CHAPTER_10.pdf

@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL

CHAPTER 10 - PARKING, MOORING, STORAGE & RETURN TO SERVICE TABLE OF CONTENTS REFERENCE CHAPTER 10 10-00-00 10-00-00 PB 001

10-10-00 10-10-00 PB 001 10-11-00 10-11-00 PB 201 10-11-00-555-006-A

PARKING, MOORING, STORAGE & RETURN TO SERVICE - GENERAL PARKING, MOORING, STORAGE & RETURN TO SERVICE - GENERAL DESCRIPTION AND OPERATION PARKING/STORAGE PARKING/STORAGE - DESCRIPTION AND OPERATION PARKING PARKING - MAINTENANCE PRACTICES Parking procedures

10-1 10 -111-00 00-5 -555 55-0 -007 07-A -A

Parkin Park ing g Pr Proc oced edur uree in Fl Flig ight ht-r -rea eady dy Co Cond ndit itio ion n (P (Par arki king ng of no nott mo more re th than an 15 Days)

10-1 10 -111-00 00-5 -555 55-0 -008 08-A -A

Parkin Park ing g Pr Proc oced edur uree in Fl Flig ight ht-r -rea eady dy Co Cond ndit itio ion n (P (Par arki king ng of no nott mo more re th than an 12 Weeks)

10-1110-1 1-00 00-5 -554 54-0 -003 03-A -A 10-1 10 -111-00 00-5 -554 54-0 -004 04-A -A 10-11-00-555-011-A 10-11-00-555-012-A 10-1 10 -111-0 -000-55 5555-01 0133-A 10-11-00-991-00100-B 10-11-00-991-00400-B 10-11-00-991-00700-A 10-11-00-991-00600-A 10-11-00-555-014-A 10-1 10 -111-00 00-5 -555 55-0 -015 15--A 10-11-00-991-01000-A 10-11-00 PB 601 10-11-00-200-002-A 10-11-00-200-003-A 10-11-00-200-004-A 10-12-00 10-12-00 PB 201 10-12-00-553-005-A 10-12-00-553-006-A

AES

SUBJECT

Return Retu rn to Op Oper erat atiion af aftter Pa Park rkin ing g no nott mor oree tha han n 15 Da Days ys Ret etur urn n to Op Oper erat atio ion n af aftter Pa Parrki king ng no nott mor oree th than an 12 We Week ekss Renewal of 15-Day Parking Period Renewal of 12-Week Parking Period Inst In stal alla lati tion on of the Ai Airc rcra rafft Pr Prot otec ecti tion on Eq Equi uipm pmen entt Protective Equipment Protective Equipment Protective Equipment Protective Equipment Remov ovaal of the Aircraft Protection Equi uipm pmeent Proc Pr oced edur uree for the In Inst stal alla lattio ion n of Whe heel el Ch Choc ocks ks on Air ircr craf aftt Location of Wheel Chocks PARKING - INSPECTION/CHECK Periodic Ground Check at 7-day In Inttervals Periodic Ground Check at 15-day In Inttervals Periodic Ground Check at 1-mon ontth In Intterval alss STORAGE STORAGE - MAINTENANCE PRACTICES Storage Procedures Storag agee Procedu durre (Storag agee No Nott More than 6 Months)

T.O.C.

Page 1 May 01/12 Revision n˚: 40

@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 10-12-00-553-007-A

SUBJECT Storage age Procedu durre (Storage age No Nott More than 2 Year arss)

10-12-00-553-008-A 10-12-00-553-009-A

Renewal for 6 Months Storage Period Renewal for 2 Years Storage Period

10-12-00 PB 601 10-12-00-200-006-A 10-12-00-200-007-A 10-12-00-200-008-A 10-12-00-200-009-A 10-12-00-200-010-A 10-20-00 10-20-00 PB 201 10-2 10 -200-00 00-5 -556 56-0 -001 01-A -A 10-20-00-991-00700-A 10-20-00-991-00500-A 10-20-000-9991-00300-A 10--20 10 20-0 -000-99 9911-00 0080 8000-A 10--20 10 20-0 -000-99 9911-00 0060 6000-A 10-2 10 -200-00 00-5 -556 56-0 -001 01-A -A-0 -011 10--20 10 20-0 -000-99 9911-00 0020 2000-A 10-30-00 10-30-00 PB 601 10-30-00-554-005-A

AES

STORAGE - INSPECTION/CHECK Periodic Periodic Periodic Periodic Periodic

Ground Check at 7-day In Inttervals Ground Check at 15-day In Inttervals Groundd-C Che hecck at 1-month Interval ground nd--check at 3-month interval Ground Check at 6-mon ontth In Intterval alss

MOORING MOORING - MAINTENANCE PRACTICES Moor Mo orin ing g of Ai Airc rcra raft ft wi with thou outt We Weig ight ht an and d Ba Bala lanc ncee Pr Prov ovis isio ion n on th thee La Land ndin ing g Gear Legs Mooring Wind Speed Limits Position of the Ground Rings Posi sittion of the Mooring Ropes Nose No se La Land ndin ing g Ge Gear ar - In Inst stal alllat atiion of th thee Mo Moor orin ing g It Item emss Main Ma in La Land ndiing Gea earr - In Inst stal alla lattio ion n of th thee Mo Moor oriing It Iteems Moor Mo orin ing g of Ai Airc rcra raft ft wi with th We Weig ight ht an and d Ba Bala lanc ncee Pr Prov ovis isio ion n on th thee La Land ndin ing g Gear Legs Atta At tach chme ment nt of th thee Mo Moor oriing Rop opees on th thee No Nose se La Land ndin ing g Ge Gear ar RETURN TO SERVICE RETURN TO SERVICE - INSPECTION/CHECK Return to Operation af aftter Storag agee Period

T.O.C.



PARKING, MOORING, STORAGE & RETURN TO SERVICE GENERAL - DESCRIPTION AND OPERATION ** On A/C ALL 1.

Gene Ge nerral This chapter cover covers: s: . Par Parkin king/S g/Stor torage age (Re (Ref. f. ATA 1010-10) 10),, . Mo Moor orin ingg (R (Ref ef.. ATA ATA 10 10-2 -20) 0),, . Ret Return urn to Ser Servic vicee (Ref (Ref.. ATA ATA 1010-30) 30)..

AES

10-00-00 PB001



PARKING/STORAGE - DESCRIPTION AND OPERATION ** On A/C ALL 1.

General This section provides information related to the parking and storage of the aircraft. It is divided as follows: . PARKING (Ref. ATA 10-11), . STORAGE (Ref. ATA 10-12).

AES

10-10-00 PB001



PARKING - MAINTENANCE PRACTICES ** On A/C ALL Task 10-11-00-555-006-A Parking procedures 1.

Reason for the Job This task gives the procedures for: . parking the aircraft in flight-ready condition . ground checks during parking . return to operation after parking . renewal parking procedures

2.

Job Set-up Information A.

Referenced Information

REFERENCE 10-11-00-200-002-A

DESIGNATION Periodic Ground Check at 7-day Intervals

10-11-00-200-003-A

Periodic Ground Check at 15-day Intervals

10-11-00-200-004-A 10-11-00-554-003-A

Periodic Ground Check at 1-month Intervals Return to Operation after Parking not more than 15 Days

10-11-00-554-004-A

Return to Operation after Parking not more than 12 Weeks

10-11-00-555-007-A

Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days)

10-11-00-555-008-A

Parking Procedure in Flight-ready Condition (Parking of not more than 12 Weeks)

10-11-00-555-011-A 10-11-00-555-012-A

Renewal of 15-Day Parking Period Renewal of 12-Week Parking Period

3.

Job Set-up Subtask 10-11-00-860-083-A A.

4.

Not Applicable

Procedure Subtask 10-11-00-555-073-A A.

Procedures to park the aircraft in flight-ready condition with related procedures to do periodic ground check, to return to operation and to do again the parking procedure (1)

AES

Parking of the aircraft in flight-ready condition not more than 15 days (Ref. TASK 10-11-00-555-007-A) (a)

During parking for not more than 15 days, you must do a periodic ground check at 7-day intervals (Ref. TASK 10-11-00-200-002-A).

(b)

You can do again the procedure to park the aircraft for not more than 15 days one time only (Ref. TASK 10-11-00-555-011-A).

(c)

At the end of the parking period and before the next flight, you must do the return to operation after parking period of not more than 15 days (Ref. TASK 10-11-00-554-003-A).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (2)

Parking of the aircraft in flight-ready condition not more than 12 weeks (Ref. TASK 10-11-00-555-008A) NOTE :

AES

The procedure for the renewal of the 12-week parking period includes an instruction to do a nonrevenue flight within the aircraft standard envelope.

(a)

During parking period of not more than 12 weeks, you must do periodic ground checks: . periodic ground check at 7-day intervals (Ref. TASK 10-11-00-200-002-A) . periodic ground check at 15-day intervals (Ref. TASK 10-11-00-200-003-A) . periodic ground check at 1-month intervals (Ref. TASK 10-11-00-200-004-A).

(b)

You can do again the procedure to park the aircraft for not more than 12 weeks more than one time (Ref. TASK 10-11-00-555-012-A).

(c)

At the end of the parking period and the before next flight, you must do the return to operation after parking period of not more than 12 weeks (Ref. TASK 10-11-00-554-004-A).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-007-A Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days) CAUTION :

DURING STORAGE OR PARKING PERIODS, DO NOT STOP OR CHANGE THE MAINTENANCE PROGRAM WITHOUT LOCAL AUTHORITY APPROVAL. THE MAINTENANCE CALENDAR CLOCK CONTINUES DURING THESE PERIODS. IF YOU DO THE AMM STORAGE OR PARKING PROCEDURES CORRECTLY, AND IF YOU HAVE THE APPROVAL 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 preservation steps for a parking period of not more than 15 days. NOTE :

2.

This procedure is to keep the aircraft in flight-ready condition during the parking period. We recommend that there is no cannibalization or removal of parts during this parking period.


Fixtures, Tools, Test and Support Equipment

REFERENCE No specific

QTY AR CHOCK - WHEEL(S)

No specific 25-01-000

AR 1

B.

DESIGNATION

SAFETY CLIP - CIRCUIT BREAKER SUN SCREEN,SET-COCKPIT


REFERENCE 05-57-00-200-001-A

Aircraft Stability

10-11-00-200-002-A 10-11-00-554-003-A

Periodic Ground Check at 7-day Intervals Return to Operation after Parking not more than 15 Days

10-11-00-555-011-A

Renewal of 15-Day Parking Period

10-11-00-555-013-A 10-11-00-555-015-A 10-20-00-556-001-A

Installation of the Aircraft Protection Equipment Procedure for the Installation of Wheel Chocks on Aircraft Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs

10-20-00-556-001-A-01

Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs

12-11-28-650-003-A 12-11-28-650-004-A 12-16-38-613-001-A 12-21-11-615-002-A

Pressure Refuel with Automatic Control Pressure Refuel with Manual Control Servicing of the Toilet System External Cleaning

AES

DESIGNATION

10-11-00 PB201



DESIGNATION Cleaning of the Cockpit Equipment/Furnishings

12-21-12-100-003-A

Cleaning of the Carpets and Non-Textile Floor Covering (NTF)

12-21-12-100-004-A

Cleaning of the Plastic Surfaces and Mirrors

12-21-12-100-005-A

Cleaning of the Seat Covers and the Curtains

12-21-12-100-006-A

Cleaning of the Light Alloy and Steel Components

12-21-12-100-007-A

Cleaning of the Cargo Compartments

12-21-12-100-008-A

Cleaning of the Cabin Monitors and Display Screens (if installed)

12-21-12-100-009-A

Cleaning of the Plastic Wash Basin in the Lavatories

12-24-38-680-001-A

Draining of the Potable Water System (with Electrical Power)

12-31-21-660-001-A

Cold Weather Maintenance - Air Conditioning

12-31-24-660-001-A 12-31-25-660-001-A

Cold Weather Maintenance - Electrical Power Cold Weather Maintenance - Equipment/Furnishings

12-31-27-660-001-A

Cold Weather Maintenance - Flight Controls

12-31-28-660-001-A 12-31-31-660-001-A

Cold Weather Maintenance - Fuel Cold Weather Maintenance - Indicating/Recording systems and Navigation

12-31-32-660-001-A

Cold Weather Maintenance - Landing Gear

12-31-35-660-001-A

Cold Weather Maintenance - Oxygen System

12-31-38-660-001-A

Cold Weather Maintenance - Water/Waste

12-31-49-660-001-A 12-31-51-660-001-A 12-31-52-660-001-A 12-31-71-660-001-A 12-32-28-281-001-A 12-34-24-869-002-A

Cold Weather Maintenance - Auxiliary Power Unit Cold Weather Maintenance - Structure Cold Weather Maintenance - Doors Cold Weather Maintenance - Power Plant Drain Water Content Aircraft Grounding for the Maintenance Operations

24-38-51-000-001-A 24-41-00-861-002-A

Removal of the Batteries Energize the Aircraft Electrical Circuits from the External Power

24-41-00-861-002-A-01

Energize the Aircraft Electrical Circuits from the APU

24-41-00-861-002-A-02

Energize the Aircraft Electrical Circuits from Engine 1(2)

24-41-00-862-002-A

De-energize the Aircraft Electrical Circuits Supplied from the External Power

24-41-00-862-002-A-01

De-energize the Aircraft Electrical Circuits Supplied from the APU

24-41-00-862-002-A-02

De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)

32-00-00-481-001-A

Installation of the Safety Devices on the Landing Gears

52-10-00-410-001-A

Closing of the Passenger/Crew Door

71-00-00-550-010-A

Preservation of the Power Plant

3.


General (1)

This section gives the procedure to park the aircraft in standard weather conditions but: (a)

AES

If the aircraft is parked in high wind conditions: . do a check of the aircraft stability (Ref. TASK 05-57-00-200-001-A)

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL . (b)

moor the aircraft (Ref. TASK 10-20-00-556-001-A) or (Ref. TASK 10-20-00-556-001-A-01) if necessary.

If the aircraft is kept in storage in cold weather conditions: . do the cold weather maintenance procedures: (Ref. TASK 12-31-21-660-001-A), (Ref. TASK 12-31-24-660-001-A), (Ref. TASK 12-31-25-660-001-A), (Ref. TASK 12-31-27-660-001-A), (Ref. TASK 12-31-28-660-001-A), (Ref. TASK 12-31-31-660-001-A), (Ref. TASK 12-31-32-660-001-A), (Ref. TASK 12-31-35-660-001-A), (Ref. TASK 12-31-38-660-001-A), (Ref. TASK 12-31-49-660-001-A), (Ref. TASK 12-31-51-660-001-A), (Ref. TASK 12-31-52-660-001-A), (Ref. TASK 12-31-71-660-001-A). NOTE :

In cold weather conditions, we recommend that you put a fiber material between the tires and the ground surface.

Subtask 10-11-00-615-053-A B.

Cleaning of the Aircraft (1)

If necessary, clean the aircraft externally (Ref. TASK 12-21-11-615-002-A).

(2)

If necessary, clean the aircraft internally: (Ref. TASK 12-21-12-100-002-A) (Ref. TASK 12-21-12-100-003-A) (Ref. TASK 12-21-12-100-004-A) (Ref. TASK 12-21-12-100-005-A) (Ref. TASK 12-21-12-100-006-A) (Ref. TASK 12-21-12-100-007-A) (Ref. TASK 12-21-12-100-008-A) (Ref. TASK 12-21-12-100-009-A)

Subtask 10-11-00-941-054-A C.

Safety Precautions (1)

Park the aircraft on a flat surface. Make sure that the wheels of the nose landing gear are on the aircraft axis and the aircraft points into the wind.

(2)

Install the safety devices on the landing gears (Ref. TASK 32-00-00-481-001-A).

(3)

Make sure that the flaps, the slats, the spoilers and the thrust reversers are retracted.

(4)

Make sure that the THS pitch-trim control wheel is set to two degrees aircraft nose up.

(5)

Put the CHOCK - WHEEL(S) in position: (Ref. TASK 10-11-00-555-015-A).

(6)

Ground the aircraft (Ref. TASK 12-34-24-869-002-A).

Subtask 10-11-00-650-058-A D.

4.

Aircraft Configuration (1)

Energize the electrical circuits (Ref. TASK 24-41-00-861-002-A) or (Ref. TASK 24-41-00-861-002-A-01) or (Ref. TASK 24-41-00-861-002-A-02).

(2)

Refuel the fuel tanks to 30% minimum of their total capacity (Ref. TASK 12-11-28-650-003-A) or (Ref. TASK 12-11-28-650-004-A).

Procedure Subtask 10-11-00-620-065-B A.

Protection of the Engines (1)

AES

Do the preservation of the engines (Ref. TASK 71-00-00-550-010-A).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-281-059-A B.

Protection of the Fuel System (1)

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A). . from the ACT, if installed (Ref. AMM 12-32-28-281-005) . NOTE :

Do the water drain procedure one hour after refueling is completed.

Subtask 10-11-00-555-065-A C.

Installation of the Protection Equipment (1)

Use adapted protection equipment to give protection to all the probes, the engines and the APU (Ref. TASK 10-11-00-555-013-A). . Install the protection immediately after the last flight to prevent contamination of the air data system.

Subtask 10-11-00-680-055-A D.

Protection of the Water and Toilet System (1)

Potable water system (a)

If the parking period is more than 2 days: . drain, flush and dry the system if necessary (Ref. TASK 12-24-38-680-001-A) NOTE :

(2)

The airline can use its experience to adapt the 2-day interval.

Toilet system (a)

If the parking period is more than 2 days: . drain, flush and clean the system with disinfectant if necessary (Ref. TASK 12-16-38-613-001A).

Subtask 10-11-00-620-060-A E.

Protection of the Windows (1)

Open the cockpit and cabin window shades.

(2)

Make sure that the sliding windows are closed.

(3)

We recommend that you put a SUN SCREEN,SET-COCKPIT (25-01-000) in the cockpit on all the windows.

Subtask 10-11-00-860-073-A F.

Aircraft Maintenance Configuration (1)

On the overhead panel 25VU, on the CABIN PRESS section: . Push the DITCHING pushbutton switch to close the ventilation skin valves and the outflow valves .

(2)

If the parking is more than 2 days: (a)

We recommend that you disconnect the batteries 2PB1 and 2PB2 (Ref. TASK 24-38-51-000-001A). NOTE :

(3)

AES

If the batteries stay connected during parking, the loads that are permanently connected (Hot Buses), will decrease the battery charge to a very low level and it will be necessary to replace the batteries.

De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002-A) or (Ref. TASK 24-41-00-862-002-A-01) or (Ref. TASK 24-41-00-862-002-A-02).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-865-051-A G.

Open, safety and tag this(these) circuit breaker(s): PANEL

105VU

DESIGNATION ELEC/HOT BUS/702PP SPLY

5PB2

D02

105VU

ELEC/HOT BUS/701PP SPLY

5PB1

D01

105VU


12PB2

E02

105VU


12PB1

E01

105VU

ELEC/BAT REF/BCL2

9PB2

F02

105VU

ELEC/BAT REF/BCL1

9PB1

F01

5.

FIN

LOCATION

Close-up Subtask 10-11-00-942-055-A A.

Close-up. (1)

Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that protection covers/devices are installed.

(2)

Remove the ground support and maintenance equipment, the special and standard tools and all other items.

(3)

Close all the pressurized access doors.

(4)

Close the passenger/crew doors (Ref. TASK 52-10-00-410-001-A).

Subtask 10-11-00-555-066-A B.

AES

Periodic Checks and Return to Operation (1)

During the parking period, do the periodic checks: . at 7-day intervals (Ref. TASK 10-11-00-200-002-A).

(2)

For return to operation, do the return to operation procedure (Ref. TASK 10-11-00-554-003-A).

(3)

You can do the renewal procedure one time (Ref. TASK 10-11-00-555-011-A).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-008-A Parking Procedure in Flight-ready Condition (Parking of not more than 12 Weeks) CAUTION :


CAUTION :


1.

Reason for the Job This procedure gives the preservation steps for a parking period of not more than 12 weeks.

2.

NOTE :

This procedure is to keep the aircraft in flight-ready condition during the parking period. We recommend that there is no cannibalization or removal of parts during this parking period.

NOTE :

The procedure for the renewal of the 12-week parking period includes an instruction to do a non-revenue flight within the aircraft standard envelope.





25-01-000

1

B.

SUN SCREEN,SET-COCKPIT

Consumable Materials

REFERENCE Material No: 05-043

Material No: 15-002 C.

DESIGNATION

DESIGNATION

SPECIAL MATERIALS VARNISH P.T.F.E SPRAY STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF


REFERENCE 05-57-00-200-001-A

DESIGNATION

10-11-00-200-002-A

Aircraft Stability Periodic Ground Check at 7-day Intervals

10-11-00-200-003-A


10-11-00-200-004-A 10-11-00-554-004-A

Periodic Ground Check at 1-month Intervals Return to Operation after Parking not more than 12 Weeks

10-11-00-555-012-A

Renewal of 12-Week Parking Period

AES

10-11-00 PB201



DESIGNATION Installation of the Aircraft Protection Equipment

10-11-00-555-015-A 10-20-00-556-001-A

Procedure for the Installation of Wheel Chocks on Aircraft Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs

10-20-00-556-001-A-01

Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs

12-11-28-650-003-A 12-11-28-650-004-A 12-16-38-613-001-A

Pressure Refuel with Automatic Control Pressure Refuel with Manual Control Servicing of the Toilet System

12-21-11-615-002-A

External Cleaning

12-21-12-100-002-A

Cleaning of the Cockpit Equipment/Furnishings

12-21-12-100-003-A


12-21-12-100-004-A


12-21-12-100-005-A


12-21-12-100-006-A


12-21-12-100-007-A


12-21-12-100-008-A


12-21-12-100-009-A


12-22-52-640-002-A 12-22-52-640-006-A

Lubrication of the FWD and AFT Cargo-Compartment Doors Lubrication of the External Control Handles of the FWD and AFT Passenger/Crew Doors

** On A/C 003-003 12-22-52-640-007-A

Lubrication of the BULK-Cargo Compartment-Door Handle and Hinge Arms Bearings

12-22-52-640-008-A 12-22-52-640-009-A

Lubrication of the Avionics Compartment-Door Handles Lubrication of the FWD and AFT Cargo-Compartment Door Handle

12-22-52-640-014-A

Lubrication of Safety Pin Guide Fitting and Door Arming/Disarming Mechanism

12-22-52-640-016-A

Lubrication of the Hinge-Arm Support-Fitting Bearings

12-24-38-680-001-A


12-31-21-660-001-A

Cold Weather Maintenance - Air Conditioning

12-31-24-660-001-A 12-31-25-660-001-A


12-31-27-660-001-A 12-31-28-660-001-A 12-31-31-660-001-A

Cold Weather Maintenance - Flight Controls Cold Weather Maintenance - Fuel Cold Weather Maintenance - Indicating/Recording systems and Navigation

12-31-32-660-001-A 12-31-35-660-001-A

Cold Weather Maintenance - Landing Gear Cold Weather Maintenance - Oxygen System

12-31-38-660-001-A


12-31-49-660-001-A 12-31-51-660-001-A 12-31-52-660-001-A 12-31-71-660-001-A

Cold Cold Cold Cold

AES

Weather Weather Weather Weather

Maintenance Maintenance Maintenance Maintenance

- Auxiliary Power Unit - Structure - Doors - Power Plant

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 12-32-28-281-001-A 12-32-28-281-003-A

Drain Water Content Sample Fuel for Microbiological Contamination Analysis

12-34-24-869-002-A

Aircraft Grounding for the Maintenance Operations

24-38-51-000-001-A 24-41-00-861-002-A


24-41-00-861-002-A-01


24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


28-11-00-600-010-A

Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig

28-11-00-600-010-A-01 28-11-00-600-010-A-02

DESIGNATION

28-11-00-600-010-A-03

Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig

32-00-00-481-001-A


34-10-00-170-001-A 34-10-00-170-002-A

Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines

34-10-00-170-003-A

Draining and Flushing of Standby Pneumatic Circuits

** On A/C 006-099 49-00-00-860-005-A

APU Start by External Power

49-00-00-860-005-A-01 49-00-00-860-006-A

APU Start by Batteries APU Shutdown by External Power

49-00-00-860-006-A-01

APU Shutdown by Batteries

** On A/C 003-005 49-00-00-860-008-A

APU Start by External Power

49-00-00-860-008-A-01

APU Start by Batteries

49-00-00-860-009-A

APU Shutdown by External Power (131-9(A))

49-00-00-860-009-A-01

APU Shutdown by Batteries (131-9(A))

52-10-00-010-001-A

Opening of the Passenger/Crew Door

52-10-00-410-001-A


52-30-00-860-001-A

Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump

52-30-00-860-002-A ** On A/C 003-003 52-30-00-860-006-A

Open the Bulk Cargo-Compartment Door

52-30-00-860-008-A 71-00-00-550-010-A

Close the Bulk Cargo-Compartment Door Preservation of the Power Plant

AES

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 71-00-00-710-018-A 71-00-00-710-043-A

DESIGNATION Discontinued Start, Restart and Shutdown Procedures Normal Engine Automatic Start Procedure

78-31-00-710-041-A

Operational Test of the Thrust Reverser System with the CFDS

78-31-00-710-041-A-01

Operational Test of the Thrust Reverser without the CFDS and Engine not Running

78-31-00-710-041-A-02

Operational test of the Thrust Reverser without the CFDS and Engine Running

3.

Job Set-up ** On A/C ALL Subtask 10-11-00-860-074-A A.

General (1)

This section gives the procedure to park the aircraft in standard weather conditions but: (a)

If the aircraft is parked in high wind conditions: . do a check of the aircraft stability (Ref. TASK 05-57-00-200-001-A) . moor the aircraft (Ref. TASK 10-20-00-556-001-A) or (Ref. TASK 10-20-00-556-001-A-01) if necessary.

