nammwzza_000008

HIGHLIGHTS __________

REVISION NO. 11 Aug 01/09

Pages which have been revised are outlined below, together with the Highlights of theRevision

--------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES--------------------------------------------------------------------------------------

CHAPTER 10__________

L.E.P. 1- 2 REVISED TO REFLECT THIS REVISION INDICATING NEW,REVISED, AND/OR DELETED PAGES10-20-00 MOD.23007P2622 INCORPORATED ALL 201- 220 LANDING GEAR - NLG - NOSE WHEELS AXLE - DELETE WEIGHT AND BALANCE SYSTEM PROVISIONS AND IMPROVE AXLE STIFFNESS MOD.23748J1090 INCORPORATED ALL LANDING GEAR - MLG - DELETE WEIGHT AND BALANCE LUGS ON MLG AXLE CORRECTION/ADDITION/AMPLIFICATION ALL REVISED PROCEDURE. LAYOUT IMPROVED/MATERIAL RELOCATED ALL WARNING/NOTE/REASON FOR THE JOB AMENDED ALL

10-HIGHLIGHTS of 1 REVISION NO. 11 Aug 01/09

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CHAPTER 10 __________

PARKING, MOORING, STORAGE & RETURN TO SERVIC

LIST OF EFFECTIVE PAGES _______________________ N, R or D indicates pages which are New, Revised or Deleted respectively Remove and insert the affected pages and complete the Record of Revisions and the Record of Temporary Revisions as necessary

CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE

RECORD 10-11-00 231 Feb01/08 10-12-00 216 May01/09OF TEMP. 10-11-00 232 May01/07 10-12-00 217 May01/09REVISION 10-11-00 233 Feb01/08 10-12-00 218 May01/09 10-11-00 234 Aug01/08 10-12-00 219 May01/09L.E.P. R 1- 2 Aug01/09 10-11-00 235 Aug01/08 10-12-00 220 May01/09T. of C. 1 Aug01/08 10-11-00 236 Aug01/08 10-12-00 221 Nov01/08T. of C. 2 Nov01/08 10-11-00 237 Aug01/08 10-12-00 222 Nov01/08 10-11-00 238 Aug01/08 10-12-00 223 Nov01/0810-00-00 1 Nov01/06 10-11-00 239 Aug01/08 10-12-00 224 May01/09 10-11-00 240 Aug01/08 10-12-00 225 Nov01/0810-10-00 1 Nov01/06 10-11-00 241 Aug01/08 10-12-00 226 Nov01/08 10-11-00 242 Aug01/08 10-12-00 227 May01/0910-11-00 201 Nov01/06 10-11-00 243 Aug01/08 10-12-00 228 Nov01/0810-11-00 202 May01/07 10-11-00 244 Aug01/08 10-12-00 229 May01/0910-11-00 203 Aug01/08 10-11-00 245 Aug01/08 10-12-00 230 May01/0910-11-00 204 Aug01/08 10-11-00 246 Aug01/08 10-12-00 231 May01/0910-11-00 205 May01/09 10-11-00 247 Aug01/08 10-12-00 232 May01/0910-11-00 206 May01/09 10-11-00 601 Feb01/07 10-12-00 233 May01/0910-11-00 207 Aug01/08 10-11-00 602 May01/08 10-12-00 234 May01/0910-11-00 208 Aug01/08 10-11-00 603 Aug01/08 10-12-00 235 Nov01/0810-11-00 209 Aug01/08 10-11-00 604 Feb01/09 10-12-00 236 May01/0710-11-00 210 Aug01/08 10-11-00 605 Feb01/09 10-12-00 237 Feb01/0810-11-00 211 Aug01/08 10-11-00 606 Feb01/09 10-12-00 238 Feb01/0810-11-00 212 Aug01/08 10-11-00 607 Feb01/09 10-12-00 601 Feb01/0710-11-00 213 May01/09 10-11-00 608 Feb01/09 10-12-00 602 Aug01/0810-11-00 214 May01/09 10-11-00 609 Aug01/08 10-12-00 603 Aug01/0810-11-00 215 May01/09 10-12-00 604 Aug01/0810-11-00 216 Aug01/08 10-12-00 201 May01/07 10-12-00 605 Aug01/0810-11-00 217 Aug01/08 10-12-00 202 Nov01/06 10-12-00 606 Aug01/0810-11-00 218 Aug01/08 10-12-00 203 May01/09 10-12-00 607 Aug01/0810-11-00 219 Aug01/08 10-12-00 204 May01/09 10-12-00 608 Aug01/0810-11-00 220 Aug01/08 10-12-00 205 May01/09 10-12-00 609 Aug01/0810-11-00 221 Feb01/08 10-12-00 206 May01/09 10-12-00 610 May01/0910-11-00 222 Feb01/08 10-12-00 207 May01/09 10-12-00 611 Nov01/0610-11-00 223 Nov01/06 10-12-00 208 May01/09 10-12-00 612 Nov01/0610-11-00 224 Nov01/06 10-12-00 209 Nov01/08 10-12-00 613 Nov01/0610-11-00 225 May01/09 10-12-00 210 Nov01/08 10-12-00 614 Nov01/0610-11-00 226 Feb01/08 10-12-00 211 May01/09 10-12-00 615 Nov01/0610-11-00 227 Nov01/06 10-12-00 212 May01/09 10-12-00 616 Nov01/0610-11-00 228 Nov01/06 10-12-00 213 May01/09 10-12-00 617 Nov01/0610-11-00 229 Nov01/06 10-12-00 214 May01/0910-11-00 230 Nov01/06 10-12-00 215 May01/09 10-20-00 R 201 Aug01/09

