Ref. AMM TASK 30-45-52-400-002).
   (9) Do the operational test of the wiper arm at the low and high wiper speed with wet windows (Ref. AMM TASK 30-45-00-720-001).
   (10) If installed, do the reactivation of the rain repellent system (Ref. AMM TASK 30-45-00-440-002).
   (11) If the printer was removed during the storage period, install it (Ref. AMM TASK 31-35-22-400-001).
   (12) 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 these EMAs were removed during the storage period, install them (Ref. AMM D/O 25-21-58-40).
     (b) If these EMAs stay connected during the storage period, do the operational check of the airbag system by EMA Push-to-Test (PTT) procedure (Ref. AMM D/O 25-21-00-71).
Subtask 10-30-00-420-068-B ** ON A/C NOT FOR ALL
G. Installation of the Removed Equipment
   (1) Make sure that the Cockpit Voice and Data Recorders (CVDR) are installed (Ref. AMM TASK 31-39-33-400-801).
   (2) If removed, install the debris guard, the impeller and the shroud of the brake fans (Ref. AMM TASK 32-48-51-400-005).
   (3) Fire-extinguishing bottles:
     (a) If removed, install the portable fire-extinguishing bottles.
     (b) If removed, install the fire-extinguisher bottles and cartridges of:
   (4) If removed, install the batteries of:
  • The flashlights and make sure that they operate correctly
  • The megaphones and make sure that they operate correctly.
   (5) Install the Emergency Locator Transmitter (ELT):
   (6) 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.
   (7) If removed, install the wiper blades (Ref. AMM TASK 30-45-53-400-001) and the wiper arms (Ref. AMM TASK 30-45-52-400-002).
   (8) Do the operational test of the wiper arm at the low and high wiper speed with wet windows (Ref. AMM TASK 30-45-00-720-001).
   (9) If installed, do the reactivation of the rain repellent system (Ref. AMM TASK 30-45-00-440-002).
   (10) If the printer was removed during storage, install it (Ref. AMM TASK 31-35-22-400-001).
   (11) 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 these EMAs were removed during the storage period, install them (Ref. AMM D/O 25-21-58-40).
     (b) If these EMAs stay connected during the storage period, do the operational check of the airbag system by EMA Push-to-Test (PTT) procedure (Ref. AMM D/O 25-21-00-71).
Subtask 10-30-00-420-073-A ** ON A/C NOT FOR ALL
H. Installation of the removed APU and Engine
   (1) If removed, install the APU:
   (2) If removed, install the engine (Ref. AMM TASK 71-00-51-400-802).
Subtask 10-30-00-420-073-C ** ON A/C NOT FOR ALL
H. Installation of the removed APU and Engine
   (1) If removed, install the APU:
   (2) If removed, install the engine (Ref. AMM TASK 71-00-00-400-040).
Subtask 10-30-00-420-073-E ** ON A/C NOT FOR ALL
H. Installation of the removed APU and Engine
   (1) If removed, install the APU:
   (2) If removed, install the engine (Ref. AMM TASK 71-00-00-400-042).
Subtask 10-30-00-420-073-F ** ON A/C NOT FOR ALL
H. Installation of the removed APU and Engine
   (1) If removed, install the APU:
   (2) If removed, install the engine (Ref. AMM TASK 71-00-20-400-040).
Subtask 10-30-00-710-167-A
I. Inspection and test of EPSUs
   (1) If the EPSUs batteries removal method was selected at the start of the storage period, no test is necessary.
   (2) If the EPSUs disconnection method was selected at the start of the storage period:
     (a) Let the aircraft energized for a minimum of 30 minutes to recharge EPSUs batteries.
     (b) Do a check of cabin lights and signs for correct illumination (Ref. AMM TASK 33-51-00-710-009).
     (c) Do an operational test of emergency lights not with CIDS (Ref. AMM TASK 33-51-00-710-001) or (Ref. AMM TASK 33-51-00-710-006).
Subtask 10-30-00-210-092-A ** ON A/C NOT FOR ALL
J. Inspection and Operational Check of the Drains
   (1) Do a check of:
     (a) The drains in the lower fuselage:
       1 If you find blockage or FOD, remove it:
     (b) The drains on the CWB in the lower fuselage (Ref. AMM TASK 53-39-00-210-001).
     (c) The drains on the pylons:
       1 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).
         a If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
  • Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
  • Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
       2 Do a check of the drains on the pylons (Ref. AMM TASK 54-50-00-200-002).
     (d) Drain holes:
       1 Make sure that all drain holes that you can see are not clogged in the locations that follow:
  • The lower fuselage
  • The lower wing
  • The lower horizontal tail plane.