(b)

If the aircraft is stored in cold weather conditions: . do the cold weather maintenance procedures: (Ref. TASK 12-31-21-660-001-A), (Ref. TASK 12-31-24-660-001-A), (Ref. TASK 12-31-25-660-001-A), (Ref. TASK 12-31-27-660-001-A), (Ref. TASK 12-31-28-660-001-A), (Ref. TASK 12-31-31-660-001-A), (Ref. TASK 12-31-32-660-001-A), (Ref. TASK 12-31-35-660-001-A), (Ref. TASK 12-31-38-660-001-A), (Ref. TASK 12-31-49-660-001-A), (Ref. TASK 12-31-51-660-001-A), (Ref. TASK 12-31-52-660-001-A), (Ref. TASK 12-31-71-660-001-A). NOTE :


Subtask 10-11-00-615-054-A B.



(2)

If necessary, clean the aircraft internally: (Ref. TASK 12-21-12-100-002-A) (Ref. TASK 12-21-12-100-003-A) (Ref. TASK 12-21-12-100-004-A) (Ref. TASK 12-21-12-100-005-A) (Ref. TASK 12-21-12-100-006-A) (Ref. TASK 12-21-12-100-007-A) (Ref. TASK 12-21-12-100-008-A) (Ref. TASK 12-21-12-100-009-A)

Subtask 10-11-00-941-055-A C.

AES



(2)


10-11-00 PB201




(4)


(5)


(6)


Subtask 10-11-00-650-059-A D.

4.



(2)

Refuel the fuel tanks to 30% minimum of their total capacity (Ref. TASK 12-11-28-650-003-A) or (Ref. TASK 12-11-28-650-004-A).




(2)

Engine operation (if necessary) NOTE :

You can ignore this step if the last flight cycle was in the last 24 hours (engines and APU operated). In these conditions, the parking period starts from the end of this last flight cycle.

(a)

Start the engines and let them become stable at ground idle for 15 to 20 minutes (Ref. TASK 71-00-00-710-043-A).

(b)

Do a thrust reverser full cycle (Ref. TASK 78-31-00-710-041-A) or (Ref. TASK 78-31-00-710-041A-01) or (Ref. TASK 78-31-00-710-041-A-02).

(c)

Stop the engines (Ref. TASK 71-00-00-710-018-A).

Subtask 10-11-00-710-056-A B.

Protection of the APU NOTE :

AES

You can ignore this step if the last flight cycle was in the last 24 hours (engines and APU operated). In these conditions, the parking period starts from the end of this last flight cycle.

(1)

Start the APU and operate it for at least 5 minutes at no load governed speed: . for a GTCP 36-300 APU: (Ref. AMM 49-00-00-860-003) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-00-00-860-005-A) or (Ref. TASK 49-00-00-860-005-A-01) . for a 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-00-00-860-008-A)(Ref. TASK 49-00-00-860-008-A-01)

(2)

After protection of the engines, stop the APU: . for a GTCP 36-300 APU: (Ref. AMM 49-00-00-860-004) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-00-00-860-006-A) or (Ref. TASK 49-00-00-860-006-A-01) . for a 131-9(A) APU: ** On A/C 003-005

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-00-00-860-009-A)(Ref. TASK 49-00-00-860-009-A-01) ** On A/C ALL Subtask 10-11-00-281-060-A C.

Protection of the fuel system (1)

Do a fuel sampling for microbiological contamination (Ref. TASK 12-32-28-281-003-A).

(2)

Do a preventive treatment:

(3)

(a)

If premixed fuel is available: . Refuel the wing tanks to 30% of the total capacity with fuel premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-01) or Biobor biocide (Ref. TASK 28-11-00-600-010-A). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel premixed with Kathon Biocide (Ref. TASK 28-11-00-600-010-A-01) or Biobor Biocide (Ref. TASK 28-11-00-600-010-A).

(b)

If premixed fuel is not available: . Refuel the wing tanks to 30% of the total capacity with fuel not premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-03) or Biobor biocide (Ref. TASK 28-11-00-600-010A-02). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel not premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-03) or Biobor biocide (Ref. TASK 28-11-00-600-010A-02).

Drain water : . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from the ACT, if installed (Ref. AMM 12-32-28-281-005) NOTE :

(4)


Close all the fuel system valves.

Subtask 10-11-00-170-055-A D.

Flushing of the Air Data System (1)

Flush the total pressure line of the Air Data Module (Ref. TASK 34-10-00-170-001-A).

(2)

Flush the static pressure line of the Air Data Module (Ref. TASK 34-10-00-170-002-A).

(3)

Drain and flush the standby static and standby total pressure lines of the Air Data Module (Ref. TASK 34-10-00-170-003-A).

Subtask 10-11-00-555-067-A E.


Put adapted protection equipment on all the probes, the engines and the APU (Ref. TASK 10-11-00-555-013-A).

Subtask 10-11-00-680-056-A F.


Potable water system (a)

AES

If the parking period is more than 2 days: . drain, flush and dry the system if necessary (Ref. TASK 12-24-38-680-001-A).

10-11-00 PB201



Toilet system (a)

If the parking period is more than 2 days: . drain, flush and disinfect the system if necessary (Ref. TASK 12-16-38-613-001-A).

Subtask 10-11-00-620-061-A G.



(2)

Make sure that the sliding window are closed.

(3)

We recommend that you put a SUN SCREEN,SET-COCKPIT (25-01-000) in the cockpit on all the windows.

Subtask 10-11-00-860-075-A H.


On the overhead panel 25VU, on the CABIN PRESS section: . Push the DITCHING pushbutton switch to close the ventilation skin valves and the outflow valves .

(2)

Disconnect the batteries 2PB1 and 2PB2 (Ref. TASK 24-38-51-000-001-A).

(3)


Subtask 10-11-00-620-062-A J.

Protection of the Seats (1)

We recommend that you do the protection of the cockpit and passenger seats with STORAGE PRESERVATION (Material No: 15-002) . This is to prevent discoloration by the sun during a long parking period.

** On A/C 004-099 Subtask 10-11-00-620-063-A K.

Protection of the Doors (1)

Open the passenger/crew doors (Ref. TASK 52-10-00-010-001-A).

(2)

Open the cargo compartment doors (Ref. TASK 52-30-00-860-001-A).

(3)

Open all the pressurized access doors.

(4)

Lubricate the external control handles of the passenger/crew doors (Ref. TASK 12-22-52-640-006-A).

(5)

Lubricate the safety pin guide fitting and the door arming/disarming mechanism (Ref. TASK 12-22-52-640-014-A).

(6)

Lubricate the hinge-arm support-fitting bearings (Ref. TASK 12-22-52-640-016-A).

(7)

Lubricate the cargo-compartment doors (Ref. TASK 12-22-52-640-002-A).

(8)

Lubricate the cargo-compartment door handles (Ref. TASK 12-22-52-640-009-A).

(9)

Lubricate the avionics compartment-door handles (Ref. TASK 12-22-52-640-008-A).

(10) Apply SPECIAL MATERIALS (Material No: 05-043) on the seals of all the doors. ** On A/C 003-003 Subtask 10-11-00-620-063-B K.


AES


10-11-00 PB201



Open the cargo compartment doors (Ref. TASK 52-30-00-860-001-A).

(3)

Open the bulk-cargo door (Ref. TASK 52-30-00-860-006-A).

(4)


(5)


(6)


(7)


(8)


(9)


(10) Lubricate the bulk-cargo door handle (Ref. TASK 12-22-52-640-007-A). (11) Lubricate the avionics compartment-door handles (Ref. TASK 12-22-52-640-008-A). (12) Apply SPECIAL MATERIALS (Material No: 05-043) on the seals of all the doors. 5.

Close-up ** On A/C 004-099 Subtask 10-11-00-942-056-A A.

Close-up. (1)


(2)


(3)

Close the FWD and aft cargo-compartment doors (Ref. TASK 52-30-00-860-002-A).

(4)


(5)

Make an entry in the aircraft log book or attach a tag on the captain side stick to tell the crew that protection covers/devices are installed.

** On A/C 003-003 Subtask 10-11-00-942-056-B A.

Close-up. (1)


(2)


(3)


(4)

Close the bulk cargo door (Ref. TASK 52-30-00-860-008-A).

(5)


(6)

Make an entry in the aircraft log book or attach a tag on the captain side stick to tell the crew that protection covers/devices are installed.

** On A/C ALL Subtask 10-11-00-555-068-A B.

Periodic Checks and Return to Operation (1)

AES

During the parking period, do the periodic checks: . at 7-day intervals (Ref. TASK 10-11-00-200-002-A).

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL . .

at 15-day intervals (Ref. TASK 10-11-00-200-003-A). at 1-month intervals (Ref. TASK 10-11-00-200-004-A).

(2)

For return to operation, do the return to operation procedure (Ref. TASK 10-11-00-554-004-A).

(3)

You can do the renewal procedure more than one time (Ref. TASK 10-11-00-555-012-A). NOTE :

AES

The procedure for the renewal of the 12-week parking period includes an instruction to do a nonrevenue flight within the aircraft standard envelope.

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-554-003-A Return to Operation after Parking not more than 15 Days CAUTION :

1.


Reason for the Job This procedure gives the instructions necessary to operate an aircraft again after a parking period of not more than 15 days.

2.




QTY DESIGNATION 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE

No specific

AR

B.

WARNING NOTICE(S)


REFERENCE 10-11-00-555-014-A

DESIGNATION Removal of the Aircraft Protection Equipment

12-14-32-614-003-A

Check of MLG Shock Absorber Charge Pressure

12-14-32-614-004-A 12-21-11-615-002-A

Check NLG Shock Absorber Charge Pressure External Cleaning

12-32-28-281-001-A 24-38-51-400-001-A 24-41-00-861-002-A 24-41-00-861-002-A-01

Drain Water Content Installation of the Batteries Energize the Aircraft Electrical Circuits from the External Power Energize the Aircraft Electrical Circuits from the APU

24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


32-41-00-210-003-A

Inspection/Check of the Tire Pressure

34-10-00-170-001-A 34-10-00-170-002-A


34-10-00-170-003-A


71-00-00-550-011-A

Depreservation of the Power Plant

AES

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL 3.


4.


Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position near the aircraft.

(2)

Put a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the systems while you prepare the aircraft for operation again.



Do a general visual inspection of the airframe from the ground for correct condition. (a)

(2)

Make sure that there is no leakage from: . the wings . the lower fuselage . the landing gear . the engines . the APU . the horizontal and vertical stabilizers.


Subtask 10-11-00-020-065-A B.

Removal of the Protection Equipment (1)

Remove all the protection equipment from the engines, the APU and the probes (Ref. TASK 10-11-00-555-014-A).

Subtask 10-11-00-860-077-A C.


Connect the batteries 2PB1, 2PB2 and make sure that the battery charge is correct (Ref. TASK 24-38-51-400-001-A).

(2)

Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002-A) or (Ref. TASK 24-41-00-861-002-A-01) or (Ref. TASK 24-41-00-861-002-A-02).

(3)

On the overhead panel 25VU, on the CABIN PRESS section: . Push the DITCHING pushbutton switch to open the ventilation skin valves and the outflow valve.

Subtask 10-11-00-865-052-A D.

Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): PANEL

105VU

DESIGNATION ELEC/HOT BUS/702PP SPLY

5PB2

D02

105VU


5PB1

D01

105VU


12PB2

E02

105VU


12PB1

E01

105VU

ELEC/BAT REF/BCL2

9PB2

F02

105VU

ELEC/BAT REF/BCL1

9PB1

F01

AES

FIN

LOCATION

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-281-061-A E.

Protection of the Fuel System (1)

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A). . from the ACT, if installed (Ref. AMM 12-32-28-281-005) .

Subtask 10-11-00-210-065-A F.

Inspection (1)

Do a check of the charge pressure of the landing gear shock absorbers: . for the NLG (Ref. TASK 12-14-32-614-004-A) . for the MLG (Ref. TASK 12-14-32-614-003-A)

(2)

Do a check of the tire pressure (Ref. TASK 32-41-00-210-003-A).

Subtask 10-11-00-170-056-A G.


Condition for flushing You must flush the air data system if there is one or more of the conditions that follow: . all probe covers not installed immediately after the last flight of the aircraft . report on air data problems on the previous flight . the aircraft was in aggressive weather conditions (dust or sand or snow storm, or heavy rain) or an aggressive environment with foreign materials that can be caught in the lines . a probe cover not found in position during periodical ground check 7 days . a probe cover not found in position at the RETURN TO SERVICE TIME . the aircraft parking period is more than 15 days (after a parking period renewal)

(2)

If one of these conditions occurs, you must flush the air data system. NOTE :

Flushing is not necessary if none of the above conditions occur.

(a)


(b)


(c)


Subtask 10-11-00-630-050-B H.


5.

Do the depreservation of the engines (Ref. TASK 71-00-00-550-011-A).


AES

Close-up (1)

De-energize the aircraft electrical circuits supplied from the external power (Ref. TASK 24-41-00-862-002-A) or (Ref. TASK 24-41-00-862-002-A-01) or (Ref. TASK 24-41-00-862-002-A-02).

(2)

Remove the tag from the Captain side stick or write in the log book that the protection covers/devices are no longer installed.

(3)

Remove all the fixtures, tools, test and support equipment used during this procedure.

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-554-004-A Return to Operation after Parking not more than 12 Weeks CAUTION :

1.


Reason for the Job This procedure gives the instructions necessary to operate an aircraft again after a parking period of not more than 12 weeks.

2.





No specific

AR

B.

WARNING NOTICE(S)


REFERENCE 10-11-00-555-014-A


12-14-32-614-003-A

Check of MLG Shock Absorber Charge Pressure

12-14-32-614-004-A 12-21-11-615-002-A

Check NLG Shock Absorber Charge Pressure External Cleaning

12-32-28-281-001-A 12-32-28-281-003-A


24-38-51-400-001-A 24-41-00-861-002-A 24-41-00-861-002-A-01

Installation of the Batteries Energize the Aircraft Electrical Circuits from the External Power Energize the Aircraft Electrical Circuits from the APU

24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


28-11-00-280-002-A 29-10-00-200-001-A 32-41-00-210-002-A

Structural Fuel Tank Leaks - General Information Check Fluid Level on Reservoir Indicators Inspection/Check of the Wheels and Tires

32-41-00-210-003-A


34-10-00-170-001-A 34-10-00-170-002-A 34-10-00-170-003-A

Flushing of the Principal Total Pressure Lines Flushing of the Principal Static Pressure Lines Draining and Flushing of Standby Pneumatic Circuits

AES

10-11-00 PB201



DESIGNATION Opening of the Passenger/Crew Door

52-10-00-410-001-A


52-30-00-860-002-A

Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump

** On A/C 003-003 52-30-00-860-006-A


52-30-00-860-008-A

Close the Bulk Cargo-Compartment Door

71-00-00-550-011-A

Depreservation of the Power Plant

3.


4.



(2)





(2)

Make sure that there is no leakage from: . the wings . the lower fuselage . the landing gear . the engines . the APU . the horizontal and vertical stabilizers.


Subtask 10-11-00-020-063-A B.

Removal of the Protection Equipment (1)

Remove all the protection equipment from the engines, the APU and the probes (Ref. TASK 10-11-00-555-014-A).

Subtask 10-11-00-860-066-A C.

AES


Connect the batteries 2PB1, 2PB2 and make sure that the battery charge is correct (Ref. TASK 24-38-51-400-001-A).

(2)


(3)

On the overhead panel 25VU, on the CABIN PRESS section: . Push the DITCHING pushbutton switch to open the ventilation skin valves and the outflow valve.

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-680-053-A D.



(2)

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from the ACT, if installed (Ref. AMM 12-32-28-281-005) . NOTE :

(3)


Do a check of all the fuel tanks for leakage (Ref. TASK 28-11-00-280-002-A).

Subtask 10-11-00-210-062-A E.

Inspection (1)

Do a check of the charge pressure of the landing-gear shock absorbers: . for the NLG (Ref. TASK 12-14-32-614-004-A) . for the MLG (Ref. TASK 12-14-32-614-003-A)

(2)


(3)

Do a check of the tire condition (Ref. TASK 32-41-00-210-002-A).

(4)

Do a check of the hydraulic reservoir level (Ref. TASK 29-10-00-200-001-A).

Subtask 10-11-00-170-054-A F.


Condition for flushing You must flush the air data system if there is one or more of the conditions that follow: . all probe covers not installed immediately after the last flight of the aircraft . report on air data problems on the previous flight. . the aircraft was in aggressive weather condition (dust or sand or snow storm, or heavy rain) or an aggressive environment with foreign materials that can be caught in the lines . any probe cover not found in position during periodical ground check 7 days . any probe covers not found in position at the RETURN TO SERVICE TIME . the aircraft parking period is more than 15 days

(2)

If one of these conditions is missing, you must flush the air data system. (a)


(b)


(c)


** On A/C 004-099 Subtask 10-11-00-010-055-A G.

Get Access (1)

AES

Open and close all the access doors to the pressurized area and make sure that they operate correctly : . the AFT and FWD passenger/crew doors (Ref. TASK 52-10-00-010-001-A) and (Ref. TASK 52-10-00-410-001-A) . the FWD and AFT cargo compartments (Ref. TASK 52-30-00-860-002-A) and (Ref. TASK 52-30-00-860-002-A)

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C 003-003 Subtask 10-11-00-010-055-B G.

Get Access (1)

Open and close all the access doors to the pressurized area and make sure that they operate correctly : . the AFT and FWD passenger/crew doors (Ref. TASK 52-10-00-010-001-A) and (Ref. TASK 52-10-00-410-001-A) . the FWD and AFT cargo compartments (Ref. TASK 52-30-00-860-002-A) and (Ref. TASK 52-30-00-860-002-A) . the bulk cargo-compartment door (Ref. TASK 52-30-00-860-006-A) and (Ref. TASK 52-30-00-860-008-A)

** On A/C ALL Subtask 10-11-00-630-051-B H.


5.

Do the depreservation of the engines (Ref. TASK 71-00-00-550-011-A).


AES

Close-up (1)


(2)

Remove the tag from the Captain side stick or write in the log book that the protection covers/devices are no longer installed.

(3)


10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-011-A Renewal of 15-Day Parking Period CAUTION :


CAUTION :


1.

Reason for the Job This procedure gives the operator the possibility to do the parking procedure of 15 days again one time.

2.



REFERENCE 10-11-00-200-002-A


10-11-00-200-003-A


12-32-28-281-001-A 12-32-28-281-003-A


3.


4.

Not Applicable



Do a periodic ground check at 7-day intervals (Ref. TASK 10-11-00-200-002-A) and at 15-day intervals (Ref. TASK 10-11-00-200-003-A).

(2)


(3)

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from ACT, if installed (Ref. AMM 12-32-28-281-005) . NOTE :

(4)

AES



10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-012-A Renewal of 12-Week Parking Period CAUTION :

1.


Reason for the Job This procedure gives the operator the possibility to do the parking procedure of 12 weeks again several times.

2.



REFERENCE 10-11-00-554-004-A

DESIGNATION Return to Operation after Parking not more than 12 Weeks

10-11-00-555-008-A

Parking Procedure in Flight-ready Condition (Parking of not more than 12 Weeks)

10-11-00-555-013-A 32-33-00-720-001-A

Installation of the Aircraft Protection Equipment Functional Check of Free-Fall Extension

3.


4.

Not Applicable


Preparation of the Aircraft (1)

Do the full return to operation after parking not more than 12 weeks procedure (Ref. TASK 10-11-00-554-004-A).

(2)

Refer to the aircraft maintenance program and make sure that you do all the scheduled maintenance tasks that are due.

Subtask 10-11-00-555-060-A B.

Procedure (1)

Do a short non-revenue flight within aircraft standard envelope.

Subtask 10-11-00-555-061-A C.

Parking Period (1)

The new parking period for 12 weeks starts from the end of this last flight. NOTE :

AES

After the 4th successive renewal, do a landing-gear free-fall extension test (Ref. TASK 32-33-00-720-001-A)

10-11-00 PB201




AES

Put the Aircraft in Parking Configuration (1)

Let the engines and the APU become cool and install protection covers/plugs on the fuselage, the engines and the APU area (Ref. TASK 10-11-00-555-013-A).

(2)

Do the 12-week parking procedure (Ref. TASK 10-11-00-555-008-A)

(3)


10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-013-A Installation of the Aircraft Protection Equipment WARNING :

DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS, SENSORS (STATIC, PITOT, TAT, AOA). USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OF THE AIRCRAFT. THE SPECIFIED TOOLS: GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT, ARE EASY TO SEE FROM THE GROUND, ARE EASY TO REMOVE. IF YOU USE TAPE, THERE IS A RISK THAT SOME TAPE, OR ADHESIVE FROM THE TAPE, WILL STAY ON THE PROBES, DUCTS OR SENSORS. THIS CAN CAUSE INCORRECT INDICATIONS ON THE RELATED COCKPIT INSTRUMENTS.

WARNING :

YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.

1.

Reason for the Job Self explanatory

2.




QTY DESIGNATION 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE

No specific

1

WARNING NOTICE(S)

98A10001005000 98A10001013000 98A10001500000 98D10003001000 98D10003003000 98D10007512000 98D10007513000 98D10103500001 IAE1N20008 IAE1N20400

3 2 3 2 3 1 1 2 2 2

COVER-PITOT PROBE COVER-TOTAL TEMP SENSOR COVER-SLIP ON,ANGLE OF ATTACK SENSOR COVER-INLET COWL ENGINE COVER - SLIP-ON, AOA SENSOR COVER-EXHAUST DUCT,APU COVER-OILCOOLER OUTLET,APU COVER-STATIC PROBE COVER-COMMON NOZZLE COVER-INLET COWL

B.


REFERENCE (Ref. Fig. 10-11-00-991-00100-B - Protective Equipment)

DESIGNATION

(Ref. Fig. 10-11-00-991-00400-B - Protective Equipment) (Ref. Fig. 10-11-00-991-00700-A - Protective Equipment) (Ref. Fig. 10-11-00-991-00600-A - Protective Equipment)

AES

10-11-00 PB201




4.


On the panel 115VU: . Make sure that the ENG/MODE selector switch is in the NORM position. . Make sure that the ENG/MASTER 1(2) control lever is in the OFF position.

(2)

On the panel 25VU: . make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).

(3)

Put a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the systems while you install the protective devices on the aircraft.

(4)

Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.


Installation of the Protection Devices on the Fuselage (Ref. Fig. 10-11-00-991-00100-B - Protective Equipment) WARNING : MAKE SURE THAT THE PROBES, THE ENGINE AND THE APU ARE COOL BEFORE INSTALLATION OF THE PROTECTIVE DEVICES. IF THE PROBES ARE HOT, THERE IS A RISK OF INJURY AND THE PROTECTIVE DEVICES CAN MELT.

(1)

Protection of the 2 total temperature sensors . Put the COVER-TOTAL TEMP SENSOR (98A10001013000) in position.

(2)

Protection of the 3 pitot probes . Put the COVER-PITOT PROBE (98A10001005000) in position.

(3)

Protection of the 3 angle-of-attack sensors . Put the COVER-SLIP ON,ANGLE OF ATTACK SENSOR (98A10001500000) or COVER - SLIPON, AOA SENSOR (98D10003003000) in position.

(4)

Protection of the 6 static probes . Put the COVER-STATIC PROBE (98D10103500001) in position.

Subtask 10-11-00-555-070-B B.

Installation of the Protection Devices on the Engines (Ref. Fig. 10-11-00-991-00400-B - Protective Equipment) (Ref. Fig. 10-11-00-991-00700-A - Protective Equipment) WARNING : MAKE SURE THAT THE PROBES, THE ENGINE AND THE APU ARE COOL BEFORE INSTALLATION OF THE PROTECTIVE DEVICES. IF THE PROBES ARE HOT, THERE IS A RISK OF INJURY AND THE PROTECTIVE DEVICES CAN MELT.

AES

(1)

Protection of the engine air intakes . Put the COVER-INLET COWL (IAE1N20400) or COVER-INLET COWL ENGINE (98D10003001000) in position.

(2)

Protection of the engine exhaust nozzles . Put the COVER-COMMON NOZZLE (IAE1N20008) in position.

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-555-071-A C.

Installation of the Protection Devices on the APU Area (Ref. Fig. 10-11-00-991-00600-A - Protective Equipment) WARNING : MAKE SURE THAT THE PROBES, THE ENGINE AND THE APU ARE COOL BEFORE INSTALLATION OF THE PROTECTIVE DEVICES. IF THE PROBES ARE HOT, THERE IS A RISK OF INJURY AND THE PROTECTIVE DEVICES CAN MELT.

5.

(1)

Protection of the APU exhaust duct . Put the COVER-EXHAUST DUCT,APU (98D10007512000) in position.

(2)

Protection of the outlet duct of the APU oil cooler . Put the COVER-OILCOOLER OUTLET,APU (98D10007513000) in position.


Close-up (1)

AES


10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL STA4762/ FR6 STA4967/ FR7

A

STA8966/ FR23 STA9499/ FR24

STA5394/ FR9 STA5594/ FR10

STATIC PROBE (Qt.2)

STA10033/ FR25 STA10566/ FR26

D

C D

C

E

E

B B

B

C

B

A

ANGLE OF ATTACK (Qt.3)

A E TOTAL TEMPERATURE SENSOR (Qt.2)

C PITOT PROBE (Qt.3)

D STATIC PROBE (Qt.2)

N_MM_101100_2_AAN0_01_00

AES

FIGURE 10-11-00-991-00100-B SHEET 1 Protective Equipment

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL

A

A A

B

B

IAE 20400 TRANSPORTATION PARKING ONLY

N_MM_101100_2_AEX0_01_00

AES

FIGURE 10-11-00-991-00400-B SHEET 1 Protective Equipment

10-11-00 PB201



A

IAE1N20008

R

E M O V E

B E F O R

E

F L I

G H T

A

13670

N_MM_101100_2_AJM0_01_00

AES

FIGURE 10-11-00-991-00700-A SHEET 1 Protective Equipment

10-11-00 PB201



B

A

B

A

N_MM_101100_2_ABM0_01_00

AES

FIGURE 10-11-00-991-00600-A SHEET 1 Protective Equipment

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-014-A Removal of the Aircraft Protection Equipment 1.


2.




B.

QTY DESIGNATION 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE


REFERENCE (Ref. Fig. 10-11-00-991-00100-B - Protective Equipment)

DESIGNATION

(Ref. Fig. 10-11-00-991-00400-B - Protective Equipment) (Ref. Fig. 10-11-00-991-00700-A - Protective Equipment) (Ref. Fig. 10-11-00-991-00600-A - Protective Equipment) 3.