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CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE

10-20-00 R 202 Aug01/0910-20-00 R 203 Aug01/0910-20-00 R 204 Aug01/0910-20-00 R 205 Aug01/0910-20-00 R 206 Aug01/0910-20-00 R 207 Aug01/0910-20-00 R 208 Aug01/0910-20-00 R 209 Aug01/0910-20-00 R 210 Aug01/0910-20-00 R 211 Aug01/0910-20-00 R 212 Aug01/0910-20-00 R 213 Aug01/0910-20-00 N 214 Aug01/0910-20-00 N 215 Aug01/0910-20-00 N 216 Aug01/0910-20-00 N 217 Aug01/0910-20-00 N 218 Aug01/0910-20-00 N 219 Aug01/0910-20-00 N 220 Aug01/09

10-30-00 601 Feb01/0910-30-00 602 Feb01/0910-30-00 603 Feb01/0910-30-00 604 Feb01/0910-30-00 605 Feb01/0910-30-00 606 Feb01/0910-30-00 607 Feb01/0910-30-00 608 Feb01/0910-30-00 609 Feb01/0910-30-00 610 Feb01/0910-30-00 611 Feb01/0910-30-00 612 Feb01/0910-30-00 613 Feb01/0910-30-00 614 Feb01/0910-30-00 615 Feb01/0910-30-00 616 Feb01/0910-30-00 617 Feb01/09

10-L.E.P. Page 2 Aug 01/09

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CHAPTER 10 __________

PARKING, MOORING, STORAGE & RETURN TO SERVICE

TABLE OF CONTENTS _________________

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ___________ PARKING, MOORING, STORAGE & RETURN TO 10-00-00 _____________________________________ SERVICE - GENERAL _________________ DESCRIPTION AND OPERATION 1 ALL General 1 ALL

PARKING/STORAGE 10-10-00 _______________ DESCRIPTION AND OPERATION 1 ALL General 1 ALL

PARKING 10-11-00 MAINTENANCE PRACTICES 201 ALL Parking procedures 201 ALL Parking Procedure in Flight-ready 203 ALL Condition (Parking of not more than 15 Days) Parking Procedure in Flight-ready 210 ALL Condition (Parking of not more than 12 Weeks) Return to Operation after Parking 221 ALL not more than 15 Days Return to Operation after Parking 225 ALL not more than 12 Weeks Renewal of 15-Day Parking Period 229 ALL Renewal of 12-Week Parking Period 231 ALL Installation of the Aircraft 233 ALL Protection Equipment Removal of the Aircraft Protection 241 ALL Equipment Procedure for the Installation of 244 ALL Wheel Chocks on Aircraft

PARKING 10-11-00 INSPECTION/CHECK 601 ALL Periodic Ground Check at 7-day 601 ALL Intervals Periodic Ground Check at 15-day 603 ALL Intervals Periodic Ground Check at 1-month 609 ALL Intervals

STORAGE 10-12-00 MAINTENANCE PRACTICES 201 ALL Storage Procedures 201 ALL Storage Procedure (Storage Not 203 ALL More than 6 Months)

10-CONTENTS Page 1 Aug 01/08R WZZ

CHAPTER 10 __________

PARKING, MOORING, STORAGE & RETURN TO SERVICE

TABLE OF CONTENTS _________________

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ___________ Storage Procedure (Storage Not 218 ALL More than 2 Years) Renewal for 6 Months Storage 235 ALL Period Renewal for 2 Years Storage Period 238 ALL

STORAGE 10-12-00 INSPECTION/CHECK 601 ALL Periodic Ground Check at 7-day 601 ALL Intervals Periodic Ground Check at 15-day 603 ALL Intervals Periodic Ground-Check at 1-month 606 ALL Interval Periodic ground-check at 3-month 610 ALL interval Periodic Ground Check at 6-month 617 ALL Intervals

MOORING 10-20-00 _______ MAINTENANCE PRACTICES 201 ALL Mooring of the Aircraft 201 ALL

RETURN TO SERVICE 10-30-00 _________________ INSPECTION/CHECK 601 ALL Return to Operation after Storage 601 ALL Period

10-CONTENTS Page 2 Nov 01/08R WZZ

PARKING, MOORING, STORAGE & RETURN TO SERVICE - GENERAL _______________________________________________________ DESCRIPTION AND OPERATION _________________________

1. General _______ This chapter covers: - Parking/Storage (Ref. ATA 10-10), - Mooring (Ref. ATA 10-20), - Return to Service (Ref. ATA 10-30).