Subtask 10-30-00-710-120-B ** ON A/C NOT FOR ALL
K. Inspection and Test of the Fire Protection
   (1) Engine fire protection
     (a) Do a test of the engine fire-extinguishing system (Ref. AMM TASK 26-12-00-710-001).
     (b) Do a check of the engine fire-extinguishing distribution-piping (Ref. AMM TASK 26-21-00-720-003).
     (c) Do a check of the engine low-pressure indicating-circuit (Ref. AMM TASK 26-21-00-710-002).
   (2) APU fire protection
     (a) Do a test of the APU fire-extinguishing system (Ref. AMM TASK 26-22-00-710-001).
     (b) Do a check of the APU fire-extinguishing distribution-piping (Ref. AMM TASK 26-22-00-210-001).
     (c) Do a check of the APU low-pressure indicating-circuit (Ref. AMM TASK 26-22-00-710-003).
   (3) Cargo-compartment fire protection (if installed)
     (a) Do a test of the cargo-compartment fire-extinguishing system and low pressure indicating-system (Ref. AMM TASK 26-23-00-710-001).
     (b) Do a check of the cargo-compartment fire-extinguishing distribution-piping:
   (4) Lavatory fire protection (if installed)
     (a) Do a check of the fire-extinguisher bottle pressure (Ref. AMM TASK 26-25-00-200-005).
   (5) Portable fire extinguishing
     (a) Do a check of all the portable fire-extinguisher bottles (Ref. AMM TASK 26-24-00-210-001).
Subtask 10-30-00-210-092-C ** ON A/C NOT FOR ALL
L. Inspection and Operational Check of the Drains
   (1) Do a check of:
     (a) The drains in the lower fuselage:
       1 If you find blockage or FOD, remove it:
     (b) The drains on the CWB in the lower fuselage (Ref. AMM TASK 53-39-00-210-001).
     (c) The drains on the pylons:
       1 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).
         a If you used Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) :
  • Lift the edge of Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) with the SPATULA - NON METALLIC.
  • Lift Adhesive Film Tape-- Aluminium Foil - (Material No.05RAB9) and slowly pull it back at an angle of 45 degrees to remove it.
       2 Do a check of the drains on the pylons (Ref. AMM TASK 54-50-00-200-803).
     (d) Drain holes:
       1 Make sure that all drain holes that you can see are not clogged in the locations that follow:
  • The lower fuselage
  • The lower wing
  • The lower horizontal tail plane.
Subtask 10-30-00-710-120-C ** ON A/C NOT FOR ALL
M. Inspection and Test of the Fire Protection
   (1) Engine fire protection
     (a) Do a test of the engine fire-extinguishing system (Ref. AMM TASK 26-12-00-710-001).
     (b) Do a check of the engine fire-extinguishing distribution-piping (Ref. AMM TASK 26-21-00-720-802).
     (c) Do a check of the engine low-pressure indicating-circuit (Ref. AMM TASK 26-21-00-710-002).
   (2) APU fire protection
     (a) Do a test of the APU fire-extinguishing system (Ref. AMM TASK 26-22-00-710-001).
     (b) Do a check of the APU fire-extinguishing distribution-piping (Ref. AMM TASK 26-22-00-210-001).
     (c) Do a check of the APU low-pressure indicating-circuit (Ref. AMM TASK 26-22-00-710-003).
   (3) Cargo-compartment fire protection (if installed)
     (a) Do a test of the cargo-compartment fire-extinguishing system and low pressure indicating-system (Ref. AMM TASK 26-23-00-710-001).
     (b) Do a check of the cargo-compartment fire-extinguishing distribution-piping:
   (4) Lavatory fire protection (if installed)
     (a) Do a check of the fire-extinguisher bottle pressure (Ref. AMM TASK 26-25-00-200-005).
   (5) Portable fire extinguishing
     (a) Do a check of all the portable fire-extinguisher bottles (Ref. AMM TASK 26-24-00-210-001).
Subtask 10-30-00-710-121-A
N. Inspection and Test of the Oxygen System
   (1) Crew oxygen system
     (a) Crew oxygen cylinders
       1 Get access to avionics-compartment door 812.
       2 Open the cylinder hand valves slowly and fully.
       3 Do a check of the pressure of the crew oxygen cylinders (Ref. AMM TASK 35-10-00-040-001).
     (b) Do a test of the full face masks (Ref. AMM TASK 35-12-41-710-001).