4.


Make sure that the ENG/MODE selector switch is in the NORM position.

(2)

Make sure that the ENG/MASTER 1(2) control lever is in the OFF position.

(3)

Make sure that a WARNING NOTICE(S) is in position in the cockpit to tell persons not to operate the systems while you remove the protective devices on the aircraft.

(4)

Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.


Removal of the Protection Devices from the Fuselage (Ref. Fig. 10-11-00-991-00100-B - Protective Equipment) (1)

Protection of the 2 total temperature sensors . Remove the COVER-TOTAL TEMP SENSOR (98A10001013000).

(2)

Protection of the 3 pitot probes . Remove the COVER-PITOT PROBE (98A10001005000).

(3)

Protection of the 3 angle-of-attack sensors . Remove the COVER-SLIP ON,ANGLE OF ATTACK SENSOR (98A10001500000) or COVER SLIP-ON, AOA SENSOR (98D10003003000).

(4)

Protection of the 6 static probes . Remove the COVER-STATIC PROBE (98D10103500001).

Subtask 10-11-00-555-076-B B.

AES

Removal of the Protection Devices from the Engines (Ref. Fig. 10-11-00-991-00400-B - Protective Equipment)

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (Ref. Fig. 10-11-00-991-00700-A - Protective Equipment) (1)

Protection of the engine air intakes . Remove the COVER-INLET COWL (IAE1N20400) or COVER-INLET COWL ENGINE (98D10003001000).

(2)

Protection of the engine exhaust nozzles . Remove the COVER-COMMON NOZZLE (IAE1N20008).

Subtask 10-11-00-555-077-A C.

5.

Removal of the Protection Devices from the APU Area (Ref. Fig. 10-11-00-991-00600-A - Protective Equipment) (1)

Protection of the APU exhaust duct . Remove the COVER-EXHAUST DUCT,APU (98D10007512000).

(2)

Protection of the outlet duct of the APU oil cooler . Remove the COVER-OILCOOLER OUTLET,APU (98D10007513000).


Close-up (1)

AES


10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-555-015-A Procedure for the Installation of Wheel Chocks on Aircraft WARNING :

1.

OBEY THESE SAFETY PRECAUTIONS DURING MOVEMENT OF THE AIRCRAFT (TOWING, PUSHBACK OR TAXIING). MAKE SURE THAT: THE PATH OF THE AIRCRAFT IS CLEAR OF PERSONS, EQUIPMENT AND OTHER OBSTACLES. NO PERSONS GO NEAR THE TOW TRACTOR, TOWBAR, LANDING GEARS, ENGINE NACELLES OR BELOW THE AIRCRAFT FUSELAGE. ONLY QUALIFIED PERSONS ARE ON THE TRACTOR AND NO PERSONS SIT OR STAND ON THE TOWBAR. NO PERSONS GO NEAR THE AIRCRAFT BEFORE IT IS FULLY STOPPED. THERE IS A RISK OF INJURY OR DEATH IF YOU DO NOT OBEY THESE INSTRUCTIONS.

Reason for the Job This task gives general recommendations about the location of wheel chocks for different aircraft conditions. NOTE :

2.

The operator can use these guidelines and his experience and knowledge of the local regulations to make a decision.





DESIGNATION

REFERENCE (Ref. Fig. 10-11-00-991-01000-A - Location of Wheel Chocks)

DESIGNATION

B.

3.



Wheel Chock Specifications (1)

Use CHOCK - WHEEL(S) that agree with SAE AIR4905 standard.

Subtask 10-11-00-941-059-A B.


4.

Make sure that the aircraft is fully stopped before you go near the landing gear to install the wheel chocks.


Location of Wheel Chocks (Ref. Fig. 10-11-00-991-01000-A - Location of Wheel Chocks) (1)

Aircraft in flight-ready condition (a)

AES

Put the CHOCK - WHEEL(S) in front of and behind the outboard wheel of the right and left MLG.

10-11-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (b)

(c)

There must be a small distance between the tires and the CHOCK - WHEEL(S). NOTE :

Weight changes can have an effect on the wheelbase, which can cause the tires to catch the chocks.

NOTE :

If you put CHOCK - WHEEL(S) at the NLG because of the local regulations, make sure that they do not touch the tires.

If the aircraft is parked on a slope, also put CHOCK - WHEEL(S) on the down-slope side of the inboard wheel of each MLG. Make sure that the down-slope chocks touch the wheels and that the up-slope chocks do not touch the wheels. NOTE :

(2)

Aircraft in flight-ready condition with wind speed more than 25 Kts (a)

Put the CHOCK - WHEEL(S) behind and in front of the NLG and MLG wheels.

(b)


(c)

On slippery surfaces, or in strong wind conditions, we recommend to apply the parking brake.

Aircraft in parking or storage condition (a)

Put the CHOCK - WHEEL(S) behind and in front of the NLG and MLG wheels.

(b)


(c)


If the aircraft is parked on a slope, put the CHOCK - WHEEL(S) against the tires of the downslope wheels. NOTE :

AES


If the aircraft is parked on a slope, put the CHOCK - WHEEL(S) against the tires of the downslope wheels. NOTE :

(3)

On slippery surfaces, we recommend to use more CHOCK - WHEEL(S) and to apply the parking brake.

On slippery surfaces, or in strong wind conditions, we recommend to apply the parking brake. The parking brake has sufficient pressure for 12 hours.

10-11-00 PB201



AIRCRAFT IN FLIGHT READY CONDITION, WIND SPEED LESS THAN 25KTS

AIRCRAFT IN FLIGHT READY CONDITION, WIND SPEED MORE THAN 25KTS OR AIRCRAFT IN PARKING OR STORAGE CONDITION

N_MM_101100_2_BCM0_01_00

AES

FIGURE 10-11-00-991-01000-A SHEET 1 Location of Wheel Chocks

10-11-00 PB201



PARKING - INSPECTION/CHECK ** On A/C ALL Task 10-11-00-200-002-A Periodic Ground Check at 7-day Intervals 1.

Reason for the Job This procedure gives the periodic ground check at 7-day intervals for a parking period of not more than 15 days or of not more than 12 weeks (aircraft in flight-ready condition).

2.



REFERENCE 29-10-00-200-001-A 32-41-00-210-003-A

3.

DESIGNATION Check Fluid Level on Reservoir Indicators Inspection/Check of the Tire Pressure


4.

Not Applicable


Inspection (1)

AES


Make sure that the protective equipment is correctly installed. . Make a record in the log book if a protective cover is missing on the pitot or static probes.

(b)

Make sure that there are no leaks from: . the wings . the lower fuselage . the landing gears . the engines . the APU . the horizontal and vertical stabilizer.

(c)

Make sure that there are no signs of bird nesting in all areas of the aircraft to which birds have access.

(d)

Do a check for bird excrements. If there are birds excrements, remove them.

(e)

Do a check of the outer skin for unusual contamination.

(2)

Make sure that the extension of the landing-gear shock absorbers is correct.

(3)


(4)


10-11-00 PB601




AES

Not Applicable

10-11-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-200-003-A Periodic Ground Check at 15-day Intervals 1.

Reason for the Job This procedure gives the periodic ground check at 15-day intervals for a parking period of not more than 12 weeks (aircraft in flight-ready condition).

2.



REFERENCE 10-11-00-555-013-A

DESIGNATION Installation of the Aircraft Protection Equipment

10-11-00-555-015-A 12-32-28-281-001-A 12-33-21-618-001-A-02

Procedure for the Installation of Wheel Chocks on Aircraft Drain Water Content Pre-conditioning with the APU

24-38-51-000-001-A 24-38-51-400-001-A 24-41-00-861-002-A 24-41-00-861-002-A-01

Removal of the Batteries Installation of the Batteries Energize the Aircraft Electrical Circuits from the External Power Energize the Aircraft Electrical Circuits from the APU

24-41-00-861-002-A-02


24-41-00-862-002-A 24-41-00-862-002-A-01

De-energize the Aircraft Electrical Circuits Supplied from the External Power De-energize the Aircraft Electrical Circuits Supplied from the APU

24-41-00-862-002-A-02


27-24-00-710-001-A

Operational Test of the Rudder Hydraulic Actuation

27-50-00-866-008-A-01

Extension of the Flaps/Slats on the Ground

27-92-41-710-001-A

Operational Test of the Side Stick Assembly

29-10-00-200-001-A 30-11-00-710-001-A

Check Fluid Level on Reservoir Indicators Operational Test of the Wing Ice-Protection System

30-21-00-710-002-A

Operational Test of the Engine Air Intake Ice Protection (with the Engines in operation)

32-41-00-210-002-A

Inspection/Check of the Wheels and Tires

32-41-00-210-003-A


32-42-00-710-001-A 32-43-00-710-001-A

Operational Check of the Normal Braking System Operational Check of Alternate Braking System

** On A/C POST SB 32-1235 FOR A/C 003-008 32-48-00-720-001-A 32-51-00-720-003-A

Functional Test of the Brake Fans Functional Test of the Nose Wheel Steering with the Handwheel

32-51-00-720-004-A

Functional Test of the Nose Wheel Steering with the Pedals

36-11-00-710-003-A

Operational Test of the Bleed Air System

** On A/C 006-099 49-00-00-860-005-A 49-00-00-860-005-A-01

APU Start by External Power APU Start by Batteries

49-00-00-860-006-A

APU Shutdown by External Power

AES

10-11-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 49-00-00-860-006-A-01

DESIGNATION

APU Shutdown by Batteries

** On A/C 003-005 49-00-00-860-008-A 49-00-00-860-008-A-01

APU Start by External Power APU Start by Batteries

49-00-00-860-009-A

APU Shutdown by External Power (131-9(A))

49-00-00-860-009-A-01

APU Shutdown by Batteries (131-9(A))

71-00-00-710-018-A 71-00-00-710-043-A

Discontinued Start, Restart and Shutdown Procedures Normal Engine Automatic Start Procedure

78-31-00-710-041-A

Operational Test of the Thrust Reverser System with the CFDS

78-31-00-710-041-A-01

Operational Test of the Thrust Reverser without the CFDS and Engine not Running

78-31-00-710-041-A-02

Operational test of the Thrust Reverser without the CFDS and Engine Running

3.


Removal of Protections (1)

Remove all protection covers/plugs from the fuselage, the engines and the APU area.

Subtask 10-11-00-860-079-A B.


Install and connect the batteries 2PB1 and 2PB2 and make sure that the charge is correct (Ref. TASK 24-38-51-400-001-A).

(2)


(3)

On the overhead panel 25 VU, on the CABIN PRESS section: . release the DITCHING pushbutton switch to open the avionics ventilation skin valves and the outflow valve. NOTE :

4.

Make sure that the avionics ventilation continues to operate correctly.


AES

Inspection (1)

Make sure that the extension of the landing gear shock absorbers is correct.

(2)


(3)

Do a check of the tire and wheel condition (Ref. TASK 32-41-00-210-002-A).

(4)


10-11-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-11-00-700-052-A B.

Test of the Landing Gear (1)

Do the test of the nose wheel steering with the handwheel and with the pedals (Ref. TASK 32-51-00-720-003-A) (Ref. TASK 32-51-00-720-004-A).

(2)

Do the test of the normal braking system and alternate braking system (Ref. TASK 32-42-00-710-001A) (Ref. TASK 32-43-00-710-001-A).

(3)

Do the test of the brake fans (if installed) ** On A/C POST SB 32-1235 FOR A/C 003-008 (Ref. TASK 32-48-00-720-001-A).

** On A/C ALL Subtask 10-11-00-700-055-B C.

Test of the APU, Engines and Systems (1)

Start the APU: . for a GTCP 36-300 APU: (Ref. AMM 49-00-00-860-003) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-00-00-860-005-A) or (Ref. TASK 49-00-00-860-005-A-01) . for a 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-00-00-860-008-A)(Ref. TASK 49-00-00-860-008-A-01)

(2)

Operate the air conditioning system ** On A/C ALL (Ref. TASK 12-33-21-618-001-A-02)

(3)

Start the engines and let them become stable at ground idle (Ref. TASK 71-00-00-710-043-A).

(4)

Stop the APU: . for a GTCP 36-300 APU: (Ref. AMM 49-00-00-860-004) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-00-00-860-006-A) or (Ref. TASK 49-00-00-860-006-A-01) . for a 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-00-00-860-009-A)(Ref. TASK 49-00-00-860-009-A-01)

(5)

Do a thrust reverser full cycle ** On A/C ALL (Ref. TASK 78-31-00-710-041-A) or (Ref. TASK 78-31-00-710-041-A-01) or (Ref. TASK 78-31-00-710-041-A-02).

(6)

AES

Do the test of the bleed air system (Ref. TASK 36-11-00-710-003-A) and make sure that the related BLEED PRESS and BLEED TEMP indications are satisfactory.

10-11-00 PB601



Do the test of the wing ice-protection system (Ref. TASK 30-11-00-710-001-A). NOTE :

You can do the operational test of the wing ice-protection system with a Ground Air Power Cart (GAPC).

(8)

Do the test of the engine air intake ice-protection (Ref. TASK 30-21-00-710-002-A).

(9)


Subtask 10-11-00-866-054-A D.

Flight Control Movement (1)

Operate all the flight control surfaces on full travel and make sure that they operate correctly. (a)

Move the flap and slat control lever one time from 0˚ to FULL and back to extend and retract the slats and the flaps (Ref. TASK 27-50-00-866-008-A-01).

(b)

Push the left then the right pedal until it touches the mechanical stop, to operate the rudder (Ref. TASK 27-24-00-710-001-A).

(c)

Move the side stick to: . the left and right roll position to operate the spoilers and the ailerons . the nose-down and nose-up position to operate the elevators (Ref. TASK 27-92-41-710-001A).

(d)

Move the pitch trim control wheel to the nose up and nose down position to operate the THS.

(e)


Subtask 10-11-00-281-062-A E.

Inspection of the Fuel System (1)

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from the ACT, if installed (Ref. AMM 12-32-28-281-005) .

(2)

Do a check of the fuel level in the tanks: (a)

if necessary refuel the tank(s): . to 30 % minimum if no contamination occurred . to 90 % minimum if contamination occurred. NOTE :

We recommend that you do not mix fuel treated with different biocides.

Subtask 10-11-00-584-054-A F.

Movement of the Aircraft NOTE :

(1)

You can ignore this step if you moved the aircraft for the engine run-up.

Remove the wheel chocks that you installed during the parking procedure. NOTE :

AES

Before remove the wheel chocks, make sure that the parking brake is ON and pressurized.

(2)

Move the aircraft, by 1/4 turn of the wheels, to prevent damage to the tires and brinelling of the bearings.

(3)

Put the wheel chocks in position: (Ref. TASK 10-11-00-555-015-A)

10-11-00 PB601



5.


On the overhead panel 25 VU, on the CABIN PRESS section: . Push the DITCHING pushbutton switch to close the ventilation skin valves and the outflow valve.

(2)

Disconnect and remove the batteries 2PB1 and 2PB2 (Ref. TASK 24-38-51-000-001-A).

(3)



Put the Aircraft in Parking Configuration (1)

AES

Let the engines and the APU become cool and install protection covers/plugs on the fuselage, the engines and the APU area (Ref. TASK 10-11-00-555-013-A).

10-11-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-11-00-200-004-A Periodic Ground Check at 1-month Intervals 1.

Reason for the Job This procedure gives the periodic ground check at 1-month intervals for a parking period of not more than 12 weeks (aircraft in flight-ready condition).

2.



REFERENCE 12-32-28-281-003-A

3.

DESIGNATION Sample Fuel for Microbiological Contamination Analysis


4.

Not Applicable


AES

Inspection (1)

Make sure that the extension of the landing gear shock absorbers is correct.

(2)

Do a check of the pressure of the oxygen cylinders.

(3)


(4)


10-11-00 PB601



STORAGE - MAINTENANCE PRACTICES ** On A/C ALL Task 10-12-00-553-005-A Storage Procedures 1.

Reason for the Job This task gives the procedures for: . storage of the aircraft for a period of not more than 6 months . storage of the aircraft for a period of not more than 2 years . ground checks during storage . return to operation after storage . renewal of storage procedure

2.



REFERENCE 10-12-00-200-006-A


10-12-00-200-007-A


10-12-00-200-008-A 10-12-00-200-009-A

Periodic Ground-Check at 1-month Interval Periodic ground-check at 3-month interval

10-12-00-200-010-A 10-12-00-553-006-A

Periodic Ground Check at 6-month Intervals Storage Procedure (Storage Not More than 6 Months)

10-12-00-553-007-A

Storage Procedure (Storage Not More than 2 Years)

10-12-00-553-008-A

Renewal for 6 Months Storage Period

10-12-00-553-009-A 10-30-00-554-005-A

Renewal for 2 Years Storage Period Return to Operation after Storage Period

3.


4.

Not Applicable


Procedure to store the aircraft with related procedures to do perodic ground checks, return to operation and renew the storage procedure (1)

AES

Storage procedure for a period of not more than 6 months (Ref. TASK 10-12-00-553-006-A) (a)

During the storage period of not more than 6 months, you must do periodic ground checks: . at 7-day intervals (Ref. TASK 10-12-00-200-006-A) . at 15-day intervals (Ref. TASK 10-12-00-200-007-A) . at 1-month interval (Ref. TASK 10-12-00-200-008-A) . at 3-month intervals (Ref. TASK 10-12-00-200-009-A).

(b)

You can do again the procedure to store the aircraft not more than six months one time only (Ref. TASK 10-12-00-553-008-A).

(c)

Return to operation after a storage period (Ref. TASK 10-30-00-554-005-A).

10-12-00 PB201



AES

Storage procedure for a period not more than 2 years (Ref. TASK 10-12-00-553-007-A). (a)

During storage period not more than 2 years, you must do perodic ground-checks: . at 7-day intervals (Ref. TASK 10-12-00-200-006-A). . at 15-day intervals (Ref. TASK 10-12-00-200-007-A). . at 1-month interval (Ref. TASK 10-12-00-200-008-A). . at 3-month intervals (Ref. TASK 10-12-00-200-009-A). . at 6-month intervals (Ref. TASK 10-12-00-200-010-A).

(b)

Return to operation after a storage period (Ref. TASK 10-30-00-554-005-A).

(c)

The procedure to store the aircraft 2 years can be renewed (Ref. TASK 10-12-00-553-009-A).

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-553-006-A Storage Procedure (Storage Not More than 6 Months) CAUTION :


CAUTION :


1.

Reason for the Job This procedure gives the preservation steps for a storage period of not more than 6 months.

2.





No specific

AR

TALCUM POWDER

No specific

1

WARNING NOTICE(S)

B.



Material No: 04-001 Material No: 04-004 Material No: 04-011 Material No: 05-005 Material No: 05-027 Material No: 05-043 Material No: 08-052 Material No: 15-002

AES

DESIGNATION

DESIGNATION

OILS MINERAL OIL (LOW TEMP) COMMON GREASES WHEEL BEARING MINERAL GREASE COMMON GREASES SYNTH. ESTER BASED GREASE HIGH PRESSURE COMMON GREASES SILICONE GREASE PNEUMATIC SYST AND SEALS SPECIAL MATERIALS CORROSION PREVENTIVE SPECIAL MATERIALS SPECIAL MATERIALS VARNISH P.T.F.E SPRAY BONDING AND ADHESIVE COMPOUNDS SELF ADHESIVE ALUMINIUM TAPE STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL C.


REFERENCE 05-57-00-200-001-A

10-11-00-555-013-A 10-11-00-555-015-A 10-20-00-556-001-A 10-20-00-556-001-A-01

DESIGNATION

Aircraft Stability Installation of the Aircraft Protection Equipment Procedure for the Installation of Wheel Chocks on Aircraft Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs

12-16-38-613-001-A

Servicing of the Toilet System

12-21-11-615-002-A

External Cleaning

12-21-12-100-002-A


12-21-12-100-003-A


12-21-12-100-004-A


12-21-12-100-005-A 12-21-12-100-006-A

Cleaning of the Seat Covers and the Curtains Cleaning of the Light Alloy and Steel Components

12-21-12-100-007-A


12-21-12-100-008-A


12-21-12-100-009-A


12-22-27-640-003-A 12-22-27-640-004-A

Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut Lubricate all Carriage Rollers on all Flap Tracks

12-22-27-640-005-A

Lubrication of Spoiler No.1 to 5 Servo Control Bearings

12-22-27-640-006-A

Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth

12-22-27-640-007-A ** On A/C 003-004

Lubrication of the THS Mechanical Control Chains

12-22-27-640-008-A 12-22-32-640-001-A

Remove Flap Rotary Actuators For Regreasing Lubrication of Main Landing Gear and Doors

12-22-32-640-002-A

Lubrication of Nose Landing Gear and Doors

12-22-52-640-002-A 12-22-52-640-006-A


** On A/C 003-003 12-22-52-640-007-A


12-22-52-640-008-A 12-22-52-640-009-A


12-22-52-640-014-A


12-22-52-640-016-A 12-22-53-640-001-A

Lubrication of the Hinge-Arm Support-Fitting Bearings Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004

12-22-55-640-001-A

Lubrication of Rudder Hinge Bearing No. 6 with Grease Mat. No. 04-004

12-24-38-680-001-A


AES

10-12-00 PB201



DESIGNATION Cold Weather Maintenance - Air Conditioning

12-31-24-660-001-A 12-31-25-660-001-A


12-31-27-660-001-A


12-31-28-660-001-A 12-31-31-660-001-A


12-31-32-660-001-A 12-31-35-660-001-A

Cold Weather Maintenance - Landing Gear Cold Weather Maintenance - Oxygen System

12-31-38-660-001-A


12-31-49-660-001-A 12-31-51-660-001-A 12-31-52-660-001-A 12-31-71-660-001-A 12-32-28-281-001-A 12-32-28-281-003-A 12-34-24-869-002-A

Cold Weather Maintenance - Auxiliary Power Unit Cold Weather Maintenance - Structure Cold Weather Maintenance - Doors Cold Weather Maintenance - Power Plant Drain Water Content Sample Fuel for Microbiological Contamination Analysis Aircraft Grounding for the Maintenance Operations

23-71-35-000-001-A

Removal of the Cockpit Voice Recorder (CVR) 1RK

24-21-00-600-040-A

Preservation/Storage/Return to Service of the IDG

24-38-51-000-001-A 24-41-00-861-002-A


24-41-00-861-002-A-01


24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


26-21-41-000-001-A

Removal of the Engine Fire-Extinguisher Bottle

26-22-41-000-001-A

Removal of the Fire Extinguisher Bottle

** On A/C 005-099 26-23-41-000-004-A

Removal of the Cargo Fire-Extinguisher Bottle

27-54-00-710-002-A

Operational Test of the Flap and Slat Systems

28-11-00-600-010-A

Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig

28-11-00-600-010-A-01 28-11-00-600-010-A-02 28-11-00-600-010-A-03

Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig

29-10-00-863-003-A

Pressurize the Blue Hydraulic System with a Ground Power Supply

29-10-00-863-003-A-01 29-10-00-864-003-A

Pressurize the Blue Hydraulic System with the Blue Electric Pump Depressurize the Blue Hydraulic System

AES

10-12-00 PB201



DESIGNATION Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump

29-23-00-864-001-A 29-24-00-863-001-A

Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU Pressurize the Yellow Hydraulic System with the Electric Pump

29-24-00-864-001-A

Depressurize the Yellow Hydraulic System

30-45-00-040-002-A

Deactivation of the Rain Repellent System

31-33-55-000-001-A

Removal of the Digital Flight Data Recorder (DFDR)

32-00-00-481-001-A


32-12-00-010-001-A 32-12-00-410-001-A 32-22-00-010-001-A

Open the Main Gear Doors for Access Close the Main Gear Doors after Access Nose Gear Doors - Ground Doors Opening

32-22-00-410-001-A

Nose Gear Doors - Ground Doors Closing

32-40-00-200-001-A

Inspection/Check of the Wheels & Brakes

32-41-00-210-003-A


32-41-11-400-006-A Installation of the MLG Wheel 32-41-12-400-001-A Installation of the NLG Wheel ** On A/C POST SB 32-1235 FOR A/C 003-008 32-48-51-000-005-A

Removal of the Fan Assy

33-51-38-000-002-A

Removal of the Battery of the Emergency Power-Supply Unit

34-10-00-170-001-A 34-10-00-170-002-A


34-10-00-170-003-A


** On A/C 006-099 49-20-00-210-001-A

APU Power Plant Visual Inspection (APS 3200)

49-20-00-600-002-A

Preservation/Storage/Return to Service of APU (APS 3200)

** On A/C 003-005 49-20-00-600-003-A

Preservation/Storage/Return to Service of APU (131-9(A))

52-10-00-010-001-A


52-10-00-410-001-A


52-30-00-860-001-A


52-30-00-860-002-A ** On A/C 003-003 52-30-00-860-006-A 52-30-00-860-008-A

Open the Bulk Cargo-Compartment Door Close the Bulk Cargo-Compartment Door

53-59-00-210-001-A

Operational Check of Single Drain Pipe Aft of FR70 from Outside

54-50-00-200-001-A 71-00-00-550-010-A

General Visual Inspection of Compartment A and F Pylon Drain System Preservation of the Power Plant

AES

10-12-00 PB201




General (1)

This section gives the procedure for aircraft storage in standard weather conditions but: (a)

If aircraft storage is in high wind conditions: . do a check of the aircraft stability (Ref. TASK 05-57-00-200-001-A) . moor the aircraft (Ref. TASK 10-20-00-556-001-A) or (Ref. TASK 10-20-00-556-001-A-01) if necessary.

(b)

If aircraft storage is in cold weather conditions: . do the cold weather maintenance procedures: (Ref. TASK 12-31-21-660-001-A), (Ref. TASK 12-31-24-660-001-A), (Ref. TASK 12-31-25-660-001-A), (Ref. TASK 12-31-27-660-001-A), (Ref. TASK 12-31-28-660-001-A), (Ref. TASK 12-31-31-660-001-A), (Ref. TASK 12-31-32-660-001-A), (Ref. TASK 12-31-35-660-001-A), (Ref. TASK 12-31-38-660-001-A), (Ref. TASK 12-31-49-660-001-A), (Ref. TASK 12-31-51-660-001-A), (Ref. TASK 12-31-52-660-001-A), (Ref. TASK 12-31-71-660-001-A). NOTE :


Subtask 10-12-00-615-054-A B.