   (2) Passenger oxygen system
     (a) Chemical emergency oxygen-system (if installed)
       1 Do an operational test of the passenger emergency oxygen-system (Ref. AMM TASK 35-23-00-710-001).
NOTE: The operational test of the manual mask release also contains the test of the decentralized gaseous oxygen-containers in the lavatories, (if installed).
     (b) Gaseous emergency oxygen-system with oxygen cylinders in the cargo hold (if installed)
       1 Open the manual shutoff valves of the passenger oxygen cylinders fully and very slowly.
       2 Do a check of the pressure of the passenger oxygen cylinders (Ref. AMM D/O 35-21-00-04).
If necessary, fill the passenger oxygen cylinders (Ref. AMM D/O 35-21-00-61).
       3 Do an operational check of the manual mask release (Ref. AMM TASK 35-23-00-710-001) (Ref. AMM D/O 35-23-00-71).
   (3) Portable oxygen devices
     (a) Portable oxygen cylinders (if installed)
       1 Do a check of the pressure of all the portable oxygen cylinders (Ref. AMM TASK 35-32-42-210-002).
       2 Do a visual inspection of the cylinder and the fasteners (Ref. AMM TASK 35-31-42-200-001).
       3 Do a detailed inspection of the portable oxygen mask (Ref. AMM TASK 35-30-00-220-001).
     (b) Protective breathing equipment
       1 Do a visual check of the tamper seal/serviceable indication of the protective breathing equipment (Ref. AMM TASK 35-30-00-210-006).
Subtask 10-30-00-710-132-C
O. Inspection and Operational Test of the Water/Waste Systems
   (1) If the aircraft was stored for more than 1 month, do the disinfection of the Potable Water System (PWS) (Ref. AMM TASK 38-10-00-670-002).
   (2) Do a test of the potable water-distribution system (Ref. AMM TASK 38-12-00-710-001) or (Ref. AMM TASK 38-12-00-710-002).
   (3) Do a test of the waste/water drain system (Ref. AMM TASK 38-32-00-710-002).
   (4) Do an operational test of the toilet unit (Ref. AMM TASK 38-31-00-710-009).
Subtask 10-30-00-710-122-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.
P. 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:
     (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) Drain water at each water drain valve:
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).
   (4) Do a test of the LP fuel shut-off-valve of the engine (Ref. AMM TASK 28-24-00-710-002).
   (5) Do a test of the APU shut-off valve (Ref. AMM TASK 28-29-00-710-001).
   (6) Do a test of the crossfeed valves (Ref. AMM TASK 28-23-00-720-001).
Subtask 10-30-00-710-123-A
Q. Inspection and Test of the Hydraulic System
   (1) Do a check of the hydraulic-reservoir fluid level:
     (a) If the hydraulic fluid level is low:
     (b) If the hydraulic fluid level is too high:
   (2) Read the maintenance record to find when the last hydraulic fluid sampling occurred (Ref. AMM TASK 12-32-29-281-001).
If the last hydraulic fluid sampling occurred more than 6 months, do an analysis of the hydraulic fluid (Ref. AMM TASK 12-32-29-281-001).
   (3) Do a test of the hydraulic shut-off valves (Ref. AMM TASK 29-10-00-710-001).
Subtask 10-30-00-710-124-A
R. Inspection and Test of the Landing Gears
   (1) Do a GVI of the NLG (Ref. AMM TASK 32-21-00-200-002).
   (2) Do a GVI of the MLG (Ref. AMM TASK 32-11-00-200-001).
   (3) Lubrication
     (a) Lubricate all the landing gears:
     (b) If the aircraft storage period was more than 6 months, do the lubrication of the retractable landing lights (Ref. AMM TASK 33-42-00-600-801).
   (4) Make sure that the charge pressure of the landing-gear shock absorbers is correct:
   (5) Clean all the actuator rods and apply a thin layer of Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
   (6) If the aircraft storage period was more than 4 months, do these tests:
   (7) Do a test of:
Subtask 10-30-00-710-125-A
S. Inspection and Operational Test of the Wheels and the Brakes
   (1) If the aircraft was in storage for more than 4 months:
     (a) Replace all the wheels of:
     (b) Do a GVI of the brakes (Ref. AMM TASK 32-40-00-200-001).
NOTE: It is not necessary to do the inspection of the parts that are replaced.
   (2) If the aircraft was in storage for not more than 4 months:
     (a) Put the tires back to the nominal pressure (Ref. AMM TASK 12-14-32-614-001).
     (b) Do a GVI of the wheels, the tires and the brakes (Ref. AMM TASK 32-41-00-210-002) and (Ref. AMM TASK 32-40-00-200-001) .
   (3) Install the debris guard, the impeller and the shroud of the brake fans (if removed during storage) (Ref. AMM TASK 32-48-51-400-005).
   (4) Do the tests that follow:
Subtask 10-30-00-710-119-A
T. Inspection and Test of the Ventilation System
   (1) Discard the recirculation filters (Ref. AMM TASK 21-21-41-920-002).
   (2) Do a test of the ventilation system of the avionics compartment (Ref. AMM TASK 21-26-00-710-001).
   (3) If the aft cargo-compartment ventilation-system is installed, do a test of the aft cargo-compartment ventilation-system (Ref. AMM TASK 21-28-00-720-004).
   (4) If the forward cargo-compartment ventilation-system is installed, do a test of the forward cargo-compartment ventilation-system (Ref. AMM TASK 21-28-00-720-003).
Subtask 10-30-00-710-134-A
U. Test of the Fuel-Tank Inerting System (FTIS) (if installed)
   (1) Do the BITE Test of the IGGS with Bleed Air (Ref. AMM TASK 47-31-34-740-001).
Subtask 10-30-00-710-128-A ** ON A/C NOT FOR ALL
V. Inspection and Operational Tests of the Flight Controls
   (1) Do the lubrication of:
   (2) Do a check of the condition of the flight control cables:
     (a) If the aircraft storage period is less than 6 months, it is not necessary to do a check of the rudder and THS cables.
     (b) If the aircraft storage period is more than 6 months, do a check of the rudder and THS cables in these areas (Ref. AMM TASK 20-24-12-200-001) and (Ref. AMM TASK 20-24-12-200-003):
  • The avionics compartment
  • The forward and aft cargo compartments
  • Between FR71 and the THS actuator and the rear rudder mechanical-control.
NOTE: It is necessary to move the cable on the pulley. There can be some corrosion that you cannot see because of the pulley guard or pulley guide.
       1 If there is corrosion on the cables or no protection with Corrosion Preventive Compound-- Soft Film System (Material No.12AGC2) or Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) or Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) :
         a Inspect the full length of the cables (Ref. AMM TASK 20-24-12-200-001) and (Ref. AMM TASK 20-24-12-200-003).
         b Clean and put a protection on the full length of the cables (Ref. AMM TASK 20-24-11-100-001).
   (3) Do a detailed inspection of the flap transmission assembly (Ref. AMM TASK 27-54-00-200-001).
   (4) Do a detailed inspection of the slat transmission system (Ref. AMM TASK 27-84-00-200-001).
   (5) If the aircraft storage period is more than 5 years:
   (6) Do a check of the fluid level of the Power Control Unit (PCU) of the flaps. If necessary, fill the PCU with oil (Ref. AMM TASK 12-13-27-612-002).
   (7) Do a check of the fluid level of the PCU of the slats. If necessary, fill the PCU with oil (Ref. AMM TASK 12-13-27-612-003).
   (8) Do the oil level check of the gearbox of the THS actuator (Ref. AMM TASK 27-44-51-210-004).
   (9) Do a test of the spoiler hydraulic control (Ref. AMM TASK 27-64-00-710-001).
   (10) Do a test of the aileron and its hydraulic control (Ref. AMM TASK 27-14-00-710-001).
   (11) Do a test of the elevator and its hydraulic control (Ref. AMM TASK 27-34-00-710-001).
   (12) Do a test of the rudder hydraulic actuation (Ref. AMM TASK 27-24-00-710-002).
   (13) Do a test of the THS actuator with the individual hydraulic systems (Ref. AMM TASK 27-44-00-710-002).
Move the THS pitch-trim control-wheel back to the 2 UP position.
   (14) Do a test of the flap and slat system (Ref. AMM TASK 27-54-00-710-002). Operate the flap and the slat system a minimum of ten times.
Subtask 10-30-00-710-128-B ** ON A/C NOT FOR ALL
V. Inspection and Operational Tests of the Flight Controls
   (1) Do the lubrication of:
   (2) Do a check of the condition of the flight control cables:
     (a) If the aircraft storage period is less than 6 months, it is not necessary to do a check of the rudder and THS cables.