(2)

If necessary, clean the aircraft internally: (Ref. TASK 12-21-12-100-002-A) (Ref. TASK 12-21-12-100-003-A) (Ref. TASK 12-21-12-100-004-A) (Ref. TASK 12-21-12-100-005-A) (Ref. TASK 12-21-12-100-006-A) (Ref. TASK 12-21-12-100-007-A) (Ref. TASK 12-21-12-100-008-A) (Ref. TASK 12-21-12-100-009-A).

Subtask 10-12-00-941-051-A C.

AES



(2)


(3)


(4)


(5)


(6)

Put a WARNING NOTICE(S) in position to tell persons not to operate the systems during the aircraft storage procedure.

(7)


10-12-00 PB201



4.



(2)

Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001-A), (Ref. TASK 29-24-00-863-001-A), (Ref. TASK 29-10-00-863-003-A) or (Ref. TASK 29-10-00-863-003-A-01).

Procedure ** On A/C 004-099 Subtask 10-12-00-010-058-A A.

Get Access (1)

Open the aft and FWD passenger/crew doors (Ref. TASK 52-10-00-010-001-A).

(2)

Open the aft and FWD cargo compartment doors (Ref. TASK 52-30-00-860-001-A).

(3)

Open the landing gear doors (Ref. TASK 32-12-00-010-001-A) (Ref. TASK 32-22-00-010-001-A).

(4)


** On A/C 003-003 Subtask 10-12-00-010-058-B A.

Get Access (1)


(2)


(3)


(4)

Open the bulk cargo-compartment door (Ref. TASK 52-30-00-860-006-A).

(5)





(2)


(3)


Subtask 10-12-00-620-073-A C.

Protection of the Landing Gears and the Wheels (1)

AES

Protection of the landing gears (a)

Apply COMMON GREASES (Material No: 04-011) : . on the sliding tube of the shock absorber . on the actuator rods . on the uplock mechanism.

(b)

Apply COMMON GREASES (Material No: 04-004) : . to the towing and debogging fittings . to the uplock and downlock mechanisms after cleaning of these mechanisms.

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (c)

Apply TALCUM POWDER to all the rubber parts but not the tires.

(d)

Lubricate all the landing gears: . nose landing gear (Ref. TASK 12-22-32-640-002-A) . main landing gear (Ref. TASK 12-22-32-640-001-A).

(e)

Put protection on the bottom sections of the landing gears with STORAGE PRESERVATION (Material No: 15-002) .

(2)

Apply SPECIAL MATERIALS (Material No: 05-005) on all hydraulic unions in the NLG and MLG wheel-well bays.

(3)

Protection of the wheels (a)

We recommend that you install unserviceable tires or wheels with unserviceable tires: . on the nose landing gear (Ref. TASK 32-41-12-400-001-A) . on the main landing gear (Ref. TASK 32-41-11-400-006-A).

(b)

Lubricate the bearings with COMMON GREASES (Material No: 04-001) .

(c)

Make sure that there is no corrosion on the brakes and on each half wheel (Ref. TASK 32-40-00-200-001-A).

(d)

Remove the debris guard, the impeller and the shroud of the brake fans ** On A/C POST SB 32-1235 FOR A/C 003-008 (Ref. TASK 32-48-51-000-005-A) (If installed). . Apply SPECIAL MATERIALS (Material No: 05-027) on the removed parts.

(e)

Do a check of the tire pressures ** On A/C ALL (Ref. TASK 32-41-00-210-003-A).

(f)

Put protection on the brakes and the wheels with STORAGE PRESERVATION (Material No: 15-002) .

Subtask 10-12-00-550-052-A D.


Protection of the potable water system (a)

(2)

Drain, flush and dry the system if necessary (Ref. TASK 12-24-38-680-001-A).

Protection of the toilet system (a)

Drain, flush and clean the system with disinfectant if necessary (Ref. TASK 12-16-38-613-001-A).

** On A/C 003-004 Subtask 10-12-00-620-074-A E.

Protection of the Flight Controls (1)

AES

Lubricate: . the mechanical control chains of the THS (Ref. TASK 12-22-27-640-007-A) . the THS-actuator ball-screw nut (Ref. TASK 12-22-27-640-003-A) . the rudder bearings No. 6 (Ref. TASK 12-22-55-640-001-A) . the trimmable horizontal stabilizer bearings and attachment fittings (Ref. TASK 12-22-53-640-001A) . the roller bearings of the flap tracks (Ref. TASK 12-22-27-640-004-A) . the roller and the pinion bearings of the slat tracks (Ref. TASK 12-22-27-640-006-A)

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL . . (2)

all the spoiler servo-control bearings (Ref. TASK 12-22-27-640-005-A) the slat tracks surface with OILS (Material No: 03-001)

Flap rotary actuator lubrication (a)

Read the maintenance record to find when the last servicing of the flap rotary actuators occurred (Ref. TASK 12-22-27-640-008-A) (Ref. MPD 275449-05).

(b)

If lubrication of the flap rotary actuators occurred more than two years (24 months) ago:

(c)

1

Lubricate the flap rotary actuators (Ref. TASK 12-22-27-640-008-A).

2

Record this servicing operation.

If lubrication of the flap rotary actuators occurred less than two years (24 months) ago: 1

(3)

Visually examine the flap rotary actuators for signs of grease leakage.

Do an operational test of the flaps and slats sytems (Ref. TASK 27-54-00-710-002-A).

** On A/C 005-099 Subtask 10-12-00-620-074-C E.


Lubricate: . the mechanical control chains of the THS (Ref. TASK 12-22-27-640-007-A) . the THS-actuator ball-screw nut (Ref. TASK 12-22-27-640-003-A) . the rudder bearings No. 6 (Ref. TASK 12-22-55-640-001-A) . the trimmable horizontal stabilizer bearings and attachment fittings (Ref. TASK 12-22-53-640-001A) . the roller bearings of the flap tracks (Ref. TASK 12-22-27-640-004-A) . the roller and the pinion bearings of the slat tracks (Ref. TASK 12-22-27-640-006-A) . all the spoiler servo-control bearings (Ref. TASK 12-22-27-640-005-A) . the slat tracks surface with OILS (Material No: 03-001)

(2)

Do an operational test of the flap and slat systems (Ref. TASK 27-54-00-710-002-A).

** On A/C ALL Subtask 10-12-00-620-075-B F.

Protection of the Engines and IDG NOTE :

To save fuel and time, we recommend that you prepare the engines, IDG and APU first, then you run the engines and APU, then you complete the preservation of the engines, IDG and APU.

(1)


(2)

Do the IDG on-wing preservation (Ref. TASK 24-21-00-600-040-A).

Subtask 10-12-00-620-076-A G.

AES

Protection of the APU (1)

Do an inspection of the APU for preservation: . for a GTCP 36-300 APU: (Ref. AMM 49-20-00-200-001) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-20-00-210-001-A)

(2)

Do the preservation of the APU: . for a GTCP 36-300 APU: (Ref. AMM 49-20-00-600-001) . for an APS 3200 APU: (Ref. TASK 49-20-00-600-002-A)

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL .

(3)

for a 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-20-00-600-003-A)

If necessary, apply SPECIAL MATERIALS (Material No: 05-027) on cases, solenoids, brackets, screws and bolt heads in the APU compartment.

** On A/C ALL Subtask 10-12-00-281-053-A H.



(2)


(3)

(a)

If premixed fuel is available: . Refuel the wing tanks to 30% of the total capacity with fuel premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-01) or Biobor biocide (Ref. TASK 28-11-00-600-010-A). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-01) or Biobor biocide (Ref. TASK 28-11-00-600-010-A).

(b)

If premixed fuel is not available: . Refuel the wing tanks to 30% of the total capacity with fuel not premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-03) or Biobor biocide (Ref. TASK 28-11-00-600-010A-02). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel not premixed with Kathon biocide (Ref. TASK 28-11-00-600-010-A-03) or Biobor biocide (Ref. TASK 28-11-00-600-010A-02).

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from ACT, if installed (Ref. AMM 12-32-28-281-005) . NOTE :

(4)



Subtask 10-12-00-210-069-A J.

Visual Inspection of the Drains (1)

Make sure that all the external structural drain holes are not clogged: (a)

In the lower fuselage (Ref. TASK 53-59-00-210-001-A).

(b)

On the pylons (Ref. TASK 54-50-00-200-001-A).

(c)

On the engines.

(d)

In all other locations.

Subtask 10-12-00-620-077-A K.

External Protection of the Aircraft (1)

With STORAGE PRESERVATION (Material No: 15-002) and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): (a)

AES

Put a cover on the top of the rudder to give protection from bird excrement.

10-12-00 PB201



Seal: . the surge-tank overpressure . the L and R ailerons to give protection from bird nests . the air conditioning inlets and outlets . the avionics ventilation inlets and outlets . the battery venturi.

(2)

Seal the fuel NACA air intakes and the overpressure protector outlet (trim and wing tanks) with fine nylon netting and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent).

(3)

Apply SPECIAL MATERIALS (Material No: 05-005) on the trailing edge of the wings.

(4)

Apply SPECIAL MATERIALS (Material No: 05-027) : . on the leading edges of the nacelles and THS . on the refuel/defuel panel . on all the unpainted light-alloy areas.

Subtask 10-12-00-620-078-A L.

Protection of the Cabin and the Cockpit (1)

Put a plastic film protection on the carpets of the cabin aisle, the cockpit and the galley areas.

(2)

Put STORAGE PRESERVATION (Material No: 15-002) on all the passenger and cockpit seats.

(3)

Open the cockpit and window shades.

(4)


(5)

Give external protection to the cockpit windows with STORAGE PRESERVATION (Material No: 15-002) and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent). Do not put BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent) on the windows.

** On A/C 004-099 Subtask 10-12-00-620-079-A M.



(2)

Lubricate the safety pin guide-fitting and the door arming/disarming mechanism (Ref. TASK 12-22-52-640-014-A).

(3)


(4)


(5)


(6)

Lubricate the avionics-compartment door handles (Ref. TASK 12-22-52-640-008-A).

(7)

Apply SPECIAL MATERIALS (Material No: 05-043) on the seals of all the doors.

** On A/C 003-003 Subtask 10-12-00-620-079-B M.

AES



(2)

Lubricate the safety pin guide-fitting and the door arming/disarming mechanism (Ref. TASK 12-22-52-640-014-A).

(3)


(4)


10-12-00 PB201




(6)

Lubricate the bulk-cargo door handle (Ref. TASK 12-22-52-640-007-A).

(7)

Lubricate the avionics-compartment door handles (Ref. TASK 12-22-52-640-008-A).

(8)


** On A/C ALL Subtask 10-12-00-620-080-A N.

Protection of the Oxygen System (1)

Close the valve of the crew oxygen-cylinder assembly. (a)

In the cockpit, on the panel 21VU, push the OXYGEN/CREW SUPPLY pushbutton switch (the OFF legend goes off).

(b)

On one of the oxygen masks, operate the PRESS TO TEST AND RESET slide a sufficient number of times to make the system empty.

(c)

On the panel 21VU, release the OXYGEN/CREW SUPPLY pushbutton switch (the OFF legend comes on).

Subtask 10-12-00-620-081-A P.

Protection of the Rain Protection System (1)

Do the deactivation of the rain repellent system (Ref. TASK 30-45-00-040-002-A).

(2)

Put plastic bags or films on the two spray nozzles and attach them on the structure with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent).

Subtask 10-12-00-020-061-A Q.

Removal of Equipments (1)

Digital Flight Data Recorder 1TU If your DFDR is not a Solid State Flight Data Recorder (SSFDR), remove it (Ref. TASK 31-33-55-000-001-A). NOTE :

(2)

Cockpit Voice Recorder 1RK If your CVR is not a Solid State Cockpit Voice Recorder (SSCVR), remove it (Ref. TASK 23-71-35-000-001-A). NOTE :

AES

It is not necessary to remove an SSFDR.

It is not necessary to remove an SSCVR.

(3)

Remove: . all the EPSU batteries (Ref. TASK 33-51-38-000-002-A).

(4)

If the external temperature is more than 70 DEG.C (158.00 DEG.F), remove: . the FWD cargo fire-extinguishing bottles and cartridges (if installed) ** On A/C 005-099 (Ref. TASK 26-23-41-000-004-A). . the AFT cargo fire-extinguishing bottles and cartridges (if installed) (Ref. AMM 26-23-42-000-001) . . the engine fire-extinguishing bottles and cartridges ** On A/C ALL (Ref. TASK 26-21-41-000-001-A). . the APU fire-extinguishing-bottle and cartridge (Ref. TASK 26-22-41-000-001-A).

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-12-00-555-056-A R.


Put protection on all the probes, the engines and APU with adapted protection equipment (Ref. TASK 10-11-00-555-013-A).

(2)

Keep all external protection equipment flags in position with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent).

Subtask 10-12-00-860-060-A S.

5.



(2)


(3)

On the Fixed Automatic Emergency Locator Transmitter (ELT) (if installed): . Set the ON/OFF/AUTO switch to the OFF position.

(4)

On the Portable Survival Emergency Locator Transmitter (ELT) (if installed): . Set the ON/OFF/AUTO switch to the OFF position.


Close-up (1)


(2)


(3)


(4)

Close all the landing gear doors (Ref. TASK 32-22-00-410-001-A), (Ref. TASK 32-12-00-410-001-A).

(5)

Close all the access door panels that you opened during the storage procedure.

(6)

Seal with STORAGE PRESERVATION (Material No: 15-002) and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent) all the openings that give access to: . the passenger compartment, . the cockpit, . the cargo compartment, . the APU, . the engines, . the landing gears.

(7)

Seal with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): . the passenger/crew door handles, . the emergency exit door handles, . the FWD and aft cargo door handles, . the avionics-compartment door handles.

(8)

Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001-A), (Ref. TASK 29-24-00-864-001-A), (Ref. TASK 29-10-00-864-003-A).

(9)


(10) Remove all the fixtures, tools, test and support equipment used during this procedure.

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (11) Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that the protection covers/devices are installed. ** On A/C 003-003 Subtask 10-12-00-942-056-B A.

Close-up (1)


(2)


(3)


(4)


(5)


(6)


(7)


(8)

Seal with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): . the passenger/crew door handles, . the emergency exit door handles, . the FWD and aft cargo door handles, . the bulk cargo door handle, . the avionics-compartment door handles.

(9)


(10) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002-A) or (Ref. TASK 24-41-00-862-002-A-01) or (Ref. TASK 24-41-00-862-002-A-02). (11) Remove all the fixtures, tools, test and support equipment used during this procedure. (12) Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that the protection covers/devices are installed.

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-553-007-A Storage Procedure (Storage Not More than 2 Years) CAUTION :


CAUTION :


1.

Reason for the Job This procedure gives the preservation steps for a storage period of not more than 2 years.

2.





No specific

AR

TALCUM POWDER

No specific

1

WARNING NOTICE(S)

B.



Material No: 04-001 Material No: 04-004 Material No: 04-011 Material No: 05-005 Material No: 05-027 Material No: 05-043 Material No: 08-052 Material No: 15-002

AES

DESIGNATION

DESIGNATION

OILS MINERAL OIL (LOW TEMP) COMMON GREASES WHEEL BEARING MINERAL GREASE COMMON GREASES SYNTH. ESTER BASED GREASE HIGH PRESSURE COMMON GREASES SILICONE GREASE PNEUMATIC SYST AND SEALS SPECIAL MATERIALS CORROSION PREVENTIVE SPECIAL MATERIALS SPECIAL MATERIALS VARNISH P.T.F.E SPRAY BONDING AND ADHESIVE COMPOUNDS SELF ADHESIVE ALUMINIUM TAPE STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL C.


REFERENCE 05-57-00-200-001-A

10-11-00-555-013-A 10-11-00-555-015-A 10-20-00-556-001-A 10-20-00-556-001-A-01

DESIGNATION

Aircraft Stability Installation of the Aircraft Protection Equipment Procedure for the Installation of Wheel Chocks on Aircraft Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs

** On A/C 005-099 12-13-27-612-005-A

Drain and Refill Flap Actuator Assemblies with Semi-fluid

12-16-38-613-001-A 12-21-11-615-002-A

Servicing of the Toilet System External Cleaning

12-21-12-100-002-A


12-21-12-100-003-A


12-21-12-100-004-A


12-21-12-100-005-A


12-21-12-100-006-A


12-21-12-100-007-A


12-21-12-100-008-A


12-21-12-100-009-A


12-22-27-640-003-A 12-22-27-640-004-A

Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut Lubricate all Carriage Rollers on all Flap Tracks

12-22-27-640-005-A

Lubrication of Spoiler No.1 to 5 Servo Control Bearings

12-22-27-640-006-A

Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth

12-22-27-640-007-A ** On A/C 003-004

Lubrication of the THS Mechanical Control Chains

12-22-27-640-008-A 12-22-32-640-001-A 12-22-32-640-002-A

Remove Flap Rotary Actuators For Regreasing Lubrication of Main Landing Gear and Doors Lubrication of Nose Landing Gear and Doors

12-22-52-640-002-A 12-22-52-640-006-A


** On A/C 003-003 12-22-52-640-007-A


12-22-52-640-008-A 12-22-52-640-009-A


12-22-52-640-014-A


12-22-52-640-016-A 12-22-53-640-001-A

Lubrication of the Hinge-Arm Support-Fitting Bearings Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004 Lubrication of Rudder Hinge Bearing No. 6 with Grease Mat. No. 04-004

12-22-55-640-001-A

AES

10-12-00 PB201



DESIGNATION Lubrication of the Cockpit Sliding Window Tracks

12-24-38-680-001-A


12-31-21-660-001-A 12-31-24-660-001-A 12-31-25-660-001-A

Cold Weather Maintenance - Air Conditioning Cold Weather Maintenance - Electrical Power Cold Weather Maintenance - Equipment/Furnishings

12-31-27-660-001-A


12-31-28-660-001-A 12-31-31-660-001-A


12-31-32-660-001-A

Cold Weather Maintenance - Landing Gear

12-31-35-660-001-A

Cold Weather Maintenance - Oxygen System

12-31-38-660-001-A


12-31-49-660-001-A

Cold Weather Maintenance - Auxiliary Power Unit

12-31-51-660-001-A 12-31-52-660-001-A 12-31-71-660-001-A 12-32-28-281-001-A 12-32-28-281-003-A

Cold Weather Maintenance - Structure Cold Weather Maintenance - Doors Cold Weather Maintenance - Power Plant Drain Water Content Sample Fuel for Microbiological Contamination Analysis

12-34-24-869-002-A

Aircraft Grounding for the Maintenance Operations

20-24-11-100-001-A

Cleaning and Protection of the Cables

23-71-35-000-001-A

Removal of the Cockpit Voice Recorder (CVR) 1RK

24-21-00-600-040-A

Preservation/Storage/Return to Service of the IDG

24-38-51-000-001-A 24-41-00-861-002-A


24-41-00-861-002-A-01


24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


25-65-35-000-001-A

Removal of the Emergency Locator Transmitter (ELT)

26-21-41-000-004-A

Removal of the Cartridge of the Engine Fire-Extinguisher Bottle

26-22-41-000-001-A

Removal of the Fire Extinguisher Bottle

** On A/C 005-099 26-23-41-000-004-A 27-54-00-710-002-A 28-11-00-600-010-A 28-11-00-600-010-A-01 28-11-00-600-010-A-02 28-11-00-600-010-A-03

AES

Removal of the Cargo Fire-Extinguisher Bottle Operational Test of the Flap and Slat Systems Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig

10-12-00 PB201



DESIGNATION Check of the External Leaks of the Hydraulic Components

29-10-00-863-003-A

Pressurize the Blue Hydraulic System with a Ground Power Supply

29-10-00-863-003-A-01

Pressurize the Blue Hydraulic System with the Blue Electric Pump

29-10-00-864-003-A 29-23-00-863-001-A

Depressurize the Blue Hydraulic System Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump

29-23-00-864-001-A 29-24-00-863-001-A

Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU Pressurize the Yellow Hydraulic System with the Electric Pump

29-24-00-864-001-A


30-45-00-040-002-A 30-45-52-000-002-A

Deactivation of the Rain Repellent System Removal of the Wiper Arm

30-45-53-000-001-A

Removal of the Wiper Blade

31-33-55-000-001-A

Removal of the Digital Flight Data Recorder (DFDR)

32-00-00-481-001-A


32-12-00-010-001-A

Open the Main Gear Doors for Access

32-12-00-410-001-A 32-22-00-010-001-A 32-22-00-410-001-A

Close the Main Gear Doors after Access Nose Gear Doors - Ground Doors Opening Nose Gear Doors - Ground Doors Closing

32-40-00-200-001-A

Inspection/Check of the Wheels & Brakes

32-41-00-210-003-A


32-41-11-400-006-A Installation of the MLG Wheel 32-41-12-400-001-A Installation of the NLG Wheel ** On A/C POST SB 32-1235 FOR A/C 003-008 32-48-51-000-005-A

Removal of the Fan Assy

33-51-38-000-002-A 34-10-00-170-001-A

Removal of the Battery of the Emergency Power-Supply Unit Flushing of the Principal Total Pressure Lines

34-10-00-170-002-A

Flushing of the Principal Static Pressure Lines

34-10-00-170-003-A


** On A/C 006-099 49-20-00-210-001-A

APU Power Plant Visual Inspection (APS 3200)

49-20-00-600-002-A


** On A/C 003-005 49-20-00-600-003-A


52-10-00-010-001-A


52-10-00-410-001-A


52-30-00-860-001-A


52-30-00-860-002-A

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE ** On A/C 003-003

DESIGNATION

52-30-00-860-006-A


52-30-00-860-008-A 53-59-00-210-001-A

Close the Bulk Cargo-Compartment Door Operational Check of Single Drain Pipe Aft of FR70 from Outside

54-50-00-200-001-A

General Visual Inspection of Compartment A and F Pylon Drain System

71-00-00-550-010-A


3.


General (1)

This section gives the procedure for aircraft storage in standard weather conditions but: (a)

If aircraft storage is in high wind conditions: . do a check of the aircraft stability (Ref. TASK 05-57-00-200-001-A) . moor the aircraft (Ref. TASK 10-20-00-556-001-A) or (Ref. TASK 10-20-00-556-001-A-01) if necessary.

(b)

If aircraft storage is in cold weather conditions: . do the cold weather maintenance procedures: (Ref. TASK 12-31-21-660-001-A), (Ref. TASK 12-31-24-660-001-A), (Ref. TASK 12-31-25-660-001-A), (Ref. TASK 12-31-27-660-001-A), (Ref. TASK 12-31-28-660-001-A), (Ref. TASK 12-31-31-660-001-A), (Ref. TASK 12-31-32-660-001-A), (Ref. TASK 12-31-35-660-001-A), (Ref. TASK 12-31-38-660-001-A), (Ref. TASK 12-31-49-660-001-A), (Ref. TASK 12-31-51-660-001-A), (Ref. TASK 12-31-52-660-001-A), (Ref. TASK 12-31-71-660-001-A). NOTE :


Subtask 10-12-00-615-055-A B.



(2)

If necessary, clean the aircraft internally: (Ref. TASK 12-21-12-100-002-A) (Ref. TASK 12-21-12-100-003-A) (Ref. TASK 12-21-12-100-004-A) (Ref. TASK 12-21-12-100-005-A) (Ref. TASK 12-21-12-100-006-A) (Ref. TASK 12-21-12-100-007-A) (Ref. TASK 12-21-12-100-008-A) (Ref. TASK 12-21-12-100-009-A).

Subtask 10-12-00-941-052-A C.

AES



(2)


10-12-00 PB201




(4)


(5)


(6)

Put a WARNING NOTICE(S) in position to tell persons not to operate the systems during the aircraft storage procedure.

(7)


Subtask 10-12-00-650-054-A D.

4.



(2)


Procedure ** On A/C 004-099 Subtask 10-12-00-010-059-A A.

Get Access (1)


(2)


(3)


(4)


** On A/C 003-003 Subtask 10-12-00-010-059-B A.

Get Access (1)


(2)


(3)


(4)


(5)



AES



(2)


(3)


10-12-00 PB201



Protection of the Landing Gears and the Wheels (1)

Protection of the landing gears (a)

Apply SPECIAL MATERIALS (Material No: 05-027) on the cases, brackets, screws and bolts.

(b)

Apply COMMON GREASES (Material No: 04-011) : . on the sliding tube of the shock absorber . on the actuator rods . on the uplock mechanism.

(c)

Apply COMMON GREASES (Material No: 04-004) : . to the towing and debogging fittings . to the uplock and downlock mechanisms after cleaning of these mechanisms.

(d)

Apply TALCUM POWDER to all the rubber parts but not the tires.

(e)

Lubricate all the landing gears: . nose landing gear (Ref. TASK 12-22-32-640-002-A) . main landing gear (Ref. TASK 12-22-32-640-001-A).

(f)

Put protection on the bottom sections of the landing gears with STORAGE PRESERVATION (Material No: 15-002) .

(2)

Apply SPECIAL MATERIALS (Material No: 05-005) on all hydraulic unions in the NLG and MLG wheel-well bays.

(3)

Protection of the wheels (a)

We recommend that you install unserviceable tires or wheels with unserviceable tires: . on the nose landing gear (Ref. TASK 32-41-12-400-001-A) . on the main landing gear (Ref. TASK 32-41-11-400-006-A).

(b)

Lubricate the bearings with COMMON GREASES (Material No: 04-001) .

(c)

Make sure that there is no corrosion on the brakes and on each half wheel (Ref. TASK 32-40-00-200-001-A).

(d)

Remove the debris guard, the impeller and the shroud of the brake fans ** On A/C POST SB 32-1235 FOR A/C 003-008 (Ref. TASK 32-48-51-000-005-A) (If installed). . Apply SPECIAL MATERIALS (Material No: 05-027) on the removed parts.

(e)

Do a check of the tire pressures ** On A/C ALL (Ref. TASK 32-41-00-210-003-A).

(f)

Put protection on the brakes and the wheels with STORAGE PRESERVATION (Material No: 15-002) .

Subtask 10-12-00-550-053-A D.


Protection of the potable water system (a)

AES

If the storage period is more than 2 days: . drain, flush and dry the system if necessary (Ref. TASK 12-24-38-680-001-A).

10-12-00 PB201



Protection of the toilet system (a)

If the storage period is more than 2 days: . drain, flush and clean the system with disinfectant if necessary (Ref. TASK 12-16-38-613-001A).

** On A/C 003-004 Subtask 10-12-00-620-083-A E.



(2)

Flap rotary actuator lubrication (a)

Read the maintenance record to find when the last servicing of the flap rotary actuators occurred (Ref. TASK 12-22-27-640-008-A) (Ref. MPD 275449-05).

(b)

If lubrication of the flap rotary actuators occurred more than one year (12 months) ago:

(c)

1

Lubricate the flap rotary actuators (Ref. TASK 12-22-27-640-008-A).

2

Record this servicing operation.

If lubrication of the flap rotary actuators occurred less than one year (12 months) ago: 1

Visually examine the flap rotary actuators for signs of grease leakage.

(3)

Do an operational test of the flaps and slat systems (Ref. TASK 27-54-00-710-002-A).

(4)

Clean and give protection to the flight control cables (Ref. TASK 20-24-11-100-001-A).

** On A/C 005-099 Subtask 10-12-00-620-083-C E.

AES



(2)

Drain and refill the flap actuator assemblies with semi-fluid (Ref. TASK 12-13-27-612-005-A).

(3)

Do an operational test of the flaps and slat systems (Ref. TASK 27-54-00-710-002-A).

(4)

Clean and give protection to the flight control cables (Ref. TASK 20-24-11-100-001-A).

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Subtask 10-12-00-620-085-B F.

Protection of the Engines NOTE :

To save fuel and time, we recommend that you prepare the engines, IDG and APU first, then you run the engines and APU, then you complete the preservation of the engines, IDG and APU.

(1)


(2)

Do the IDG on wing preservation (Ref. TASK 24-21-00-600-040-A).

Subtask 10-12-00-620-086-A G.

Protection of the APU (1)

Do an inspection of the APU for preservation: . for a GTCP 36-300 APU: (Ref. AMM 49-20-00-200-001) . for an APS 3200 APU: ** On A/C 006-099 (Ref. TASK 49-20-00-210-001-A)

(2)

Do the preservation of the APU: . for a GTCP 36-300 APU: (Ref. AMM 49-20-00-600-001) . for an APS 3200 APU: (Ref. TASK 49-20-00-600-002-A) . for a 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-20-00-600-003-A)

(3)

If necessary, apply SPECIAL MATERIALS (Material No: 05-027) on cases, solenoids, brackets, screws and bolt heads in the APU compartment.

** On A/C ALL Subtask 10-12-00-620-084-A H.



(2)


(3)

AES

(a)

If premixed fuel is available: . Refuel the wing tanks to 30% of the total capacity with fuel premixed with Biobor biocide (Ref. TASK 28-11-00-600-010-A) or Kathon biocide (Ref. TASK 28-11-00-600-010-A-01). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel premixed with Biobor biocide (Ref. TASK 28-11-00-600-010-A) or Kathon biocide (Ref. TASK 28-11-00-600-010-A-01).

(b)

If premixed fuel is not available: . Refuel the wing tanks to 30% of the total capacity with fuel not premixed with Biobor biocide (Ref. TASK 28-11-00-600-010-A-02) or Kathon biocide (Ref. TASK 28-11-00-600-010-A-03). . If ACT is installed, do the preventive treatment on ACT (Ref. AMM 28-28-00-610-001) . . Refuel the center tank to 30% of the total capacity with fuel not premixed with Biobor biocide (Ref. TASK 28-11-00-600-010-A-02) or Kathon biocide (Ref. TASK 28-11-00-600-010-A-03).

Drain water: . from all the fuel tanks (Ref. TASK 12-32-28-281-001-A) . from ACT, if installed (Ref. AMM 12-32-28-281-005) .

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL NOTE :

(4)



Subtask 10-12-00-210-070-A J.

Visual Inspection of the Drains (1)

Make sure that all the external structural drain holes are not clogged: (a)


(b)

On the pylons (Ref. TASK 54-50-00-200-001-A).

(c)

On the engines.

(d)


Subtask 10-12-00-620-087-A K.

External Protection of the Aircraft (1)

With STORAGE PRESERVATION (Material No: 15-002) and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): (a)

Put a cover on the top of the rudder to give protection from bird excrement.

(b)

Seal: . the surge-tank overpressure, . the L and R ailerons to give protection from bird nest, . the air conditioning inlets and outlets, . the avionics ventilation inlets and outlets, . the battery venturi.

(2)

Seal with fine nylon netting and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): . the fuel NACA air-intakes . the overpressure protector outlet (wing tanks) . all the drain valves

(3)

Apply SPECIAL MATERIALS (Material No: 05-005) on the trailing edge of the wings.

(4)

Apply SPECIAL MATERIALS (Material No: 05-027) : . on the leading edges of the nacelles and THS . on the refuel/defuel panel . on all the unpainted light-alloy areas.

Subtask 10-12-00-620-088-A L.

Protection of the Cabin and Cockpit (1)

Put a plastic film protection on: . all the passenger and cockpit seats . the carpets of the cabin aisles, cockpit and galley areas.

(2)

Open the cockpit and window shades.

(3)


** On A/C 004-099 Subtask 10-12-00-620-096-A M.


AES


10-12-00 PB201




(3)


(4)


(5)


(6)


(7)


** On A/C 003-003 Subtask 10-12-00-620-096-B M.



(2)


(3)


(4)


(5)


(6)

Lubricate the bulk-cargo door handle (Ref. TASK 12-22-52-640-007-A).

(7)


(8)


** On A/C ALL Subtask 10-12-00-620-089-A N.

Protection of the Oxygen System (1)

Close the valve of the crew oxygen-cylinder assembly. (a)

In the cockpit, on the panel 21VU, push the OXYGEN/CREW SUPPLY pushbutton switch (the OFF legend goes off).

(b)

On one of the oxygen masks, operate the PRESS TO TEST AND RESET slide a sufficient number of times to make the system empty.

(c)

On the panel 21VU, release the OXYGEN/CREW SUPPLY pushbutton switch (the OFF legend comes on).

Subtask 10-12-00-620-090-A P.

Protection of the Rain Protection System (1)

Do the deactivation of the rain repellent system (Ref. TASK 30-45-00-040-002-A).

(2)

Put plastic bags or films on the two spray nozzles and attach them on the structure with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent).

(3)

Remove the wiper blades (Ref. TASK 30-45-53-000-001-A) and the wiper arms (Ref. TASK 30-45-52-000-002-A).

Subtask 10-12-00-620-091-A Q.


AES

Lubricate the sliding windows (Ref. TASK 12-22-56-600-001-A).

10-12-00 PB201




(3)

Give external protection to the cockpit and cabin windows with STORAGE PRESERVATION (Material No: 15-002) and BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent). Do not put BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent) on the windows.

(4)


Subtask 10-12-00-020-062-A R.

Removal of Equipments (1)

Digital Flight Data Recorder 1TU If your DFDR is not a Solid State Flight Data Recorder (SSFDR), remove it (Ref. TASK 31-33-55-000-001-A). NOTE :

(2)

It is not necessary to remove a SSFDR.

Cockpit Voice Recorder 1RK If your CVR is not a Solid State Cockpit Voice Recorder (SSCVR), remove it (Ref. TASK 23-71-35-000-001-A). NOTE :

It is not necessary to remove a SSCVR.

(3)

Remove the batteries of: . all the EPSU (Ref. TASK 33-51-38-000-002-A), . the megaphones, . the flashlights.

(4)

Remove the Emergency Locator Transmitter (ELT):

(5)

(a)

For the Fixed Automatic Emergency Locator Transmitter (ELT) (if installed): (Ref. TASK 25-65-35-000-001-A).

(b)

For the Portable Survival Emergency Locator Transmitter (ELT) (if installed): 1

If the Portable ELT has a programming dongle, remove the portable ELT: (Ref. AMM 25-65-32-000-001) .

2

If the Portable ELT does not have a programming dongle, remove the ELT. . Set the ON/OFF/AUTO switch to the OFF position.

If the external temperature is more than 70 DEG.C (158.00 DEG.F), remove: . the FWD cargo fire-extinguishing bottles and cartridges (if installed) ** On A/C 005-099 (Ref. TASK 26-23-41-000-004-A). . the AFT cargo fire-extinguishing bottles and cartridges (if installed) (Ref. AMM 26-23-42-000-001) . . the engine fire-extinguishing bottles and cartridges ** On A/C ALL (Ref. TASK 26-21-41-000-004-A). . the APU fire-extinguishing bottle and cartridge (Ref. TASK 26-22-41-000-001-A).

Subtask 10-12-00-620-092-A S.

Protection of the Hydraulic System (1)

AES

Do a check of the hydraulic components for external leakage (Ref. TASK 29-00-00-790-001-A).

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-12-00-555-057-A T.


Put protecton on all the probes, the engines and APU with adapted protection equipment (Ref. TASK 10-11-00-555-013-A).

(2)

Keep all external protection equipment flags in position with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent).

Subtask 10-12-00-860-062-A U.

5.



(2)



Close-up (1)


(2)


(3)


(4)


(5)


(6)


(7)

Seal with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): . the passenger/crew door handles, . the emergency exit door handles, . the FWD and aft cargo door handles, . the avionics-compartment door handles.

(8)


(9)


(10) Remove all the fixtures, tools, test and support equipment used during this procedure. (11) Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that the protection covers/devices are installed.

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C 003-003 Subtask 10-12-00-942-057-B A.

Close-up (1)


(2)


(3)


(4)


(5)


(6)


(7)


(8)

Seal with BONDING AND ADHESIVE COMPOUNDS (Material No: 08-052) (or equivalent): . the passenger/crew door handles, . the emergency exit door handles, . the FWD and aft cargo door handles, . the bulk cargo door handle, . the avionics-compartment door handles.

(9)


(10) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002-A) or (Ref. TASK 24-41-00-862-002-A-01) or (Ref. TASK 24-41-00-862-002-A-02). (11) Remove all the fixtures, tools, test and support equipment used during this procedure. (12) Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that the protection covers/devices are installed.

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-553-008-A Renewal for 6 Months Storage Period CAUTION CAUT ION :

1.

DURING STORAGE DURING STORAGE OR PARKING PARKING PERIODS PERIODS,, DO NOT STOP STOP OR CHANGE CHANGE THE MAINTENANC MAINTENANCE E PROGRAM WITHOUT LOCAL AUTHORITY APPROVAL. THE MAINTENANCE CALENDAR CLOCK CONTINUES DURING THESE PERIODS. IF YOU DO THE AMM STORAGE OR PARKING PROCEDURES CORRECTLY, AND IF YOU HAVE THE APPROVAL 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.

Reas Re ason on fo forr th thee Jo Job b This procedure lets the operator do the storage procedure for 6 months again one time.

2.

Job Jo b Se Sett-up up In Info form rmat atio ion n A.

Fixtur Fix tures, es, Too Tools, ls, Tes Testt and and Supp Support ort Equ Equipm ipment ent


B.

Cons Co nsum umab able le Ma Mate teri rial alss


Material No: 05-005 C.


DESIGNATION

COMMON GREASES SYNTH. ESTER BASED GREASE HIGH PRESSURE SPECIAL MATERIALS CORROSION PREVENTIVE

Refere Ref erence nced d Inf Inform ormati ation on

REFERENCE 10-12-00-200-006-A


10-12-00-200-007-A 10-12-00-200-008-A 10-12-00-200-009-A

Periodic Ground Check at 15-day Intervals Periodic Ground-Check at 1-month Interv rval al Periodic ground-check at 3-month interval

12-2212-2 2-27 27-6 -640 40-0 -003 03-A -A 12-22-27-640-004-A

Lubric Lubr icat atio ion n of Tr Trim imma mabl blee Ho Hori rizo zont ntal al St Stab abil iliz izer er Ac Actu tuat ator or Ba Ball ll Sc Scre rew w Nu Nutt Lubr briicate al alll Carriage Rollers on all Flap Tracks

12-2 12 -222-27 27-6 -640 40-0 -005 05--A

Lubr Lu bric icat atiion of Sp Spoi oiller No No.1 .1 to 5 Se Serv rvo o Co Cont ntrrol Be Bear arin ings gs

12-2 12 -222-27 27-6 -640 40-0 -006 06-A -A

Lubr Lu bric icat atio ion n of al alll Sl Slat at Tr Trac ackk Ro Roll ller ers, s, Pi Pini nion on Be Bear arin ings gs,, Pi Pini nion onss an and d Ra Rack ck Te Teet eth h

12-22-27-640-007-A 12-22-32-640-001-A 12-22-32-640-002-A

Lubrication of the THS Mechanical Control Chai ain ns Lubrication of Main Lan and ding Gear and Doors Lubri riccation of Nose Landing Gear and Doors

12-2 12 -222-53 53-6 -640 40-0 -001 01-A -A

Lubric Lubr icat atio ion n of Tr Trim imma mabl blee Ho Hori rizo zont ntal al St Stab abil iliz izer er Be Bear arin ings gs an and d At Atta tach chme ment nt Fittings with Grease Mat. No. 04-004

12-2 12 -222-55 55-6 -640 40-0 -001 01--A

Lubr Lu briica cati tion on of Ru Rudd dder er Hi Hing ngee Be Bear arin ing g No No.. 6 wi with th Gr Grea ease se Mat at.. No No.. 04 04-0 -004 04

12-32-28-281-001-A 12-3 12 -322-28 28-2 -281 81-0 -003 03--A 20-24-11-100-001-A

Drain Water Content Samp Sa mplle Fue uell for Mi Miccro robi biol olog ogic ical al Co Cont ntam amin inat atio ion n Ana nallys ysis is Cleaning and Protection of the Cables

AES

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 25-6 25 -655-35 35-0 -000 00-0 -001 01--A

DESIGNATION Rem Re mov oval al of the Em Emer erge genc ncyy Lo Loccat ator or Tr Tran ansm smit itte terr (EL ELT) T)

32-3 32 -311-00 00-7 -720 20-0 -002 02-A -A

Func Fu ncti tion onal al Te Test st of th thee No Norm rmal al Ex Exte tens nsio ion n an and d Re Retr trac acti tion on of th thee La Land ndin ing g Ge Gear ar

3.

Job Se Sett-up up Subtask 10-12-00-941-056-A A.

Get Access (1)

4.

Put an ACCESS ACCESS PLATFORM PLATFORM 15M 15M (49 FT) - ADJUSTA ADJUSTABLE BLE in position position near the aircr aircraft. aft.

Pro roce cedu dure re Subtask 10-12-00-553-070-A A.

Grou Gr ound nd Che heck ck (1)

Do . . . .

tthe he peri periodi odicc groun ground d chec checks ks at: at: 7-day inter intervals vals (Ref (Ref.. TASK 10-12 10-12-00-20 -00-200-006 0-006-A) -A) 15-day inter intervals vals (Ref (Ref.. TASK 10-12 10-12-00-20 -00-200-007 0-007-A) -A) 1-month 1-mon th inter intervals vals (Ref (Ref.. TASK 10-12 10-12-00-20 -00-200-008 0-008-A) -A) 3-month 3-mon th inter intervals vals (Ref (Ref.. TASK TASK 10-12 10-12-00-20 -00-200-009 0-009-A). -A).

Subtask 10-12-00-620-095-A B.

Prot Pr otec ecttio ion n (1)

Lubrication of the Lubrication the mechanical mechanical control control chains of the the THS (Ref. TASK TASK 12-22-27-64012-22-27-640-007 007-A) -A) and the actuator ballscrew nut (Ref. TASK 12-22-27-640-003-A).

(2)

Cleaning Cleani ng and and protectio protection n of the flight flight contr control ol cables cables (a)

Make sure that that the rudder rudder and THS cables cables are lubric lubricated ated and have have no corrosion corrosion in these these areas: areas: . the avi avioni onics cs com compar partme tment, nt, . the FWD and AFT car cargo go com compar partme tments nts,, . betwe between en FR71 FR71 and the the THS actuat actuator or and the the rear rudder mechan mechanicalical-contro control. l. NOTE NO TE :

(b)

Be caref careful ul of cabl cablee areas areas hidd hidden en by pull pulley ey guard guard or or pulley pulley guide guide..

If there there is corrosion corrosion on the cables cables or ifif there is no no protection protection with with SPECIAL SPECIAL MATERIALS MATERIALS (Material No: 05-005) or COMMON GREASES (Material No: 04-004) , clean and put protection along the full length of the cables (Ref (Ref.. TASK 20-24-11-100-00 20-24-11-100-0011-A). A).

(3)

Lubrication Lubric ation of the the rollers rollers of the flap flap tracks (Ref. (Ref. TASK TASK 12-22-27-640 12-22-27-640-004 -004-A). -A).

(4)

Lubrication Lubric ation of all the the rollers rollers and pinions of the the slat tracks tracks (Ref. TASK 12-22-2712-22-27-640-0 640-006 06-A). -A).

(5)

Lubrication Lubric ation of spoiler spoiler servo-cont servo-control rol bearings bearings (Ref. (Ref. TASK 12-22-27-640 12-22-27-640-005 -005-A). -A).

(6)

Lubrication of the Lubrication the hinges hinges and the attach attach fittings fittings of of the horizontal horizontal stabili stabilizer zer (Ref. (Ref. TASK 12-22-53-640-001-A).

(7)

Lubrication Lubric ation of of the rudder rudder bearing bearing No. 6 (Ref. (Ref. TASK TASK 12-22-55-640 12-22-55-640-001 -001-A). -A).

(8)

Lubricate Lubric ate all the land landing ing gea gears: rs: . nose landin landing g gear (Ref (Ref.. TASK TASK 12-2212-22-32-64 32-640-002 0-002-A) -A) . mai main n landing landing gear gear (Ref (Ref.. TASK 12-2 12-22-3 2-32-6 2-64040-001 001-A) -A)

Subtask 10-12-00-710-072-A C.

Test Te st of th thee La Land ndin ingg Ge Gear ar (1)

AES

Do a test of extensi extension on and retractio retraction n of the landing landing gear (Ref. (Ref. TASK TASK 32-31-00-720 32-31-00-720-002 -002-A) -A)

10-12-00 PB201



Prot Pr otec ecti tion on of th thee fu fuel el (1)

Do a fuel sampling sampling for microbiol microbiological ogical contami contamination nation (Ref. (Ref. TASK 12-32-2812-32-28-281-00 281-003 3-A).

(2)) (2

Drain Drai n wa wate ter: r: . from all the fuel tanks (Ref (Ref.. TASK TASK 12-32-2812-32-28-281-00 281-001 1-A) . fro from m ACT, ifif instal installed led (Ref (Ref.. AMM 12-32 12-32-28 -28-28 -281-0 1-005) 05) . NOTE :

(3)

Do the the water water drai drainn procedu procedure re one one hour hour after after refu refuelin elingg is comple completed. ted.

Close Clo se all the fue fuell syste system m valve valves. s.

Subtask 10-12-00-020-063-A E.

5.

Remo Re mova vall of Co Comp mpon onen ents ts (1)

Remove all the bat Remove batter teries ies of: . th thee me mega gaph phon ones es . th thee fl flash ashli ligh ghts ts..

(2)

Removee the Remov the Emerge Emergency ncy Locato Locatorr Transmit Transmitter ter (ELT) (ELT):: (a)

For the Fixed Fixed Automatic Automatic Emergency Emergency Locator Locator Transmitt Transmitter er (ELT) (if (if installed): installed): (Ref. (Ref. TASK 25-65-35-000-001-A).

(b)

For the Portabl Portablee Survival Survival Emergency Emergency Locator Locator Transmitt Transmitter er (ELT) (ELT) (if installed installed): ): 1

If the the Portab Portable le ELT ELT has a prog program rammin ming g dongle dongle,, remove remove the the porta portable ble ELT ELT:: (Ref. (Ref. AMM AMM 25-65-32-000-001) .

2

If tthe he Port Portabl ablee ELT ELT does does not not have have a pro progra grammi mming ng dongl dongle, e, remo remove ve the the ELT. ELT. . set the ON/ ON/OFF OFF/AU /AUTO TO switc switch h to the the OFF OFF posit position ion..

Clo lose se-u -up p Subtask 10-12-00-942-061-A A.

Put the air aircra craft ft back back to its its init initial ial con config figura uratio tion. n. (1)

AES

Removee all the fixtur Remov fixtures, es, tools, tools, test and support support equipm equipment ent used during during this this procedure. procedure.

10-12-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-553-009-A Renewal for 2 Years Storage Period CAUTION :

1.



2.



REFERENCE 10-12-00-553-007-A

DESIGNATION Storage Procedure (Storage Not More than 2 Years)

10-30-00-554-005-A

Return to Operation after Storage Period

3.


4.

Not Applicable


Preparation of the Aircraft (1)

Do the full return to operation after storage (Ref. TASK 10-30-00-554-005-A).

(2)

Refer to the aircraft maintenance program and make sure that you do all the scheduled maintenance tasks that are due.

Subtask 10-12-00-554-050-A B.

Non-revenue Flight (1)

Do a short non-revenue flight within the aircraft standard envelope.

Subtask 10-12-00-553-071-A C.

Store the Aircraft (1)

AES

Do the storage procedure (Ref. TASK 10-12-00-553-007-A).

10-12-00 PB201



STORAGE - INSPECTION/CHECK ** On A/C ALL Task 10-12-00-200-006-A Periodic Ground Check at 7-day Intervals 1.

Reason for the Job To do a check of the condition of the aircraft during the storage period.

2.




B.


REFERENCE 71-00-00-550-010-A

3.


DESIGNATION



4.



Visual Inspection (1)

Do a general visual inspection of the airframe from the ground for correct condition.

(2)

Make sure that there is no bird nest. If you find bird nests, remove them and clean the aircraft surface around the bird nest.

(3)

Make sure that there are no leaks: . at the engine drain masts . on the wheels and landing gears . from the wings . from the APU . from the horizontal and vertical stabilizer.

(4)

Make sure that the protection cover/plugs are correctly installed.

(5)

Do a check of the outer skin for contamination that is not usual.

Subtask 10-12-00-210-083-A B.

Inspection of the Engine Humidity Indicator (1)

AES

For engines PRE-SB72-0369 Examine the indicators. If one or more of the indicators show too much humidity, replace the indicator and desiccant and do the engine preservation procedure again (Ref. TASK 71-00-00-550-010-A).

10-12-00 PB601



5.

For engines POST-SB72-0369 Only examine the indicators after the first 7 days. If one or more of the indicators show too much humidity, replace the indicator and desiccant and do the engine preservation procedure again (Ref. TASK 71-00-00-550-010-A).


AES

Remove the access platform(s).

10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-200-007-A Periodic Ground Check at 15-day Intervals 1.


2.




B.



REFERENCE 10-11-00-555-015-A 12-24-34-600-001-A

DESIGNATION Procedure for the Installation of Wheel Chocks on Aircraft Bleeding of the Standby Air Data System

12-32-28-281-001-A 32-41-00-210-002-A

Drain Water Content Inspection/Check of the Wheels and Tires

32-41-00-210-003-A


3.


4.



Move the Aircraft NOTE :

if unserviceable tires are installed, do not do this procedure.

(1)

Remove the wheel chocks that you installed during the storage procedure.

(2)

Move the aircraft, by a 1/4 turn of the wheels, to prevent damage to the tires.

(3)

Put the wheel chocks in position: (Ref. TASK 10-11-00-555-015-A)

Subtask 10-12-00-210-072-A B.


Make sure that there is no fuel leak.

(2)

Examine the condition of the wheels and the tires (Ref. TASK 32-41-00-210-002-A).

(3)

Do a tire pressure check, if necessary inflate the tires (Ref. TASK 32-41-00-210-003-A).

Subtask 10-12-00-170-055-A C.

Drain the Standby Static Line (1)

AES

Remove the water from the standby static line (Ref. TASK 12-24-34-600-001-A).

10-12-00 PB601



5.

Inspection of the Fuel Tanks (1)

Drain water from the fuel tanks (Ref. TASK 12-32-28-281-001-A).

(2)

Drain water from ACT fuel tank, if installed (Ref. AMM 12-32-28-281-005) .


Put the aircraft back to its initial configuration. (1)

AES

Remove the access platform(s).

10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-200-008-A Periodic Ground-Check at 1-month Interval 1.


2.




Material No: 15-002 B.

DESIGNATION

SPECIAL MATERIALS VARNISH P.T.F.E SPRAY STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF


REFERENCE 12-32-28-281-003-A

DESIGNATION Sample Fuel for Microbiological Contamination Analysis

21-26-00-710-001-A

Operational Check of the Avionics Equipment Ventilation-System via MCDU

21-26-00-710-001-A-01

Operational Check of the Avionics Equipment Ventilation (without the CFDS)

21-28-00-710-006-A

Operational Test of the AFT Cargo-Compartment Ventilation-System

24-41-00-861-002-A

Energize the Aircraft Electrical Circuits from the External Power

24-41-00-861-002-A-01


24-41-00-861-002-A-02


24-41-00-862-002-A


24-41-00-862-002-A-01


24-41-00-862-002-A-02


28-24-00-710-002-A

Operational Test of the ENG 1(2) LP Fuel Valve

30-11-00-710-001-A

Operational Test of the Wing Ice-Protection System

30-21-00-710-001-A

Operational Test of the Anti Ice System Fault Warning

52-10-00-010-001-A


52-10-00-410-001-A


52-30-00-860-001-A


52-30-00-860-002-A ** On A/C 003-003 52-30-00-860-006-A


52-30-00-860-008-A

Close the Bulk Cargo-Compartment Door

71-00-00-550-010-A


AES

10-12-00 PB601



Job Set-up ** On A/C 004-099 Subtask 10-12-00-010-060-A A.

Get Access (1)


(2)

Open the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-860-001-A).

(3)

Open the emergency exit doors (Ref. AMM 52-22-00-010-001) .

** On A/C 003-003 Subtask 10-12-00-010-060-B A.

Get Access (1)


(2)

Open the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-860-001-A).

(3)

Open the emergency exit doors (Ref. AMM 52-22-00-010-001) .

(4)




Remove the STORAGE PRESERVATION (Material No: 15-002) and adhesive tape from : . the avionics ventilation-system inlets and outlets (15HQ and 22HQ) . the outflow valve (10HL).