     (b) If the aircraft storage period is more than 6 months, do a check of the rudder and THS cables in these areas (Ref. AMM TASK 20-24-12-200-001) and (Ref. AMM TASK 20-24-12-200-003):
  • The avionics compartment
  • The forward and aft cargo compartments
  • Between FR71 and the THS actuator and the rear rudder mechanical-control.
NOTE: It is necessary to move the cable on the pulley. There can be some corrosion that you cannot see because of the pulley guard or pulley guide.
       1 If there is corrosion on the cables or no protection with Corrosion Preventive Compound-- Soft Film System (Material No.12AGC2) or Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) or Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) :
         a Inspect the full length of the cables (Ref. AMM TASK 20-24-12-200-001) and (Ref. AMM TASK 20-24-12-200-003).
         b Clean and put a protection on the full length of the cables (Ref. AMM TASK 20-24-11-100-001).
   (3) Do a detailed inspection of the flap transmission assembly (Ref. AMM TASK 27-54-00-200-001).
   (4) Do a detailed inspection of the slat transmission system (Ref. AMM TASK 27-84-00-200-001).
   (5) If the aircraft storage period is more than 5 years, drain and fill the flap rotary actuators (Ref. AMM TASK 12-13-27-612-005).
   (6) Do a check of the fluid level of the Power Control Unit (PCU) of the flaps. If necessary, fill the PCU with oil (Ref. AMM TASK 12-13-27-612-002).
   (7) Do a check of the fluid level of the PCU of the slats. If necessary, fill the PCU with oil (Ref. AMM TASK 12-13-27-612-003).
   (8) Do the oil level check of the gearbox of the THS actuator (Ref. AMM TASK 27-44-51-210-004).
   (9) Do a test of the spoiler hydraulic control (Ref. AMM TASK 27-64-00-710-001).
   (10) Do a test of the aileron and its hydraulic control (Ref. AMM TASK 27-14-00-710-001).
   (11) Do a test of the elevator and its hydraulic control (Ref. AMM TASK 27-34-00-710-001).
   (12) Do a test of the rudder hydraulic actuation (Ref. AMM TASK 27-24-00-710-002).
   (13) Do a test of the THS actuator with the individual hydraulic systems (Ref. AMM TASK 27-44-00-710-002).
Move the THS pitch-trim control-wheel back to the 2 UP position.
   (14) Do a test of the flap and slat system (Ref. AMM TASK 27-54-00-710-002). Operate the flap and the slat system a minimum of ten times.
Subtask 10-30-00-710-140-A
W. Extend the Flight Controls
   (1) Fully extend the flaps (Ref. AMM TASK 27-50-00-866-008).
   (2) Fully extend the slats (Ref. AMM TASK 27-80-00-866-004).
Subtask 10-30-00-866-050-A
X. Safety precautions
   (1) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever on panel 114VU.
Subtask 10-30-00-865-053-A
Y. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B10
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B05
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** ON A/C ALL
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/FCDC2/SPLY20CE2Q20
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
123VUB HYD/ELEC PUMP2701GJAB09
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 10-30-00-210-075-A
Z. Visual Inspection of the Leading Edge and the Trailing Edge of the Wings
   (1) Do a visual inspection of the leading edge and the trailing edge for FOD, fluid leakage (hydraulic fluid, fuel), missing parts, blockage and corrosion of:
     (a) The wing rear spar, the false rear spar and all the components that do not move
     (b) The upper and lower surfaces of the flaps
     (c) The lower surface of the spoilers
     (d) Do a check of all the flap tracks for corrosion
     (e) Do a check of all the slat tracks for corrosion.
Subtask 10-30-00-210-093-A
AA. Visual Inspection of the Horizontal Tail Plane and the Vertical Tail Plane (VTP)
   (1) Make sure that the Blue, Green and Yellow hydraulic systems are depressurized:
   (2) Make sure that there is no GROUND POWER CART-HYDRAULIC connected to the aircraft on:
  • Green hydraulic-system service-panel 197CB
  • Blue hydraulic-system service-panel 197EB
  • Yellow hydraulic-system service-panel 198CB.
   (3) In the cockpit, put the WARNING NOTICE(S) in position to tell persons:
  • Not to pressurize the hydraulic systems,
  • Not to operate the flight controls.
   (4) Install the 98D27903500000 PIN-SIDE STICK LOCKING on the CAPT and F/O side sticks.
   (5) Install the 98D27403500000 PITCH TRIM CONTROL LOCKING on the pitch-trim control wheels (Ref. AMM TASK 27-00-00-480-001).
   (6) Put the ACCESS PLATFORM 4M (13 FT) in position at the horizontal tail plane.
   (7) ) Do a visual inspection of the horizontal tail plane for impacts by foreign objects, fluid leakage (hydraulic fluid, fuel), missing parts, blockage and corrosion of:
  • The THS leading-edge access-panels and tips
  • The THS trailing-edge access-panels
  • The THS skin panels
  • The elevators.
     (a) Open all the lower access panels of the THS trailing-edges (Ref. AMM TASK 55-13-11-000-001).
NOTE: It is not necessary to remove the panels fully.
     (b) Make sure that there is no hydraulic leak, FOD and corrosion in the elevator servo-control area.
     (c) Make sure that the hand-hole cover foils are not missing or damaged.
       1 If it is missing or damaged:
  • Check the inner side for FOD and
  • Replace the hand-hole cover foils.
     (d) Close all the lower access panels of the THS trailing-edges (Ref. AMM TASK 55-13-11-560-001) and (Ref. AMM TASK 55-13-11-400-001).
     (e) Open access door 312AR.
     (f) Make sure that there is no hydraulic leak, FOD and corrosion in the THS actuator (9CE), the ball screw assembly, the cable tension regulator and the aft-control chain areas.
     (g) Close access door 312AR.
   (8) Put the ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position at the vertical stabilizer.
   (9) Do a visual inspection of the VTP for impacts by foreign objects, hydraulic fluid leakage, missing parts, blockage and corrosion of:
  • The vertical-stabilizer leading-edge access-panels and tip
  • The vertical-stabilizer trailing-edge access-panels
  • The vertical-stabilizer skin panels
  • The rudder.
     (a) Open the vertical-stabilizer trailing-edge access-panel(s) (Ref. AMM TASK 55-33-13-010-002).
     (b) Make sure that there is no hydraulic leak, FOD and corrosion in the rudder servo-control area (on the actuation system).
     (c) Make sure that the hand-hole cover foils are not missing or damaged.
       1 If it is missing or damaged:
  • Check the inner side for FOD and
  • Replace the hand-hole cover foils.
     (d) Close the vertical-stabilizer trailing-edge access-panel(s) (Ref. AMM TASK 55-33-13-410-002).
   (10) Remove the access platform(s).
   (11) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the CAPT and F/O side sticks.
   (12) Remove the 98D27403500000 PITCH TRIM CONTROL LOCKING from the pitch-trim control wheels (Ref. AMM TASK 27-00-00-080-001).
Subtask 10-30-00-630-062-A
AB. De-preservation of the APU
   (1) If the APU was not removed:
     (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):
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).
Subtask 10-30-00-710-127-A ** ON A/C NOT FOR ALL
AC. Inspection and Test of the Engine
   (1) If the engine was not removed:
     (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) Remove the Film-- Waterproof Barrier - (Material No.14HMB1) and 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 bleed-air precooler exhaust-grids and ventilation exhaust grid on each pylon.
       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.
     (d) 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).
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 engines.
For the parking, storage, periodic checks and return to operation of the engines, ATA 10 refers to the applicable procedures in the related ATA chapter (7X).
   (2) Do the de-preservation of the Integrated Drive Generator (IDG) (Ref. AMM TASK 24-21-00-550-001).
   (3) Replace the oil of the pneumatic starter (Ref. AMM TASK 12-13-80-610-001).
   (4) Start the engines, make them turn for one minute (Ref. AMM TASK 71-00-00-710-003) or (Ref. AMM TASK 71-00-00-710-004).
   (5) Do an engine run-up for the two engines (Ref. AMM TASK 71-00-00-710-006).
   (6) Stop the engines (Ref. AMM TASK 71-00-00-710-028).
   (7) After the shutdown, do a check of the engines for oil, hydraulic and fuel leakage.
Subtask 10-30-00-710-127-B ** ON A/C NOT FOR ALL
AC. Inspection and Test of the Engine
   (1) If the engine was not removed:
     (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) Remove the Film-- Waterproof Barrier - (Material No.14HMB1) and 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 bleed-air precooler exhaust-grids and ventilation exhaust grid on each pylon.
       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.
     (d) 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).
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 engines.
For the parking, storage, periodic checks and return to operation of the engines, ATA 10 refers to the applicable procedures in the related ATA chapter (7X).
   (2) Do the de-preservation of the Integrated Drive Generator (IDG) (Ref. AMM TASK 24-21-00-600-040).
   (3) Replace the oil of the pneumatic starter (Ref. AMM TASK 12-13-80-600-011) or (Ref. AMM TASK 12-13-80-600-011).