(2)

Energize the aircraft electrical circuits from the external power (Ref. TASK 24-41-00-861-002-A) or (Ref. TASK 24-41-00-861-002-A-01) or (Ref. TASK 24-41-00-861-002-A-02).

(3)

On the overhead panel 25VU, on the CABIN PRESS section: . release the DITCHING pushbutton switch to open the avionics ventilation skin- valves. NOTE :

4.



Protection (1)

Apply SPECIAL MATERIALS (Material No: 05-043) on all the seals of the doors.

(2)

Make sure that all the doors operate correctly.

Subtask 10-12-00-210-079-A B.

AES

Inspection (1)

Make sure that the extension of the landing gear shock-absorbers is correct.

(2)

Do a check of the pressure of the oxygen cylinders.

(3)


(4)


10-12-00 PB601



Inspection of the Engine Humidity Indicator Examine the indicators. If one or more of the indicators shows too much humidity, replace the indicator and desiccant and do the engine preservation procedure again (Ref. TASK 71-00-00-550-010-A).

Subtask 10-12-00-710-071-A D.

5.

Do these Tests: (1)

Do a test of the avionics equipment ventilation (Ref. TASK 21-26-00-710-001-A) or (Ref. TASK 21-26-00-710-001-A-01).

(2)

If the aft cargo-compartment ventilation-system is installed, do a test of the aft cargo-compartment ventilation-system (Ref. TASK 21-28-00-710-006-A).

(3)

If the FWD cargo-compartment ventilation-system is installed, do a test of the FWD cargocompartment ventilation-system (Ref. AMM 21-28-00-720-003) .

(4)

Do a test of the wing ice-protection system (Ref. TASK 30-11-00-710-001-A).

(5)

Do a test of the anti ice system fault warning (Ref. TASK 30-21-00-710-001-A).

(6)

Do a test of the ENG 1(2) LP fuel valve 12QM (13QM) (Ref. TASK 28-24-00-710-002-A).


Put the Aircraft back to its Initial Configuration (1)

On the overhead panel 25VU, on the CABIN PRESS section: . push the DITCHING pushbutton switch to close the avionics ventilation skin- valves.

(2)


(3)


(4)

Close the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-860-002-A).

(5)

Close the emergency exit doors (Ref. AMM 52-22-00-410-001) .

(6)

Seal with STORAGE PRESERVATION (Material No: 15-002) and adhesive tape: . the avionics ventilation-system inlets and outlets (15HQ and 22HQ) . the outflow valve (10HL) . the doors and the handles.

(7)


** On A/C 003-003 Subtask 10-12-00-410-059-B A.

AES

Put the Aircraft back to its Initial Configuration (1)

On the overhead panel 25VU, on the CABIN PRESS section: . push the DITCHING pushbutton switch to close the avionics ventilation skin- valves.

(2)


(3)


(4)

Close the FWD and AFT cargo-compartment doors (Ref. TASK 52-30-00-860-002-A).

(5)

Close the bulk cargo-compartment door (Ref. TASK 52-30-00-860-008-A).

10-12-00 PB601



AES

(6)

Close the emergency exit doors (Ref. AMM 52-22-00-410-001) .

(7)

Seal with STORAGE PRESERVATION (Material No: 15-002) and adhesive tape: . the avionics ventilation-system inlets and outlets (15HQ and 22HQ) . the outflow valve (10HL) . the doors and the handles.

(8)


10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-200-009-A Periodic ground-check at 3-month interval 1.


2.




B.



Material No: 05-005 Material No: 05-027 Material No: 11-002 Material No: 15-002 C.


DESIGNATION

COMMON GREASES SILICONE GREASE PNEUMATIC SYST AND SEALS SPECIAL MATERIALS CORROSION PREVENTIVE SPECIAL MATERIALS CLEANING AGENTS DRY CLEANING SOLVENT (VARSOL/WHT SPIRIT) STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF


REFERENCE 05-27-10-200-001-A

DESIGNATION GENERAL VISUAL INSPECTION OF NOSE GEAR AND NOSE GEAR DOORS (EWIS)

05-27-30-200-001-A

GENERAL VISUAL INSPECTION OF LH/RH MAIN LANDING GEAR (EWIS)

07-12-00-582-001-A

Jacking for Nose Gear Wheel Change

07-12-00-582-002-A

Jacking for Main Gear Wheel Change

10-20-00-556-001-A

Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs

10-20-00-556-001-A-01 12-21-11-615-002-A

External Cleaning

24-41-00-861-002-A 24-41-00-861-002-A-01

Energize the Aircraft Electrical Circuits from the External Power Energize the Aircraft Electrical Circuits from the APU

24-41-00-861-002-A-02


24-41-00-862-002-A 24-41-00-862-002-A-01

De-energize the Aircraft Electrical Circuits Supplied from the External Power De-energize the Aircraft Electrical Circuits Supplied from the APU

24-41-00-862-002-A-02


27-14-00-710-001-A

Operational Test of the Aileron and Hydraulic Actuation

27-24-00-710-001-A

Operational Test of the Rudder Hydraulic Actuation

AES

10-12-00 PB601



DESIGNATION Operational Test of the Elevator and Hydraulic Actuation

27-54-00-710-001-A

Operational Test of the Flap System

27-64-00-710-001-A

Operational Test of the Spoiler Hydraulic Actuation

27-84-00-710-001-A 28-23-00-720-001-A

Operational Test of the Slat System Operational Test of Crossfeed Valve Using Individual Motors: ...

28-24-00-710-002-A

Operational Test of the ENG 1(2) LP Fuel Valve

28-29-00-710-001-A 29-10-00-200-001-A 29-10-00-863-003-A

Operational Test of the APU Low Pressure Fuel Valve using each individual Motor in turn Check Fluid Level on Reservoir Indicators Pressurize the Blue Hydraulic System with a Ground Power Supply

29-10-00-863-003-A-01

Pressurize the Blue Hydraulic System with the Blue Electric Pump

29-10-00-864-003-A

Depressurize the Blue Hydraulic System

29-23-00-863-001-A

29-24-00-863-001-A

Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU Pressurize the Yellow Hydraulic System with the Electric Pump

29-24-00-864-001-A


32-31-00-710-002-A

Operational Test of the Landing Gear Doors (With False Targets)

32-31-00-710-002-A-01

Operational Test of the Landing Gear Doors (Without False Targets)

51-74-11-300-001-A

Repair of Corroded Areas

53-59-00-210-001-A 54-50-00-200-001-A

Operational Check of Single Drain Pipe Aft of FR70 from Outside General Visual Inspection of Compartment A and F Pylon Drain System

29-23-00-864-001-A

3.


Get Access (1)

4.




AES

Do a visual inspection of the aircraft for impacts by foreign objects, bird nests, fluid leakages, (hydraulic fluid, fuel), missing parts, obstruction and corrosion of: (a)

the upper and the lower surface of the wing

(b)

the nacelles and the pylons

(c)

the external surfaces of the fuselage

(d)

the flight control surfaces

(e)

the leading and the trailing edge of the horizontal and vertical stabilizers

(f)

the external skin of: . the passenger/crew doors . the cargo doors

10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL .

(2)

the frame around the doors

(g)

the external handle of the passenger/crew doors

(h)

the drains: 1


2

On the pylons (Ref. TASK 54-50-00-200-001-A)

3


(i)

the toilet areas

(j)

all steel parts for corrosion.

If you find corrosion, remove it (Ref. TASK 51-74-11-300-001-A).

Subtask 10-12-00-615-056-A B.


Remove all the STORAGE PRESERVATION (Material No: 15-002) and adhesive tapes.

(2)

We recommend to clean the aircraft externally (Ref. TASK 12-21-11-615-002-A).

Subtask 10-12-00-650-055-A C.


Energize the aircraft electrical circuits from the external power (Ref. TASK 24-41-00-861-002-A) or (Ref. TASK 24-41-00-861-002-A-01) or (Ref. TASK 24-41-00-861-002-A-02).

(2)

On the overhead panel 25 VU, on the CABIN PRESS section: . release the DITCHING pushbutton switch to open the avionics ventilation skin valves and the outflow valves. NOTE :

(3)



Subtask 10-12-00-710-070-A D.

Do these Tests: (1)

Do a test of the crossfeed valves (Ref. TASK 28-23-00-720-001-A).

(2)

Do a test the engine LP-fuel shut-off valve (Ref. TASK 28-24-00-710-002-A).

(3)

Do a test of the APU shut-off valve (Ref. TASK 28-29-00-710-001-A).

(4)

Do a test of the aileron and its hydraulic system (Ref. TASK 27-14-00-710-001-A).

(5)

Do a test of the elevator and its hydraulic system (Ref. TASK 27-34-00-710-001-A).

(6)

Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-001-A).

(7)

Do a test of the flap system (Ref. TASK 27-54-00-710-001-A).

(8)

Do a test of the spoiler hydraulic system (Ref. TASK 27-64-00-710-001-A).

(9)

Do a test of the slat system (Ref. TASK 27-84-00-710-001-A).

(10) Do a test of the landing gear doors (Ref. TASK 32-31-00-710-002-A) or (Ref. TASK 32-31-00-710-002A-01).

AES

10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-12-00-210-074-A E.

Inspection of the Landing Gear (1)

Do a general visual inspection: . of the NLG (Ref. TASK 05-27-10-200-001-A) . of the MLG (Ref. TASK 05-27-30-200-001-A)

(2)

Remove the mooring tool from the NLG.

(3)

Lift and turn the wheels by hand to make sure that there is no defect on the bearings: . for NLG (Ref. TASK 07-12-00-582-001-A) . for MLG (Ref. TASK 07-12-00-582-002-A)

(4)

Put the aircraft on its wheels.

(5)

Put the aircraft in mooring condition (Ref. TASK 10-20-00-556-001-A) or (Ref. TASK 10-20-00-556-001-A-01).

(6)

Do a Check of each wheel-half for corrosion. If you find corrosion, clean with CLEANING AGENTS (Material No: 11-002) .

(7)

Do a check of all painted and unpainted parts for corrosion.

Subtask 10-12-00-620-093-A F.

Protection (1)

Apply SPECIAL MATERIALS (Material No: 05-027) in all the holes, specially in the area which can have condensation. On the wings, apply SPECIAL MATERIALS (Material No: 05-005) .

(2)

Apply COMMON GREASES (Material No: 04-011) on : . the sliding tube of the shock absorber . the actuator rods . the uplock mechanism.

Subtask 10-12-00-210-075-A G.

Inspection of the Hydraulic System (1)

Do a check of the reservoir fluid level (Ref. TASK 29-10-00-200-001-A).

(2)

Do a check for corrosion on hydraulic pipes and unions on the landing gear wells, the wings and the stabilizers.

Subtask 10-12-00-210-076-A H.

Inspection of the Flight Controls (1)

Check of the condition of the flight control cables in non-pressurized area and avionics compartment.

(2)

Do a check of all the flap tracks for corrosion.

(3)

Do a check of the slat tracks for corrosion.

Subtask 10-12-00-210-077-A J.

Inspection of the Fuel System (1)

Do a check of the fuel level in the tanks: (a)

if necessary refuel the tank(s): . to 30 % minimum if no contamination occurred. . to 90 % minimum if contamination occurred. NOTE :

AES

We recommend that you do not mix fuel treated with different biocides.

10-12-00 PB601




AES


On the overhead panel 25 VU, on the CABIN PRESS section : . release the DITCHING pushbutton switch to close the avionics ventilation skin valves and the outflow valve.

(2)


(3)


(4)

Install STORAGE PRESERVATION (Material No: 15-002) with new adhesive tape to prevent film hardening and paint removal.

(5)


10-12-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-12-00-200-010-A Periodic Ground Check at 6-month Intervals 1.

Reason for the Job This procedure prevents the damage of the landing gears seals.

2.



REFERENCE 32-31-00-720-002-A

3.

DESIGNATION Functional Test of the Normal Extension and Retraction of the Landing Gear


4.

Not Applicable


Test of the Landing Gear (1)

5.

Do a test of extension and retraction of the landing gear (Ref. TASK 32-31-00-720-002-A)



AES


10-12-00 PB601



MOORING - MAINTENANCE PRACTICES ** On A/C ALL Task 10-20-00-556-001-A Mooring of Aircraft without Weight and Balance Provision on the Landing Gear Legs WARNING WARN ING :

MAKE SURE SURE THAT THE GROUND GROUND SAFETY-LO SAFETY-LOCKS CKS ARE IN POSITION POSITION ON THE LANDING LANDING GEAR. GEAR.

CAUTION CAUT ION :

THE LAST FEET FEET OF ALL TAXIING TAXIING AND TOWING TOWING OPERATIO OPERATIONS NS MUST BE IN A STRAIGHT STRAIGHT LINE. LINE. THIS THIS IS TO PREVENT FORCE ON THE TIRES AND THE MAIN LANDING GEAR.

1.

Reas Re ason on fo forr th thee Jo Job b The function of mooring is to prevent damage to the aircraft on the ground in high wind conditions. This procedure is only applicable to aircrafts without weight and balance provision on the landing gear legs.

2.

Job Jo b Se Sett-up up In Info form rmat atio ion n A.

Fixtur Fix tures, es, Too Tools, ls, Tes Testt and and Supp Support ort Equ Equipm ipment ent


B.


DESIGNATION

Refere Ref erence nced d Inf Inform ormati ation on

REFERENCE 05-57-00-200-001-A

DESIGNATION

Aircraft Stability

10-1 10 -111-00 00-5 -555 55-0 -007 07-A -A

Parkin Park ing g Pr Proc oced edur uree in Fl Flig ight ht-r -rea eady dy Co Cond ndit itio ion n (P (Par arki king ng of no nott mo more re th than an 15 Days)

10-1110-1 1-00 00-5 -555 55-0 -015 15--A 12-3 12 -344-24 24-8 -869 69-0 -002 02--A

Proced Proc edur uree for the In Inst stal alla lati tion on of Wh Whee eell Ch Choc ocks ks on Ai Airc rcrraf aftt Airc Ai rcra rafft Gr Grou ound ndiing fo forr the Mai aint nteena nanc ncee Op Opeera rattio ions ns

32-0 32 -000-00 00-4 -481 81-0 -001 01--A

Inst In stal alllat atio ion n of the Saf afet etyy De Devi vice cess on th thee La Land ndiing Ge Gear arss

32-41-00-210-002-A

Insspection/Check of the Wheels and Tires In

32-47-15-000-001-A 32-47-15-400-001-A

Removal of the Brake Temperature Sensor Insstal In alllat atiion of the Brak akee Temperature Sensor

(Ref. Fig. 10-20-00-991-00700-A - Mooring Wind Speed Limits) (Ref.. Fig. 10-20-00-991-00 (Ref 10-20-00-991-00500 500-A -A - Positi Position on of the Ground Rings) (Ref.. Fig. 10-20-00-991-00 (Ref 10-20-00-991-00300 300-A -A - Posit Position ion of the Mooring Ropes) (Ref. Fig. 10-20-00-991-00800-A - Nose Landing Gear - Installation of the Mooring Items) (Ref. Fig. 10-20-00-991-00600-A - Main Landing Gear - Installation of the Mooring Items) 3.

Job Se Sett-up up Subtask 10-20-00-941-050-A A.

Weat We athe herr Li Limi mits ts (1)) (1

Wind Wi nd co condi nditi tion onss (a)

AES

For win wind d speed speedss of les lesss than than 50 50 Kts: Kts: - Mooring is not necessary if the aircraft configuration is in the limits given in chapter 05-57-00.

10-20-00 PB201



If the wind wind speed is betwee between n 50 and 70 Kts and stable stable (no (no gusts and the wind wind directi direction on does not not change by more than +/- 30 degrees) and the aircraft points into the wind: - Moor the aircraft at the NLG only. NOTE NO TE :

(c)

If the wind wind speed is betwee between n 50 and 70 Kts and not stabl stable, e, with with the directi direction on that chang changes es by more than +/- 30 degrees: - Point the aircraft into the primary wind direction (if possible) and moor at the NLG and the MLG.

(d)

If the wind wind speed speed is between between 70 Kts Kts and the upper upper limits limits defin defined ed in: (Ref. Fig. 10-20-00-991-00700-A - Mooring Wind Speed Limits) - Make sure that the aircraft variant mass is sufficient for the necessary wind speed - Point the aircraft into the primary wind direction (if possible) and moor at the NLG and MLG. NOTE :

(e)

(2)

If it is is not poss possibl iblee to point point the the aircr aircraft aft int intoo the wind wind,, see para para (c). (c).

If you canno cannott get the necess necessary ary aircraft aircraft varia variant nt mass, mass, you must move move the the aircraft aircraft into a hangar.

If the the wind speed speed is more more than than the maxi maximum mum limi limits ts given given in: in: (Ref. Fig. 10-20-00-991-00700-A - Mooring Wind Speed Limits) - You must move the aircraft into a hangar.

Icing Ici ng condit condition ion limit limitss in high high wind wind conditi conditions ons (a)

For a tempe temperat rature ure of less less than than -5 deg.C deg.C (23.00 (23.00 deg.F deg.F): ): . Mov Movee the the air aircra craft ft int into o a hanga hangar. r.

(b)

For a tempe temperat rature ure of more more than than -5 deg.C deg.C (23.00 (23.00 deg.F deg.F): ): . If there there is ice or if ice ice is possibl possible, e, Airbus Airbus recomm recommend endss that you put put salt around around and below below the the tires. . If there there is thick thick ice or compa compacte cted d snow, snow, remove remove the ice ice or snow, snow, or move the the aircraf aircraftt into a hangar.

Subtask 10-20-00-860-050-A B.

AES

Aircra Air craft ft Mai Mainte ntenan nance ce Con Config figura uratio tion n (1)

Put the aircr aircraft aft in positio position n on a flat flat surface surface with with the mooring mooring point points. s. Make sure that the wheels of the nose landing gear are on the aircraft axis and that the aircraft points into the wind. Make sure that the ground rings are in the ground-ring position area. (Ref.. Fig. 10-20-00-991-005 (Ref 10-20-00-991-00500 00-A -A - Posit Position ion of the Ground Rings) (Ref.. Fig. 10-20-00-991-003 (Ref 10-20-00-991-00300 00-A -A - Positi Position on of the Moori Mooring ng Ropes)

(2)

In relation relation to the wind speed, speed, make sure sure that the aircraft aircraft is stable. stable. Refer to the the aircraft aircraft stability stability procedure (Ref. TASK 05-57-00-200-001-A).

(3)

Make sure that that the landing-gear landing-gear safety safety devices devices are in position position (Ref. (Ref. TASK 32-00-00-48 32-00-00-481-001 1-001-A). -A).

(4)

Electricall Elect ricallyy ground ground the aircraf aircraftt (Ref. (Ref. TASK 12-34-24 12-34-24-869-0 -869-002 02-A). -A).

(5)

Put the CHOCK - WHEEL(S WHEEL(S)) in position position (Ref. (Ref. TASK TASK 10-11-00-5 10-11-00-555-015 55-015-A). -A).

(6)

Make sure that that the flaps, flaps, the slats, the spoilers spoilers,, the speed brakes brakes and the thrust thrust reversers reversers are retracted. retracted.

(7)

Makee sure Mak sure that that the the THS is is set to neutr neutral. al.

(8)

Makee sure that Mak that the slidin sliding g windows windows of the the cockpi cockpitt are closed. closed.

(9)

Make sure sure that the passenge passenger/cre r/crew w doors and the the cargo compart compartment ment doors doors are closed. closed.

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (10) Put the aircraft in the parkin parking g configuration configuration (Ref. TASK 10-11-00-555-0 10-11-00-555-007 07-A) -A) in relation to weather conditions. (11) Make sure the aircraft aircraft variant weight is commensura commensurate te with the wind speed expected expected (Ref. Fig. 10-20-00-991-00700-A - Mooring Wind Speed Limits) . (12) Remov Removee the brake temp temperatur eraturee sensors and cables (Ref. (Ref. TASK 32-4732-47-15-00 15-000-001 0-001-A). -A). 4.

Pro roce cedu dure re Subtask 10-20-00-481-050-A A.

Moor Mo orin ingg of of the the No Nose se La Land ndin ing g Gea Gearr (1)

With the With the moori mooring ng item itemss that that foll follow: ow: (Ref. Fig. 10-20-00-991-00800-A - Nose Landing Gear - Installation of the Mooring Items)

DESCRIPTION

ITEM

QUANTITY

LENGTH

Textile Roundsling

1

2

Joker

2

2

2000 mm 78.74 in /

Polyester Lashing Strap with Ratchet Mechanism (with the ratchet mechanism in the center of the lash)

4&7

4

as necessary

Steel Bow Shackle

5

4

/

Master Link

3

2

/

Ground Ring (set into ground)

6

4

/

NOTE :

AES

MIN ULTIMATE FAILURE LOAD 12945 daN 29101 lbf 24271 daN 54563 lbf 9807 daN 22047 lbf

7845 daN 17636 lbf 24271 daN 54563 lbf 15691 daN 35275 lbf

The manuf manufactur acturer er of the the mooring mooring equipm equipment ent (shown (shown in the the table table above) above) can can possibly possibly also also supply supply a Minimum Ultimate Failure Load or a Safe Working Load with a Safety Factor for the equipment. The Minimum Ultimate Failure Load is the load at which equipment failure will occur. The Safe Working Load is lower than the Minimum Ultimate Failure Load. To calculate the Safe Working Load, you must use a special safety factor applicable for the initial function of the equipment. If a Safe Working Load is shown on the equipment, you can multiply this load by the Safety Factorr give Facto givenn by the manufacture manufacturerr to get the Minim Minimum um Ultim Ultimate ate Failure Load of the equipment. equipment. You must then make sure that the calculated Minimum Ultimate Failure Load is equal to or more than the value given in the table above for the related equipment. Here is an example: A textile roundsling has a Safe Working Load of 5000 daN. A Safety Factor of 7 is given by the manufacturer. Minimum Ultimate Failure Load = 5000 daN x 7 = 35000 daN The minimum permitted failure load of the textile roundsling for this configuration (as shown in the above table) is 12945 daN. The equipment is thus serviceable.

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL NOTE :

Roundslings are continuous loops. The Roundsling Minimum Failure Load relates to the Roundsling load as a single loop.

NOTE :

It is not necessary to use the bow shackle in the system. If you do not use the bow shackle, use the ratchet mechanism to attach the two ends of the lashing strap together. But we recommend that you use the bow shackle to make installation easier.

(a)

Wind two roundslings (1) around the NLG sliding tube and below the axles.

(b)

Pull each roundsling (1) to a point that is in line with the centerline of the sliding tube (make sure that each section of roundslings is of equal length). Then attach them to the roundsling joker hook (2).

(c)

Attach the joker (2) to the master link (3).

(d)

Get one lash with the integral ratchet mechanism assembly (4) and put one of its ends through the ground ring (6).

(e)

Put the other end of the lash (4) through the master link (3). Move the two loose ends of the lash (4) to a point in the middle between the ground ring (6) and the master link (3).

(f)

Connect the two ends of the lash (4) together with a bow shackle (5).

(g)

Do steps (d) thru (f) again for each ground position.

(h)

Use the integral ratchet (7) to lightly pull each lash (4) so that it is not loose. Make sure that the last lateral position of the master link (3) is in the axis of the centerline of the sliding tube. NOTE :

(i) (2)

The function of the ratchet (7) is to make sure that the lashes (4) are not loose but not to put tension in the system.

Make sure that the polyester lash axes are in the ground-ring position area. (Ref. Fig. 10-20-00-991-00500-A - Position of the Ground Rings)

Post Mooring Inspection Because wind speed is not constant or predictable, it is necessary to examine the landing gear for damage. This is to prevent the possible effects of too much wind speed and thus a possible landing gear overload. Because of this, you must do the inspections that follow after the mooring configuration is removed (when high winds stop). (a)

Do a visual inspection of the roundsling interfaces on the sliding tube and axle for signs of damage to the landing-gear surface finish (chrome detachment, scratches or flaking paint).

(b)

Do a check of the tires for flat spots and signs of increased wear (Ref. TASK 32-41-00-210-002A).

(c)

Do an inspection of the NLG/fuselage attachments and make sure that: . There are no cracks. . There is no damage to the paint and sealant.

Subtask 10-20-00-481-052-A B.

Mooring of the Main Landing Gear (1)

With the mooring items that follow: (Ref. Fig. 10-20-00-991-00600-A - Main Landing Gear - Installation of the Mooring Items)

DESCRIPTION

Textile Roundsling

AES

ITEM

1

QUANTITY

4

LENGTH

2000 mm 78.74 in

MIN ULTIMATE FAILURE LOAD 12945 daN 29101 lbf

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL DESCRIPTION

ITEM

QUANTITY

LENGTH

Joker

2

4

/

Polyester Lashing Strap with Ratchet Mechanism (with the ratchet mechanism in the center of the lash)

4&7

8

as necessary

Steel Bow Shackle

5

8

/

Master Link

3

4

/

Ground Ring (set into ground)

6

8

/

AES

MIN ULTIMATE FAILURE LOAD 24271 daN 54563 lbf 9807 daN 22047 lbf

7845 daN 17636 lbf 24271 daN 54563 lbf 15691 daN 35275 lbf

NOTE :

The manufacturer of the mooring equipment (shown in the table above) can possibly also supply a Minimum Ultimate Failure Load or a Safe Working Load with a Safety Factor for the equipment. The Minimum Ultimate Failure Load is the load at which equipment failure will occur. The Safe Working Load is lower than the Minimum Ultimate Failure Load. To calculate the Safe Working Load, you must use a special safety factor applicable for the initial function of the equipment. If a Safe Working Load is shown on the equipment, you can multiply this load by the Safety Factor given by the manufacturer to get the Minimum Ultimate Failure Load of the equipment. You must then make sure that the calculated Minimum Ultimate Failure Load is equal to or more than the value given in the table above for the related equipment. Here is an example: A textile roundsling has a Safe Working Load of 5000 daN. A Safety Factor of 7 is given by the manufacturer. Minimum Ultimate Failure Load = 5000 daN x 7 = 35000 daN The minimum permitted failure load of the textile roundsling for this configuration (as shown in the above table) is 12945 daN. The equipment is thus serviceable.

NOTE :

Roundslings are continuous loops. The Roundsling Minimum Failure Load relates to the Roundsling load as a single loop.