   (4) Start the engines, make them turn for one minute (Ref. AMM TASK 71-00-00-710-043) or (Ref. AMM TASK 71-00-00-710-047).
   (5) Do an engine run-up for the two engines (Ref. AMM TASK 71-00-00-710-012) or (Ref. AMM TASK 71-00-00-710-012).
   (6) Stop the engines (Ref. AMM TASK 71-00-00-710-018).
   (7) After the shutdown, do a check of the engines for oil, hydraulic and fuel leakage.
Subtask 10-30-00-710-127-C ** ON A/C NOT FOR ALL
AC. Inspection and Test of the Engine
   (1) If the engine was not removed:
     (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) Remove the Film-- Waterproof Barrier - (Material No.14HMB1) and 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 bleed-air precooler exhaust-grids and ventilation exhaust grid on each pylon.
       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.
     (d) 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).
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 engines.
For the parking, storage, periodic checks and return to operation of the engines, ATA 10 refers to the applicable procedures in the related ATA chapter (7X).
   (2) Do the de-preservation of the Integrated Drive Generator (IDG) (Ref. AMM TASK 24-21-00-550-002).
   (3) Replace the oil of the pneumatic starter (Ref. AMM TASK 12-13-80-610-001).
   (4) Start the engines, make them turn for one minute (Ref. AMM TASK 71-00-00-710-003) or (Ref. AMM TASK 71-00-00-710-004).
   (5) Do an engine run-up for the two engines (Ref. AMM TASK 71-00-00-710-006).
   (6) Stop the engines (Ref. AMM TASK 71-00-00-710-028).
   (7) After the shutdown, do a check of the engines for oil, hydraulic and fuel leakage.
Subtask 10-30-00-710-127-F ** ON A/C NOT FOR ALL
AC. Inspection and Test of the Engine
   (1) If the engine was not removed:
     (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) Remove the Film-- Waterproof Barrier - (Material No.14HMB1) and 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 bleed-air precooler exhaust-grids and ventilation exhaust grid on each pylon.
       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.
     (d) 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).
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 engines.
For the parking, storage, periodic checks and return to operation of the engines, ATA 10 refers to the applicable procedures in the related ATA chapter (7X).
   (2) Do the de-preservation of the Integrated Drive Generator (IDG) (Ref. AMM TASK 24-21-00-550-803).
   (3) Do an engine run-up for the two engines (Ref. AMM TASK 71-00-00-720-811).
   (4) Stop the engines (Ref. AMM TASK 71-00-00-860-814).
   (5) After the shutdown, do a check of the engines for oil, hydraulic and fuel leakage.
Subtask 10-30-00-710-133-A ** ON A/C NOT FOR ALL
AD. Test of the Bleed System
   (1) Do the operational test of the bleed air system (Ref. AMM TASK 36-11-00-710-003)
Subtask 10-30-00-710-133-B ** ON A/C NOT FOR ALL
AD. Test of the Bleed System
   (1) Do the operational test of the bleed air system (Ref. AMM TASK 36-11-00-710-802).
Subtask 10-30-00-710-129-A
AE. Tests of the Ice Protection Systems
   (1) If the aircraft storage period was more than 1 month, do the steps that follow:
     (a) Do a test of the wing ice-protection system (Ref. AMM TASK 30-11-00-710-001).
     (b) Do a test of the ice protection system of the air intakes (Ref. AMM TASK 30-21-00-710-002).
Subtask 10-30-00-170-050-A ** ON A/C NOT FOR ALL
AF. Inspection of the Probes and the Sensors and 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) If not already removed, remove the aircraft protection equipment from the probes and the sensors (Ref. AMM TASK 10-11-00-555-014).
   (2) Do the inspection procedure of the sensor/probe:
     (a) For the pitot probe (Ref. AMM TASK 34-11-15-200-001).
     (b) For the static probe (Ref. AMM TASK 34-11-16-200-001).
     (c) For the Total Air Temperature (TAT) sensor (Ref. AMM TASK 34-11-18-200-002).
     (d) For the Angle Of Attack (AOA) sensor (Ref. AMM TASK 34-11-19-200-001).
   (3) Do a check of the insulation resistance of the pitot probe heater (Ref. AMM TASK 30-31-00-720-001).
   (4) Flush the total pressure line of the Air Data Module (ADM) (Ref. AMM TASK 34-10-00-170-001).
   (5) Flush the static pressure line of the ADM (Ref. AMM TASK 34-10-00-170-002).