NOTE :

It is not necessary to use the bow shackle in the system. If you do not use the bow shackle, use the ratchet mechanism to attach the two ends of the lashing strap together. But we recommend that you use the bow shackle to make installation easier.

(a)

Wind two roundslings (1) around the left MLG sliding tube and below the axles.

(b)

Pull each roundsling (1) to a point that is in line with the centerline of the sliding tube (make sure that each section of roundslings is of equal length). Then attach them to the roundslings joker hooks (2).

(c)

Attach the joker (2) to the master link (3).

(d)

Get one lash with the integral ratchet mechanism assembly (4) and put one of its ends through the ground ring (6).

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (e)

Put the other end of the lash (4) through the master link (3). Move the two loose ends of the lash (4) to a point in the middle between the ground ring (6) and the master link (3).

(f)

Connect the two ends of the lash (4) together with a bow shackle (5).

(g)

Do steps (d) thru (f) again for each ground position.

(h)

Use the integral ratchet (7) to lightly pull each lash (4) so that it is not loose. Make sure that the last lateral position of the master link (3) is in the axis of the centerline of the sliding tube. NOTE :

(2)

5.

The function of the ratchet (7) is to make sure that the lashes (4) are not loose but not to put tension in the system.

(i)

Do steps (a) thru (h) again for the right MLG.

(j)

Make sure that the polyester lash axes are in the ground-ring position area. (Ref. Fig. 10-20-00-991-00500-A - Position of the Ground Rings) .

Post Mooring Inspection Because wind speed is not constant or predictable, it is necessary to examine the landing gear for damage. This is to prevent the possible effects of too much wind speed and thus a possible landing gear overload. Because of this, you must do the inspections that follow after the mooring configuration is removed (when high winds stop). (a)

Do a visual inspection of the roundsling interfaces on the sliding tube and axle for signs of damage to the landing-gear surface finish (chrome detachment, scratches or flaking paint).

(b)

Do a check of the tires for flat spots and signs of increased wear (Ref. TASK 32-41-00-210-002A).

(c)

If there was possible interference between the roundslings and MLG dressings, do a detailed visual inspection of the MLG dressings and attachments for signs of damage/wear.

(d)

Do an inspection of the brake piston housing for signs of damage to the surface finish (wear, flaking paint).

(e)

Do an inspection of the MLG/wing attachments and make sure that: . There are no cracks. . There is no damage to the paint and sealant.

(f)

If you find damage during inspections, replace or repair the damaged component (refer to the applicable manuals SRM, AMM, CMM) and make sure that the adjacent area has no damage.


AES


After removal of the mooring equipment, install the brake temperature sensors and cables (Ref. TASK 32-47-15-400-001-A).

(2)


(3)

Make sure that the work area is clean and clear of tool(s) and other items.

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL 0 0 0 8 9

0 0 0 8 8

0 0 0 8 7

0 0 0 8 6

) g K ( S S A M T F A R C R I A 0 2 3 A

0 0 0 8 5

0 0 0 8 4

0 0 1

5 9

0 9

5 8

5 7

0 8

0 7

0 0 0 5 8 6 3

MAX MOORING WIND SPEED (Kts)

N_MM_102000_2_BAM0_01_00

AES

FIGURE 10-20-00-991-00700-A SHEET 1 Mooring Wind Speed Limits

10-20-00 PB201



MAX ANGLE

2.0m (78.74in.) 0.4m (15.75in.)

MIN ANGLE

1.0m (39.37in.)

2.0m (78.74in.)

MASTER LINK POSITION

AREA OF GROUND RING POSITION

NOTE : THERE IS A MINIMUM LIMIT FOR THE DISTANCE BETWEEN THE GROUND RINGS AND THE MLG. THERE IS NO MAXIMUM LIMIT FOR THIS DISTANCE ALTHOUGH THE GROUND RING POSITIONS CANNOT MAKE STRAP ANGLES LARGER OR SMALLER THAN THE ANGLES PERMITTED BY THE NEAR LIMITS.OPERATORS MUST TRY TO KEEP THE GROUND POINTS SYMMETRICAL IN RELATION TO THE MLG CENTER LINES.

N_MM_102000_2_AGM0_01_00

AES

FIGURE 10-20-00-991-00500-A SHEET 1 Position of the Ground Rings

10-20-00 PB201



N_MM_102000_2_AEM0_01_00

AES

FIGURE 10-20-00-991-00300-A SHEET 1 Position of the Mooring Ropes

10-20-00 PB201



1

2

3

A

A

3

2

1 1 NOTE: ROUNDSLINGS ARE CONTINUOUS LOOPS

N_MM_102000_2_ACT0_01_00

AES

FIGURE 10-20-00-991-00800-A SHEET 1 Nose Landing Gear - Installation of the Mooring Items

10-20-00 PB201



6

7

3

2

1

2

3

1

5 5

4

7 4

6

N_MM_102000_2_ACT0_02_00

AES


10-20-00 PB201



6

4

5

3

5 7 6

6

7

3

2

1

2

4

7

1

5 5

4

7 4 6

N_MM_102000_2_ACT0_03_00

AES


10-20-00 PB201



1

2

3

A

A 3

2

1

1 NOTE: ROUNDSLINGS ARE CONTINUOUS LOOPS

N_MM_102000_2_AHM0_01_00

AES

FIGURE 10-20-00-991-00600-A SHEET 1 Main Landing Gear - Installation of the Mooring Items

10-20-00 PB201



6

7

3

2 1

2

3

1

5 5

4

7 4

6

N_MM_102000_2_AHM0_02_00

AES


10-20-00 PB201



6

4

5

3

5 7

6

7

3

6

2 1

2

4

7

1 5 5

4

7 4

6

N_MM_102000_2_AHM0_03_00

AES


10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C ALL Task 10-20-00-556-001-A-01 Mooring of Aircraft with Weight and Balance Provision on the Landing Gear Legs WARNING :

MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR.

CAUTION :

THE LAST FEET OF ALL TAXIING AND TOWING OPERATIONS MUST BE IN A STRAIGHT LINE. THIS IS TO PREVENT FORCE ON THE TIRES AND THE MAIN LANDING GEAR.

1.

Reason for the Job The function of mooring is to prevent damage to the aircraft on the ground in high wind conditions. This procedure is only applicable to aircraft with weight and balance provision on the landing gear legs.

2.





No specific

AR

SHACKLES - NLG

98D10203500004

1

MOORING KIT-NLG (USED FOR OPT. B727 TOWING BRACKET)

B.

DESIGNATION


REFERENCE 05-57-00-200-001-A

DESIGNATION

Aircraft Stability

10-11-00-555-007-A

Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days)

10-11-00-555-015-A 12-34-24-869-002-A 32-00-00-481-001-A

Procedure for the Installation of Wheel Chocks on Aircraft Aircraft Grounding for the Maintenance Operations Installation of the Safety Devices on the Landing Gears

(Ref. Fig. 10-20-00-991-00200-A - Attachment of the Mooring Ropes on the Nose Landing Gear) (Ref. Fig. 10-20-00-991-00300-A - Position of the Mooring Ropes) 3.


Weather Limits (1)

Wind conditions For wind speeds of less than 50 Kts: . mooring is not necessary if the aircraft configuration is in the limits given in chapter 05-57-00. If the aircraft points into the wind and wind speed is: . between 50 and 70 Kts, moor the aircraft at the NLG, . more than 70 Kts, moor the aircraft at the NLG and MLG. If the aircraft does not point into the wind or the direction of the wind is not stable: . for wind speeds or gusts more than 50 Kts, moor the aircraft at the NLG and the MLG.

(2)

Icing condition limits in high wind conditions: (a)

AES

For a temperature of less than -5 deg.C (23.00 deg.F): . Move the aircraft into a hangar.

10-20-00 PB201



For a temperature of more than -5 deg.C (23.00 deg.F): . If there is ice or if ice is possible, Airbus recommends that you put salt around and below the tires. . If there is thick ice or compacted snow, remove the ice or snow, or move the aircraft into a hangar.

Subtask 10-20-00-860-051-A B.


Put the aircraft in position on a flat surface with the mooring points. Make sure that the wheels of the nose landing gear are on the aircraft axis and that the aircraft points into the wind.

(2)

In relation to the wind speed, make sure that the aircraft is stable. Refer to the aircraft stability procedure (Ref. TASK 05-57-00-200-001-A).

(3)

Make sure that the landing-gear safety devices are in position (Ref. TASK 32-00-00-481-001-A).

(4)

Electrically ground the aircraft (Ref. TASK 12-34-24-869-002-A).

(5)

Put the CHOCK - WHEEL(S) in position (Ref. TASK 10-11-00-555-015-A).

(6)

Make sure that the flaps, the slats, the spoilers, the speed brakes and the thrust reversers are retracted.

(7)

Make sure that the THS is set to neutral.

(8)

Make sure that the sliding windows of the cockpit are closed.

(9)

Make sure that the passenger/crew doors and the cargo compartment doors are closed.

(10) Put the aircraft in the parking configuration (Ref. TASK 10-11-00-555-007-A) in relation to weather conditions. 4.


Mooring of the Nose Landing Gear (1)

With the Mooring Kit (a)

(2)

Put the MOORING KIT-NLG (USED FOR OPT. B727 TOWING BRACKET) (98D10203500004) in position.

Or with Ropes (Ref. Fig. 10-20-00-991-00200-A - Attachment of the Mooring Ropes on the Nose Landing Gear) (Ref. Fig. 10-20-00-991-00300-A - Position of the Mooring Ropes) (a)

Attach the short ropes (1) of a diameter of 50.8 mm (2.0000 in.) in position on the towing lug of the nose landing gear with the SHACKLES - NLG. NOTE :

If manila or sisal rope is used, make sure that there is not too much tension on the rope because contraction can occur in wet weather.

(b)

Attach the other ropes (2) of a diameter of 50.8 mm (2.0000 in.).

(c)

Attach all the ropes on the ground with the mooring points. Put tension on this assembly.

Subtask 10-20-00-481-055-A B.

Mooring of the Main Landing Gear with Ropes (Ref. Fig. 10-20-00-991-00300-A - Position of the Mooring Ropes)

AES

10-20-00 PB201



Attach the ropes (3) and (4) of a diameter of 50.8 mm (2.0000 in.) on the towing lug and the debogging lug of the main landing gear. NOTE :

(2) 5.

If manila or sisal rope is used, make sure that there is not too much tension on the rope because contraction can occur in wet weather.

Attach the ropes on the ground with the mooring points. Put tension on this assembly.


AES



(2)

Make sure that the work area is clean and clear of tool(s) and other items.

10-20-00 PB201



A

A

1

2

GROUND RING OR STAKE

N_MM_102000_2_ACM0_01_00

AES

FIGURE 10-20-00-991-00200-A SHEET 1 Attachment of the Mooring Ropes on the Nose Landing Gear

10-20-00 PB201


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL DELETED

AES

10-20-00 PB201

Page May 01/12 Revision n˚: 40


RETURN TO SERVICE - INSPECTION/CHECK ** On A/C ALL Task 10-30-00-554-005-A Return to Operation after Storage Period CAUTION :

1.



2.





No specific

1

B.



Material No: 02-008 Material No: 04-004 Material No: 05-005 Material No: 15-002 C.

WARNING NOTICE(S)

DESIGNATION

HYDRAULIC FLUIDS NO LONGER AVAILABLE HYDRAULIC FLUIDS HYDRAULIC FLUID COMMON GREASES SYNTH. ESTER BASED GREASE HIGH PRESSURE SPECIAL MATERIALS CORROSION PREVENTIVE STORAGE PRESERVATION BARRIER MATERIAL WATER VAPOR PROOF


REFERENCE 10-11-00-555-014-A


12-13-27-612-002-A

Oil Replenishment of the Flap PCU Gearbox

12-13-27-612-003-A

Oil Replenishment of the Slat PCU Gearbox

** On A/C 005-099 12-13-27-612-005-A 12-13-80-600-011-B 12-14-32-614-001-A

AES

Drain and Refill Flap Actuator Assemblies with Semi-fluid Drain and Replenish Oil System Nitrogen Filling of the Tires

10-30-00 PB601



DESIGNATION Check of MLG Shock Absorber Charge Pressure

12-14-32-614-004-A

Check NLG Shock Abso sorrber Char arg ge Press ssu ure

12-21-11-615-002-A

External Cleaning

12-2212-2 2-27 27-6 -640 40-0 -003 03-A -A 12-22-27-640-004-A

Lubric Lubr icat atio ion n of Tr Trim imma mabl blee Ho Hori rizo zont ntal al St Stab abil iliz izer er Ac Actu tuat ator or Ba Ball ll Sc Scre rew w Nu Nutt Lubr briicate al alll Carriage Rollers on all Flap Tracks

12-2 12 -222-27 27-6 -640 40-0 -005 05--A

Lubr Lu bric icat atiion of Sp Spoi oiller No No.1 .1 to 5 Se Serv rvo o Co Cont ntrrol Be Bear arin ings gs

12-2 12 -222-27 27-6 -640 40-0 -006 06-A -A

Lubr Lu bric icat atio ion n of al alll Sl Slat at Tr Trac ackk Ro Roll ller ers, s, Pi Pini nion on Be Bear arin ings gs,, Pi Pini nion onss an and d Ra Rack ck Te Teet eth h

12-22-27-640-007-A ** On A/C 003-004

Lubrication of the THS Mechanical Control Chai ain ns

12-22-27-640-008-A

Remove Flap Rotar aryy Actua uattors For Regreas asiing

12-22-32-640-001-A

Lubrication of Main Lan and ding Gear and Doors

12-22-32-640-002-A

Lubri riccation of Nose Landing Gear and Doors

12-2 12 -222-53 53-6 -640 40-0 -001 01-A -A

12-2 12 -222-55 55-6 -640 40-0 -001 01--A

Lubric Lubr icat atio ion n of Tr Trim imma mabl blee Ho Hori rizo zont ntal al St Stab abil iliz izer er Be Bear arin ings gs an and d At Atta tach chme ment nt Fittings with Grease Mat. No. 04-004 Lubr Lu bric icat atio ion n of Tr Trim imma mabl blee Ho Hori rizo zont ntal al St Stab abil iliz izer er Be Bear arin ings gs an and d At Atta tach chme ment nt Fittings with Grease Mat. No. 04-037 Lubr Lu briica cati tion on of Ru Rudd dder er Hi Hing ngee Be Bear arin ing g No No.. 6 wi with th Gr Grea ease se Mat at.. No No.. 04 04-0 -004 04

12-2 12 -222-55 55-6 -640 40-0 -002 02--A

Lubr Lu briica cati tion on of Ru Rudd dder er Hi Hing ngee Be Bear arin ing g No No.. 6 wi with th Gr Grea ease se MA MAT. T. No No.. 04 04-0 -037 37

12-32-28-281-001-A 12-3 12 -322-28 28-2 -281 81-0 -003 03--A 12-3 12 -322-29 29-2 -281 81-0 -001 01--A

Drain Water Content Samp Sa mplle Fue uell for Mi Miccro robi biol olog ogic ical al Co Cont ntam amin inat atio ion n Ana nallys ysis is Hydr Hy drau aullic Fl Flui uid d Sa Sam mpl plee of Gr Gree een, n, Blu luee an and d Ye Yell llow ow Sy Syst stem emss for An Anal alys ysis is

20-24-11-100-001-A

Cleaning and Protection of the Cables

21-2121-2 1-41 41-9 -920 20-0 -002 02--A 21-2 21 -266-00 00-7 -710 10-0 -001 01-A -A

Schedu Sche dulled Re Repl plac acem emen entt of the Rec eciirc rcul ulat atio ion n Fil iltter 40 4012 12HM HM Oper Op erat atio iona nall Ch Chec eckk of th thee Av Avio ioni nics cs Eq Equi uipm pmen entt Ve Vent ntil ilat atio ionn-Sy Syst stem em vi viaa MC MCDU DU

21-2 21 -266-00 00-7 -710 10-0 -001 01-A -A-0 -011

Operat Ope ratio iona nall Ch Chec eckk of th thee Av Avio ioni nics cs Eq Equi uipm pmen entt Ve Vent ntil ilat atio ion n (w (wit itho hout ut th thee CF CFDS DS))

21-2 21 -288-00 00-7 -720 20-0 -004 04-A -A

Func Fu ncti tion onal al Te Test st of th thee AF AFT T Ca Carg rgoo-Co Comp mpar artm tmen entt Ve Vent ntil ilat atio ionn-Sy Syst stem em

23-6 23 -611-00 00-2 -200 00-0 -001 01-A -A

- Ch Chec eckk Re Resi sist stan ance ce of Ti Tip p to Re Reta tain iner er - Ch Chec eckk Bo Bond ndin ing g of Re Reta tain iner er to St Stru ruct ctur uree

23-7 23 -711-35 35-4 -400 00-0 -001 01--A

Inst In stal alla lati tio on of th thee Co Cock ckpi pitt Vo Voic icee Re Reco cord rder er (CV CVR) R) 1R 1RK K

24-2 24 -211-00 00-6 -600 00-0 -040 40--A

Pres Pr eser ervvat atio ion/ n/St Stor orag age/ e/R Ret etur urn n to Ser ervi vice ce of th thee ID IDG G

24-38-51-400-001-A 24-4 24 -411-00 00-8 -861 61-0 -002 02-A -A 24-4 24 -411-00 00-8 -861 61-0 -002 02-A -A-0 -011

Installation of the Batteries Ener En ergi gize ze th thee Ai Airc rcra raft ft El Elec ectr tric ical al Ci Circ rcui uits ts fr from om th thee Exte Extern rnal al Po Powe werr Ener En ergi gize ze th thee Ai Airc rcra raft ft El Elec ectr tric ical al Ci Circ rcui uits ts fr from om th thee AP APU U

24-4 24 -411-00 00-8 -861 61-0 -002 02-A -A-0 -022

Ener En ergi gize ze th thee Ai Airc rcra raft ft El Elec ectr tric ical al Ci Circ rcui uits ts fr from om En Engi gine ne 1( 1(2) 2)

24-4 24 -411-00 00-8 -862 62-0 -002 02-A -A

De-e De -ene nerg rgiz izee th thee Ai Airc rcra raft ft El Elec ectr tric ical al Ci Circ rcui uits ts Su Supp ppli lied ed fr from om th thee Ex Exte tern rnal al Po Powe werr

24-4 24 -411-00 00-8 -862 62-0 -002 02-A -A-0 -011

De-e De -ene nerg rgiz izee th thee Ai Airc rcra raft ft El Elec ectr tric ical al Ci Circ rcui uits ts Su Supp ppli lied ed fr from om th thee AP APU U

24-4 24 -411-00 00-8 -862 62-0 -002 02-A -A-0 -022

De-e De -ene nerg rgiz izee th thee Ai Airc rcraf raftt El Elec ectr tric ical al Ci Circ rcui uits ts Su Supp ppli lied ed fr from om th thee En Engi gine ne 1( 1(2) 2)

25-23-42-000-002-A

Removal of the Ce Ceiiling Pane nells - Aft Utility Area

25-2 25 -233-42 42-4 -400 00-0 -002 02--A

Inst In stal alla lati tion on of the Ce Ceiili ling ng Pan anel elss - Af Aftt Uti tillit ityy Are reaa

25-6 25 -655-00 00-7 -740 40-0 -001 01--A

Emeerg Em rgen ency cy Lo Loca cato torr Tr Tran ansm smiitt tter er (E (ELT LT)) Sy Syst stem em - BI BITE TE Te Test st

25-6 25 -655-35 35-4 -400 00-0 -001 01--A

Inst In stal alla lati tion on of th thee Em Emer erge genc ncyy Lo Loca cato torr Tr Tran ansm smit itte terr (EL ELT) T)

26-12-00-710-001-A

Operational Check of Loop/Squib

12-2 12 -222-53 53-6 -640 40-0 -002 02-A -A

AES

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 26-2 26 -211-00 00-7 -710 10-0 -002 02--A

DESIGNATION Opeera Op rattio iona nall Che heck ck of Bot ottl tlee Lo Loww-Pr Pres essu sure re In Indi dica cati ting ng-C -Ciirc rcui uitt

26-2 26 -211-00 00-7 -720 20-0 -003 03--C

Chec Ch eckk Di Dist stri ribu buti tio on Pi Pipi ping ng for Le Leak akag agee an and d Ob Obst stru ruct ctio ion n

26-2 26 -211-00 00-7 -720 20-0 -003 03-C -C-0 -011

Chec Ch eckk Di Dist stri ribu buti tion on Pi Pipi ping ng fo forr Le Leak akag agee an and d Ob Obst stru ruct ctio ion n

26-2 26 -211-41 41-4 -400 00-0 -001 01--A

Inst In stal alllat atio ion n of the En Engi gine ne Fi Fire re-E -Ext xtin ingu guis ishe herr Bot ottl tlee

26-2 26 -222-00 00-2 -210 10-0 -001 01--A

Insp In spec ecttio ion n of the APU Fi Firree-Ex Exti ting ngui uish shiing Di Dist strrib ibut utio ion n Pi Pipi ping ng

26-2 26 -222-00 00-7 -710 10-0 -001 01--A

Opeera Op rati tio ona nall Te Test st of th thee AP APU U Fir iree-Ex Exttin ingu guis ishi hing ng Loo oop/ p/Sq Squi uib b

26-2 26 -222-00 00-7 -710 10-0 -003 03-A -A

Operat Oper atio iona nall Te Test st of th thee Lo Loww-Pr Pres essu sure re In Indi dica cati ting ng Ci Circ rcui uitt of th thee AP APU U Fi Fire re-Extinguishing Bottle

26-22-41-400-001-A

Insstallation of the Fire Exting In ngui uish sheer Bottle

** On A/C 005-099 26-2 26 -233-00 00-2 -200 00-0 -001 01--A

Chec Ch eckk Fi Fire re Ex Exttin ingu guis ishe herr Li Line ness fo forr Le Leak akag agee an and d Bl Bloc ocka kage gess

26-2 26 -233-00 00-7 -710 10-0 -001 01-A -A

Oper Op erat atio iona nall Te Test st of th thee Ca Carg rgoo-Co Comp mpar artm tmen entt Fi Fire re-E -Ext xtin ingu guis ishi hing ng Sy Syst stem em

26-2 26 -233-41 41-4 -400 00-0 -004 04--A

Inst In stal alllat atiion of the Ca Carg rgo o Fir iree-Ex Exttin ingu guis ishe herr Bo Botttl tlee

26-2 26 -244-00 00-2 -210 10-0 -001 01--A

Insp In spec ecttio ion/ n/Ch Chec eckk of the Po Port rtab able le Fir iree Ex Exti ting ngui uish sheers

26-2 26 -255-00 00-2 -200 00-0 -005 05--A

Visu Vi sual al Ch Chec eckk of Fi Firre Ex Exti ting ngui uish sheer Bot ottl tlee Pr Pres essu surre Rea eadi ding ng

27-1 27 -144-00 00-7 -710 10-0 -001 01--A

Oper Op erat atiion onal al Te Test st of the Ail ileero ron n an and d Hy Hydr drau auli licc Ac Actu tuat atio ion n

27-2 27 -244-00 00-7 -710 10-0 -002 02-A -A

Oper Op erat atio iona nall Te Test st of th thee Ru Rudd dder er Se Serv rvoc ocon ontr trol olss wi with th In Indi divi vidu dual al Hy Hydr drau auli licc Sy Syst stem em

27-3 27 -344-00 00-7 -710 10-0 -001 01--A

Opeera Op rati tio ona nall Te Test st of th thee El Eleeva vattor an and d Hy Hydr drau auli licc Ac Actu tuat atiion

27-5 27 -544-00 00-2 -200 00-0 -001 01-A -A

Detail Deta iled ed Vi Visu sual al In Insp spec ecti tion on of th thee Tr Tran ansm smis issi sion on As Asse semb mbly ly (I (Inc nclu ludi ding ng Pa Part rt of th thee Transmission in Zone 140)

27-54-00-710-002-A

Operational Test of the Flap and Slat Systems

27-6 27 -644-00 00-7 -710 10-0 -001 01--A

Oper Op erat atiion onal al Te Test st of the Sp Spoi oile lerr Hy Hydr drau auli licc Ac Actu tuat atio ion n

27-8427-8 4-00 00-2 -200 00-0 -001 01--A 28-11-00-280-002-A 28-1 28 -111-00 00-6 -600 00-0 -008 08-A -A

Detail Deta iled ed Vi Visu sual al In Insp spec ecttio ion n of th thee Sl Slat at Tr Tran ansm smiiss ssiion Sy Syst steem Structural Fuel Tank Leaks - General In Infformation Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Mo Mode dera rate te Co Cont ntam amin inat atio ion n - Wi With th Fu Fuel el Mi Mixe xed d wi with th Biobor Biocide Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Mo Mode dera rate te Co Cont ntam amin inat atio ion n - Wi With th Fu Fuel el Mi Mixe xed d wi with th Kathon Biocide Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Mo Mode dera rate te Co Cont ntam amin inat atio ion n - Us Usin ing g Bi Biob obor or Bi Bioc ocid idee With a Metered Injection Rig Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Mo Mode dera rate te Co Cont ntam amin inat atio ion n - Us Usin ing g Kat Katho hon n Bi Bioc ocid idee With a Metered Injection Rig

28-1 28 -111-00 00-6 -600 00-0 -008 08-A -A-0 -011 28-1 28 -111-00 00-6 -600 00-0 -008 08-A -A-0 -022 28-1 28 -111-00 00-6 -600 00-0 -008 08-A -A-0 -033 28-1 28 -111-00 00-6 -600 00-0 -009 09-A -A 28-1 28 -111-00 00-6 -600 00-0 -009 09-A -A-0 -011 28-1 28 -111-00 00-6 -600 00-0 -009 09-A -A-0 -022 28-1 28 -111-00 00-6 -600 00-0 -009 09-A -A-0 -033

Biocid Bioc idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Biobor Biocide Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr Kathon Biocide Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr With a Metered Injection Rig Bioc Bi ocid idal al Sh Shoc ockk Tr Trea eatm tmen entt fo forr With a Metered Injection Rig

Heav He avyy Co Cont ntam amin inat atio ion n - Wi With th Fu Fuel el Mi Mixe xed d wi with th Heav He avyy Co Cont ntam amin inat atio ion n - Wi With th Fu Fuel el Mi Mixe xed d wi with th Heav He avyy Co Cont ntam amin inat atio ion n - Us Usin ing g Bi Biob obor or Bi Bioc ocid idee Heav He avyy Co Cont ntam amin inat atio ion n - Us Usin ing g Ka Kath thon on Bi Bioc ocid idee

28-2 28 -233-00 00-7 -720 20-0 -001 01--A

Opeera Op rati tio ona nall Te Test st of Cr Cros ossf sfee eed d Va Valv lvee Us Usiing In Indi divi vidu dual al Mot oto ors rs:: .. ....

28-24-00-710-002-A

Operat atiional Te Test st of the ENG 1(2) LP Fuel Val alvve

AES

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE 28-2 28 -299-00 00-7 -710 10-0 -001 01-A -A

29-10-00-200-001-A 29-1 29 -100-00 00-7 -710 10-0 -001 01-A -A

DESIGNATION Oper Op erat atio iona nall Te Test st of the the APU APU Lo Low w Pr Pres essu sure re Fu Fuel el Va Valv lvee usin using g each each in indi divi vidu dual al Motor in turn Check Flui uid d Level on Rese serrvoir Indicat ato ors Oper Op erat atio iona nall Ch Chec eckk of Hy Hydr drau auli licc Fi Fire re Sh Shut ut Of Offf Va Valv lves es an and d As Asso soci ciat ated ed In Indi dica cati ting ng System

30-1130-1 1-00 00-7 -710 10-0 -001 01--A 30-2 30 -211-00 00-7 -710 10-0 -001 01--A

Opera Ope rati tio ona nall Te Test st of th thee Wi Wing ng Ic Icee-Pr Prot oteect ctiion Sy Syst stem em Oper Op erat atiion onal al Te Test st of the Ant ntii Ic Icee Sy Syst stem em Fau aullt War arni ning ng

30-45-00-440-002-A

Reactivation of the Rain Repellent System

30-45-52-400-002-A 30-45-53-400-001-A 31-21-00-750-002-A 31-3 31 -333-55 55-4 -400 00-0 -002 02--A

Installation of the Wiper Arm Installation of the Wiper Blade Procedure to set the Clock Inst In stal alla lati tion on of th thee Di Digi gita tall Fli ligh ghtt Da Datta Rec ecor orde derr (DF DFDR DR))

32-11-00-200-001-A

Genera rall Visual Inspection of the Main Landing Gear

32-21-00-200-002-A 32-3 32 -311-00 00-7 -720 20-0 -002 02-A -A

Genera rall Visual Inspection of the Nose Lan and ding Gear Func Fu ncti tion onal al Te Test st of th thee No Norm rmal al Ex Exte tens nsio ion n an and d Re Retr trac acti tion on of th thee La Land ndin ing g Ge Gear ar

32-33-00-720-001-A 32-41-00-210-002-A

Functional Check of Free-Fal alll Extension Insspection/Check of the Wheels and Tires In

32-41-00-210-003-A

Insspection/Check of the Ti In Tirre Pressur uree

32-41-11-000-006-A 32-41-11-400-006-A 32-41-12-000-001-A 32-41-12-400-001-A 32-42-00-710-001-A

Removal of the MLG Wheel Installation of the MLG Wheel Removal of the NLG Wheel Installation of the NLG Wheel Opeerationa Op nall Check of the Normal Braking System

32-43-00-710-001-A

Ope perrational Check of Alternate Brak akiing System

** On A/C POST SB 32-1235 FOR A/C 003-008 32-48-51-400-005-A 32-5 32 -511-00 00-7 -720 20-0 -003 03--A

Installation of the Fan Assy Func Fu ncti tion onal al Te Test st of th thee No Nose se Wh Wheeel Ste teeeri ring ng wit ith h th thee Ha Hand ndw whe heel el

32-5132-5 1-00 00-7 -720 20-0 -004 04--A 33-5 33 -511-38 38-4 -400 00-0 -002 02--A 34-10-00-170-001-A

Functi Func tion onal al Te Test st of th thee No Nose se Wh Wheeel Ste teeeri ring ng wit ith h th thee Pe Peda dalls Inst In stal alllat atio ion n of th thee Ba Batt tteery of th thee Em Emer erge genc ncyy Po Powe werr-Su Supp pply ly Uni nitt Flushing of the Principal Total Pressur uree Lines

34-10-00-170-002-A 34-1 34 -100-00 00-1 -170 70-0 -003 03--A 35-10-00-200-001-A

Flushing of the Principal Static Pressure Lines Drai Dr aini ning ng an and d Fl Flus ushi hing ng of St Stan andb dbyy Pn Pneu eum mat atiic Ci Circ rcui uitts Insspection of Oxygen Press In ssu ure for the Flight Crew

35-1 35 -122-41 41-7 -710 10-0 -001 01--A

Oper Op erat atiion onal al Te Test st of th thee Fu Full ll Fa Face ce/Q /Qui uick ck Do Donn nnin ing g Ox Oxyg ygeen Mas asks ks

35-30-00-210-004-A 36-11-00-710-003-A

Check Pressure on Portable Oxygen Cylinders Gage Ope perrational Test of the Bleed Air System

38-1338-1 3-00 00-7 -710 10-0 -001 01--A 38-31-00-710-009-A

Operat Oper atio iona nall Test Test of the Qu Quan anti tity ty In Indi dica cati ting ng Sy Syst steem Operational Test of the Toilet Unit

38-32-00-710-002-A

Ope perrational Te Test st of the Waste/Water Drain Syst steem

** On A/C 006-099 49-11-11-400-003-A

AES

Insstallation of the Power Plan In antt (APU) (APS 3200)

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL REFERENCE ** On A/C 003-005

DESIGNATION

49-11-11-400-004-A

Installation of the Power Plant (APU) (131-9(A))

** On A/C 006-099 49-20-00-600-002-A


** On A/C 003-005 49-20-00-600-003-A


51-74-11-300-001-A

Repair of Corroded Areas

53-59-00-210-001-A

Operational Check of Single Drain Pipe Aft of FR70 from Outside

54-50-00-200-001-A

General Visual Inspection of Compartment A and F Pylon Drain System

71-00-00-550-011-A 71-00-00-710-012-B 71-00-00-710-018-A 71-00-00-710-043-A 71-00-00-710-047-A

Depreservation of the Power Plant Test No.3 : Idle Leak Check Discontinued Start, Restart and Shutdown Procedures Normal Engine Automatic Start Procedure Normal Engine Manual Start Procedure

71-00-20-400-040-A 71-00-20-400-040-A-01

Installation of the Power Plant Installation of the Power Plant with the Engine Positioner TWW 75E (MIAG)

3.


4.



(2)




AES

Do a visual inspection of the aircraft for impacts by foreign objects, bird nests, fluid leakages (hydraulic fluid, fuel), missing parts, blockage and corrosion of: (a)

the upper and the lower surfaces of the wing

(b)

the nacelles and the pylons

(c)

the external surfaces of the fuselage

(d)

the flight control surfaces

(e)

the leading and the trailing edges of the horizontal and vertical stabilizers

(f)

the . . .

(g)

the external handle of the passenger/crew doors

external skin of: the passenger/crew doors the cargo doors the frame around the doors.

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL (h)

the drains 1

In the lower fuselage (Ref. TASK 53-59-00-210-001-A)

2

On the pylons (Ref. TASK 54-50-00-200-001-A)

3


(i)

the toilet areas

(j)

all steel parts for corrosion.

(2)

If you find corrosion, remove it (Ref. TASK 51-74-11-300-001-A).

(3)

Make sure that: . the communication and navigation antennas are correctly installed . the static dischargers are correctly installed and in correct condition (Ref. TASK 23-61-00-200-001A).

(4)

Do a check of the avionics compartment.

Subtask 10-30-00-615-051-A B.


Remove all the STORAGE PRESERVATION (Material No: 15-002) and adhesive tapes.

(2)

We recommend that you clean the aircraft externally (Ref. TASK 12-21-11-615-002-A).

Subtask 10-30-00-420-067-A C.


Install and connect the batteries 2PB1 and 2PB2 and make sure that the charge is correct (Ref. TASK 24-38-51-400-001-A).

(2)


(3)

On the overhead panel 25 VU, on the CABIN PRESS section: . release the DITCHING pushbutton switch to open the avionics ventilation skin valves and the outflow valve. NOTE :


Subtask 10-30-00-554-053-A D.

Removal of the Protection (1)

Remove all the protective equipment from the engines, the APU and the probes (Ref. TASK 10-11-00-555-014-A).

(2)

Remove the protection from the cockpit, the passenger seats and the carpets.

Subtask 10-30-00-710-118-A E.

Inspection of the Doors (1)

Make sure that the doors open and close correctly.

Subtask 10-30-00-420-068-A F.

AES

Installation of the Equipment Removed (1)

Install the Digital Flight Data Recorder (if removed) (Ref. TASK 31-33-55-400-002-A).

(2)

Install the Cockpit Voice Recorder (if removed) (Ref. TASK 23-71-35-400-001-A).

10-30-00 PB601



Install the debris guard, the impeller and the shroud of the brake fans (If installed) ** On A/C POST SB 32-1235 FOR A/C 003-008 (Ref. TASK 32-48-51-400-005-A).

(4)

Install the fire-extinguisher bottles and cartridges if removed of: . the FWD cargo compartment (if installed) ** On A/C 005-099 (Ref. TASK 26-23-41-400-004-A) . the AFT cargo compartment (if installed) (Ref. AMM 26-23-42-400-001) . the engines ** On A/C ALL (Ref. TASK 26-21-41-400-001-A) . the APU (Ref. TASK 26-22-41-400-001-A).

(5)

Install the batteries of: . the EPSU if removed (Ref. TASK 33-51-38-400-002-A) . the flashlights if removed and make sure that they operate correctly . the megaphones if removed and make sure that they operate correctly.

(6)

Fixed automatic Emergency Locator Transmitter (ELT) (if installed) (a)

(7)

Make sure that the automatic ELT is installed: 1

Get access to the ceiling panel 261BC (Ref. TASK 25-23-42-000-002-A).

2

If the ELT was removed from the aircraft during the storage period: . Install the automatic ELT (Ref. TASK 25-65-35-400-001-A).

3

If the ELT was not removed from the aircraft during the storage period: . Close the ceiling panel 261BC (Ref. TASK 25-23-42-400-002-A).

(b)

In the cockpit, on the overhead panel, on the Remote Control Panel (RCP) (111MX): . Set the ELT switch to TEST/RESET.

(c)

Do the BITE test (Ref. TASK 25-65-00-740-001-A).

Portable survival Emergency Locator Transmitter (ELT) (if installed) (a)

(b)

If the portable ELT has a programming dongle: 1

Install the portable ELT (if removed during the storage period): (Ref. AMM 25-65-32-400-001) .

2

Do the BITE test (Ref. AMM 25-65-00-740-002) .

If the portable ELT does not have a programming dongle: 1

Make sure that the portable ELT is in the correct position on its bracket.

2

Make sure that the toggle switch is set to the OFF or to the ARMED position. NOTE :

AES

Refer to the customer’s operational procedures for the correct position of the toggle switch.

(8)

Install the wiper blades (Ref. TASK 30-45-53-400-001-A) and the wiper arms (Ref. TASK 30-45-52-400-002-A), if removed.

(9)

Do the reactivation of the rain repellent system (Ref. TASK 30-45-00-440-002-A).

10-30-00 PB601





(2)


(3)


Subtask 10-30-00-710-120-B H.

Inspection and Test of Fire Protection (1)

(2)

(3)

Engine fire protection (a)

Do a test of the engine fire-extinguishing system (Ref. TASK 26-12-00-710-001-A).

(b)

Do a check of the engine extinguishing distribution-piping (Ref. TASK 26-21-00-720-003-C) or (Ref. TASK 26-21-00-720-003-C-01).

(c)

Do a check of the engine low-pressure indicating (Ref. TASK 26-21-00-710-002-A).

APU fire protection (a)

Do a test of the APU fire-extinguishing system (Ref. TASK 26-22-00-710-001-A).

(b)

Do a check of the APU extinguishing distribution-piping (Ref. TASK 26-22-00-210-001-A).

(c)

Do a check of the APU low-pressure indicating (Ref. TASK 26-22-00-710-003-A).

Cargo-Compartment fire protection (a)

Do a test of the cargo-compartment fire-extinguishing system and low pressure indicating ** On A/C 005-099 (Ref. TASK 26-23-00-710-001-A).

(b)

(4)

Do a check of the cargo-compartment extinguishing distribution-piping: . for cargo-compartment with one bottle: (Ref. TASK 26-23-00-200-001-A). . for cargo-compartment with two bottles: (Ref. AMM 26-23-00-200-003) .

Lavatory fire protection (a)

Do a check of the fire extinguisher bottle pressure ** On A/C ALL (Ref. TASK 26-25-00-200-005-A).

(5)

Portable fire-extinguishing (a)

Do a check of all the portable fire-extinguishing bottles (Ref. TASK 26-24-00-210-001-A).

Subtask 10-30-00-710-121-A J.

Inspection and Test of the Oxygen System (1)

(2)

Crew oxygen cylinders (a)

Open very slowly the crew oxygen cylinder/valves 3 to 4 turns and do a check of the crew oxygen pressure (Ref. TASK 35-10-00-200-001-A).

(b)

Do a test of the full-face masks (Ref. TASK 35-12-41-710-001-A).

Portable oxygen cylinders (a)

AES

Do a check of the pressure of all portable oxygen cylinders (Ref. TASK 35-30-00-210-004-A).

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL Subtask 10-30-00-710-132-A K.

Inspection and Test of the Water/Waste Systems (1)

Do a test of the potable-water distribution system (Ref. TASK 38-13-00-710-001-A).

(2)

Do a test of the waste/water drain system (Ref. TASK 38-32-00-710-002-A).

(3)

Do a test of the toilet system (Ref. TASK 38-31-00-710-009-A).

Subtask 10-30-00-710-122-A L.



(2)

If you find contamination, do a shock treatment:

(3)

(a)

For a moderate contamination: (Ref. TASK 28-11-00-600-008-A) or (Ref. TASK 28-11-00-600-008-A-01) or (Ref. TASK 28-11-00-600-008-A-02) or (Ref. TASK 28-11-00-600-008-A-03).

(b)

For a heavy contamination: (Ref. TASK 28-11-00-600-009-A) or (Ref. TASK 28-11-00-600-009A-01) or (Ref. TASK 28-11-00-600-009-A-02) or (Ref. TASK 28-11-00-600-009-A-03).

Drain water from all the fuel tanks (Ref. TASK 12-32-28-281-001-A). NOTE :


(4)

Do a check of all the fuel tanks for leakage (Ref. TASK 28-11-00-280-002-A).

(5)

Do a test of the engine LP fuel shut-off valve (Ref. TASK 28-24-00-710-002-A).

(6)

Do a test of the APU shut-off valve (Ref. TASK 28-29-00-710-001-A).

(7)

Do a test of the crossfeed valves (Ref. TASK 28-23-00-720-001-A).

Subtask 10-30-00-710-123-A M.

Inspection and Test of the Hydraulic System (1)

Do an analysis of the hydraulic fluid (Ref. TASK 12-32-29-281-001-A).

(2)

Do a check of the fluid level in the hydraulic reservoirs (Ref. TASK 29-10-00-200-001-A).

(3)

Do a test of the hydraulic shut-off valves (Ref. TASK 29-10-00-710-001-A).

Subtask 10-30-00-710-124-A N.

Inspection and Test of the Landing Gears (1)

Do a general visual inspection of the nose landing gear (Ref. TASK 32-21-00-200-002-A).

(2)

Do an inspection of the main landing gear (Ref. TASK 32-11-00-200-001-A).

(3)

Lubricate all the landing gears: . lubrication of the NLG (Ref. TASK 12-22-32-640-002-A) . lubrication of the MLG (Ref. TASK 12-22-32-640-001-A).

(4)

Do a check of the shock-absorber charge pressure of the NLG (Ref. TASK 12-14-32-614-004-A).

(5)

Do a check of the shock-absorber charge pressure of the MLG (Ref. TASK 12-14-32-614-003-A).

(6)

Clean all the actuator rods and apply a thin layer of HYDRAULIC FLUIDS (Material No: 02-003) or HYDRAULIC FLUIDS (Material No: 02-008) . NOTE :

AES

It is necessary to use the same hydraulic fluid as the fluid used to fill the landing-gear hydraulic system.

10-30-00 PB601



Do a test of: . the extension and retraction of the landing gear (Ref. TASK 32-31-00-720-002-A) . the free-fall extension (Ref. TASK 32-33-00-720-001-A).

(8)

Do a test of: . the nose wheel steering with the handwheel (Ref. TASK 32-51-00-720-003-A) . the nose wheel steering with the rudder pedals (Ref. TASK 32-51-00-720-004-A).

Subtask 10-30-00-710-125-A P.

Inspection and Operational Test of the Wheels and the Brakes (1)

(2)

(3)

If the aircraft was in storage with unserviceable tires: (a)

Remove all the unserviceable tires: . for the nose landing gear (Ref. TASK 32-41-12-000-001-A) . for the main landing gear (Ref. TASK 32-41-11-000-006-A).

(b)

Install serviceable tires on the nose landing gear (Ref. TASK 32-41-12-400-001-A).

(c)

Install serviceable tires on the main landing gear (Ref. TASK 32-41-11-400-006-A).

(d)


(e)

If necessary, inflate the tires (Ref. TASK 12-14-32-614-001-A).

If the aircraft was in storage with serviceable tires: (a)

Remove all the wheels and send them to the overhaul shop for inspection of the bearings: . for the nose landing gear (Ref. TASK 32-41-12-000-001-A) . for the main landing gear (Ref. TASK 32-41-11-000-006-A).

(b)

Install the nose landing gear wheels (Ref. TASK 32-41-12-400-001-A).

(c)

Install the main landing gear wheels (Ref. TASK 32-41-11-400-006-A).

(d)

Put the tires back to the nominal pressure (Ref. TASK 12-14-32-614-001-A).

(e)

Make sure that there are no cracks in the tires (Ref. TASK 32-41-00-210-002-A).

Do a test of: . the normal braking system (Ref. TASK 32-42-00-710-001-A) . the alternate braking system (Ref. TASK 32-43-00-710-001-A).

Subtask 10-30-00-710-126-A Q.

AES

Inspection and Test of the APU (1)

Install the APU, if removed: . for the GTCP 36-300 APU: (Ref. AMM 49-11-11-400-001) . for the APS 32000 APU: ** On A/C 006-099 (Ref. TASK 49-11-11-400-003-A) . for the 131-9(A) APU: ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-11-11-400-004-A)

(2)

Do the APU depreservation: . for the GTCP 36-300 APU: (Ref. AMM 49-20-00-600-001) . for the APS 32000 APU: ** On A/C 006-099 (Ref. TASK 49-20-00-600-002-A) . for the 131-9(A) APU:

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL ** On A/C 003-005 EMB SB 49-1082 FOR A/C 003-005 (Ref. TASK 49-20-00-600-003-A) ** On A/C ALL Subtask 10-30-00-710-119-A R.

Inspection and Test of the Ventilation System (1)

Discard the recirculation filters (Ref. TASK 21-21-41-920-002-A).

(2)

Do a test of the ventilation system of the avionics compartment (Ref. TASK 21-26-00-710-001-A) or (Ref. TASK 21-26-00-710-001-A-01).

(3)

If the aft cargo-compartment ventilation system is installed, do a test of the aft cargo-compartment ventilation system (Ref. TASK 21-28-00-720-004-A).

(4)

If the FWD cargo-compartment ventilation system is installed, do a test of the FWD cargocompartment ventilation system (Ref. AMM 21-28-00-720-003) .

Subtask 10-30-00-710-127-B S.

Inspection and Test of the Engine (1)

Install the engine if removed (Ref. TASK 71-00-20-400-040-A) or (Ref. TASK 71-00-20-400-040-A-01).

(2)

Do the engine depreservation if it is not removed (Ref. TASK 71-00-00-550-011-A).

(3)

Do the depreservation of the IDG (Ref. TASK 24-21-00-600-040-A)

(4)

Change the oil of the pneumatic starter (Ref. TASK 12-13-80-600-011-B) or (Ref. TASK 12-13-80-600-011-B).

(5)

Start the engines, make them turn for one minute (Ref. TASK 71-00-00-710-043-A) or (Ref. TASK 71-00-00-710-047-A).

(6)

Do an engine run-up for the two engines (Ref. TASK 71-00-00-710-012-B) or (Ref. TASK 71-00-00-710-012-B).

(7)


(8)

After shutdown, do a check of the engines for oil, hydraulic and fuel leakage.

Subtask 10-30-00-710-133-A T.

Test of the Bleed System (1)

Do a test of the bleed system (Ref. TASK 36-11-00-710-003-A).

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 47-31-34-740-001) .

** On A/C 003-004 Subtask 10-30-00-710-128-A V.


AES

Do the lubrication of: . the mechanical control chains of the THS (Ref. TASK 12-22-27-640-007-A) . the THS-actuator ball-screw nut (Ref. TASK 12-22-27-640-003-A) . the rudder bearings No. 6 (Ref. TASK 12-22-55-640-001-A) or (Ref. TASK 12-22-55-640-002-A). . the trimmable-horizontal-stabilizer bearings and attachment fittings (Ref. TASK 12-22-53-640-001A) or (Ref. TASK 12-22-53-640-002-A).

10-30-00 PB601


@A318/A319/A320/A321 AIRCRAFT MAINTENANCE MANUAL . . . (2)

the roller bearings of the flap tracks (Ref. TASK 12-22-27-640-004-A) the roller and the pinion bearings of the slat tracks (Ref. TASK 12-22-27-640-006-A) all the spoiler servo-control bearings (Ref. TASK 12-22-27-640-005-A).

Cleaning and protection 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: . the avionics compartment, . the FWD and AFT cargo compartments, . between FR71 and the THS actuator and the rear rudder mechanical-control. NOTE :

1

Be careful of cable areas hidden by pulley guard or pulley guide.

If there is corrosion on the cables or if there is no protection with SPECIAL MATERIALS (Material No: 05-005) or COMMON GREASES (Material No: 04-004) , clean and put protection along the full length of the cables (Ref. TASK 20-24-11-100-001-A).

(3)

Do a detailed inspection of the flap transmission assembly (Ref. TASK 27-54-00-200-001-A).

(4)

Do a detailed inspection of the slat transmission system (Ref. TASK 27-84-00-200-001-A).

(5)

Apply grease to the flap rotary actuators (Ref. TASK 12-22-27-640-008-A).

(6)

Do a check of the fluid level of the flap power-control-unit. If necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-002-A).

(7)

Do a check of the fluid level of the slat power-control-unit. If necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-003-A).

(8)

Do a test of the spoiler hydraulic control (Ref. TASK 27-64-00-710-001-A).

(9)

Do a test of the aileron and its hydraulic control (Ref. TASK 27-14-00-710-001-A).

(10) Do a test of the elevator and its hydraulic control (Ref. TASK 27-34-00-710-001-A). (11) Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-002-A). (12) Do a test of the flap and slat system (Ref. TASK 27-54-00-710-002-A). Operate the flap system a minimum of ten times. ** On A/C 005-099 Subtask 10-30-00-710-128-B V.


Do the lubrication of: . the mechanical control chains of the THS (Ref. TASK 12-22-27-640-007-A) . the THS-actuator ball-screw nut (Ref. TASK 12-22-27-640-003-A) . the rudder bearings No. 6 (Ref. TASK 12-22-55-640-001-A) or (Ref. TASK 12-22-55-640-002-A). . the trimmable-horizontal-stabilizer bearings and attachment fittings (Ref. TASK 12-22-53-640-001A) or (Ref. TASK 12-22-53-640-002-A). . the roller bearings of the flap tracks (Ref. TASK 12-22-27-640-004-A) . the roller and the pinion bearings of the slat tracks (Ref. TASK 12-22-27-640-006-A) . all the spoiler servo-control bearings (Ref. TASK 12-22-27-640-005-A).

(2)

Cleaning and protection of the flight control cables (a)

AES

If the aircraft storage period is less than 6 months, it is not necessary to do a check of the rudder and THS cables.

10-30-00 PB601



If the aircraft storage period is more than 6 months, do a check of the rudder and THS cables in these areas: . the avionics compartment, . the FWD and AFT cargo compartments, . between FR71 and the THS actuator and the rear rudder mechanical-control. NOTE :

1

Be careful of cable areas hidden by pulley guard or pulley guide.

If there is corrosion on the cables or if there is no protection with SPECIAL MATERIALS (Material No: 05-005) or COMMON GREASES (Material No: 04-004) , clean and put protection along the full length of the cables (Ref. TASK 20-24-11-100-001-A).

(3)

Do a detailed inspection of the flap transmission assembly (Ref. TASK 27-54-00-200-001-A).

(4)

Do a detailed inspection of the slat transmission system (Ref. TASK 27-84-00-200-001-A).

(5)

Drain and fill the flap rotary actuators (Ref. TASK 12-13-27-612-005-A).

(6)

Do a check of the fluid level of the flap power-control-unit. If necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-002-A).

(7)

Do a check of the fluid level of the slat power-control-unit. If necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-003-A).

(8)

Do a test of the spoiler hydraulic control (Ref. TASK 27-64-00-710-001-A).

(9)

Do a test of the aileron and its hydraulic control (Ref. TASK 27-14-00-710-001-A).

(10) Do a test of the elevator and its hydraulic control (Ref. TASK 27-34-00-710-001-A). (11) Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-002-A). (12) Do a test of the flap and slat system (Ref. TASK 27-54-00-710-002-A). Operate the flap system a minimum of ten times. ** On A/C ALL Subtask 10-30-00-710-129-A W.

Tests of the Ice Protection Systems (1)

Do a test of the wing ice-protection system (Ref. TASK 30-11-00-710-001-A).

(2)

Do a test of the ice protection system of the air intakes (Ref. TASK 30-21-00-710-001-A).

Subtask 10-30-00-750-050-A X.

Set of the Clock (1)

5.

Set the clock (Ref. TASK 31-21-00-750-002-A).




(2)

Remove the warning notice(s).

Subtask 10-30-00-410-057-A B.

Close Access (1)

AES

Make sure that the work area is clean and clear of tools and other items.

10-30-00 PB601


CHAPTER_10.pdf

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