   (6) Drain and flush the standby static and standby total pressure-lines of the ADM (Ref. AMM TASK 34-10-00-170-003).
   (7) 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 10-30-00-170-050-B ** ON A/C NOT FOR ALL
AF. Inspection of the Probes and the Sensors and 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) If not already removed, remove the aircraft protection equipment from the probes and the sensors (Ref. AMM TASK 10-11-00-555-014).
   (2) Do the inspection procedure of the sensor/probe:
     (a) For the pitot probe (Ref. AMM TASK 34-11-15-200-001).
     (b) For the static probe (Ref. AMM TASK 34-11-16-200-001).
     (c) For the Total Air Temperature (TAT) sensor (Ref. AMM TASK 34-11-18-200-002).
     (d) For the Angle Of Attack (AOA) sensor (Ref. AMM TASK 34-11-19-200-001).
   (3) Do a check of the insulation resistance of the pitot probe heater (Ref. AMM TASK 30-31-00-720-001).
   (4) Flush the total pressure line of the Air Data Module (ADM) (Ref. AMM TASK 34-10-00-170-001).
   (5) Flush the static pressure line of the ADM (Ref. AMM TASK 34-10-00-170-002).
   (6) Drain and flush the standby static and standby total pressure-lines of the ADM (Ref. AMM TASK 34-22-25-170-001).
   (7) 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 10-30-00-210-087-B
AG. Check of the Filters for Clogging
   (1) Do a check of the filters for clogging (Ref. AMM TASK 29-10-00-210-002)
5. Close-up
Subtask 10-30-00-865-057-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B11
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B10
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B09
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B08
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
49VUAUTO FLT/FAC1/28VDC5CC1B04
49VUAUTO FLT/FAC1/26VAC14CC1B03
** ON A/C ALL
49VUHYD/HYD PWR/B WARN/& CTL2702GJC12
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/ELAC1/NORM/SPLY15CE1B06
49VUFLIGHT CONTROLS/FCDC1/SPLY20CE1B05
49VUFLIGHT CONTROLS/THS/ACTR/MOT219CE2B04
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
49VUAUTO FLT/FAC1/28VDC5CC1H10
49VUAUTO FLT/FAC1/26VAC14CC1H09
** ON A/C ALL
105VUFLIGHT CONTROLS/ELAC2/STBY SPLY16CE2A02
105VUFLT CTL/ELAC1/STBY SPLY16CE1A01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN30
** ON A/C ALL
121VUAUTO FLT/RUDDER/TRIM/IND15CCM20
121VUAUTO FLT/FAC2/28VDC5CC2M19
121VUAUTO FLT/FAC2/26VAC14CC2M18
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/FCDC2/SPLY20CE2Q20
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/THS ACTR/MOT319CE3Q17
121VUFLIGHT CONTROLS/THS ACTR/MOT119CE1Q16
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
121VUFLIGHT CONTROLS/ELAC2/NORM/SPLY15CE2R20
** ON A/C NOT FOR ALL
121VUHYDRAULIC/HYD POWER/Y3803GXN31
** ON A/C ALL
123VUB HYD/ELEC PUMP2701GJAB09
123VUY HYD/ELEC/PUMP3802GXAB06
123VUY HYD/ELEC/ELEC PUMP/NORM3801GXAB03
Subtask 10-30-00-280-054-A
B. Checklist
   (1) Do the checklist for the return to operation after a storage period (Ref. AMM TASK 10-30-00-280-802).
Subtask 10-30-00-860-050-B
C. Put the Aircraft back to its Initial Configuration
   (1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever.
   (2) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
   (3) Retract the slats (Ref. AMM TASK 27-80-00-866-005).
   (4) Make sure that the 98D29208246000 SAFETY DEVICE-RAT or 98D29208246001 DEVICE-SAFETY,RAT is removed, (Ref. AMM TASK 29-22-00-860-008).
   (5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
   (6) Close forward avionics-compartment access-door 811 (Ref. AMM TASK 52-41-00-410-002).
   (7) Make sure that all the external connections (external power supply, etc.) are disconnected from the aircraft.
   (8) Remove the WARNING NOTICE(S).
Subtask 10-30-00-410-057-A
D. Close Access
   (1) Make sure that all the access doors and panels opened during this procedure are closed.
   (2) Make sure that the work area is clean and clear of tools and other items.
   (3) Remove the access platform(s).
   (4) Remove all the fixtures, tools, test and support equipment used during this procedure.
[Rev.10 from 2021] 2026.04.01 04:24:23 UTC
"Aviabrain" 2025