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PARKING/STORAGE - DESCRIPTION AND OPERATION ___________________________________________

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).


PARKING - MAINTENANCE PRACTICES _______________________________

TASK 10-11-00-555-006

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 DESIGNATION -------------------------------------------------------------------------------

10-11-00-200-002 Periodic Ground Check at 7-day Intervals 10-11-00-200-003 Periodic Ground Check at 15-day Intervals 10-11-00-200-004 Periodic Ground Check at 1-month Intervals 10-11-00-554-003 Return to Operation after Parking not more than 15 Days 10-11-00-554-004 Return to Operation after Parking not more than 12 Weeks 10-11-00-555-007 Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days) 10-11-00-555-008 Parking Procedure in Flight-ready Condition (Parking of not more than 12 Weeks) 10-11-00-555-011 Renewal of 15-Day Parking Period 10-11-00-555-012 Renewal of 12-Week Parking Period

3. Job Set-up __________

Subtask 10-11-00-860-083

A. Not Applicable


4. Procedure _________

Subtask 10-11-00-555-073

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

(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).

(b) Return to operation after parking period of not more than 15 days (Ref. TASK 10-11-00-554-003).

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

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

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

(b) Return to operation after parking period of not more than 12 weeks (Ref. TASK 10-11-00-554-004).

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

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TASK 10-11-00-555-007

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

CAUTION : MAKE SURE THAT YOU OBEY THE MAINTENANCE PROGRAM FOR STORED/ PARKED _______ AIRCRAFT. DO NOT CHANGE OR STOP THE MAINTENANCE PROGRAM WITHOUT APPROVAL FROM YOUR LOCAL AUTHORITIES.

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).


This procedure gives the preservation steps for a parking period of not more than 15 days.

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.


A. Fixtures, Tools, Test and Support Equipment

------------------------------------------------------------------------------- REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------

R No specific AR CHOCK - WHEEL 25-01-000 1 SUN SCREEN,SET-COCKPIT

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B. Referenced Information


05-57-00-200-001 Aircraft Stability 10-11-00-200-002 Periodic Ground Check at 7-day Intervals 10-11-00-554-003 Return to Operation after Parking not more than 15 Days 10-11-00-555-011 Renewal of 15-Day Parking Period 10-11-00-555-013 Installation of the Aircraft Protection EquipmentR 10-11-00-555-015 Procedure for the Installation of Wheel Chocks onR Aircraft 10-20-00-556-001 Mooring of the Aircraft 12-11-28-650-003 Pressure Refuel with Automatic Control 12-11-28-650-004 Pressure Refuel with Manual Control 12-16-38-613-001 Servicing of the Toilet System 12-21-11-615-002 External Cleaning 12-21-12-100-002 Cleaning of the Cockpit Equipment/Furnishings 12-21-12-100-003 Cleaning of the Carpets and Non-Textile Floor Covering (NTF) 12-21-12-100-004 Cleaning of the Plastic Surfaces and Mirrors 12-21-12-100-005 Cleaning of the Seat Covers and the Curtains 12-21-12-100-006 Cleaning of the Light Alloy and Steel Components 12-21-12-100-007 Cleaning of the Cargo Compartments 12-21-12-100-008 Cleaning of the Cabin Monitors and Display Screens (if installed) 12-21-12-100-009 Cleaning of the Plastic Wash Basin in the Lavatories 12-24-38-680-001 Draining of the Potable Water System (with Electrical Power) 12-31-21-660-001 Cold Weather Maintenance - Air Conditioning 12-31-24-660-001 Cold Weather Maintenance - Electrical Power 12-31-25-660-001 Cold Weather Maintenance - Equipment/Furnishings 12-31-27-660-001 Cold Weather Maintenance - Flight Controls 12-31-28-660-001 Cold Weather Maintenance - Fuel 12-31-31-660-001 Cold Weather Maintenance - Indicating/Recording systems and Navigation 12-31-32-660-001 Cold Weather Maintenance - Landing Gear 12-31-35-660-001 Cold Weather Maintenance - Oxygen System 12-31-38-660-001 Cold Weather Maintenance - Water/Waste 12-31-49-660-001 Cold Weather Maintenance - Auxiliary Power Unit 12-31-51-660-001 Cold Weather Maintenance - Structure 12-31-52-660-001 Cold Weather Maintenance - Doors 12-31-71-660-001 Cold Weather Maintenance - Power Plant 12-32-28-281-001 Drain Water Content 12-34-24-869-002 Aircraft Grounding for the Maintenance Operations



24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 52-10-00-410-001 Closing of the Passenger/Crew Door

3. Job Set-up __________

Subtask 10-11-00-860-072

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

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

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

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Subtask 10-11-00-615-053

B. Cleaning of the Aircraft

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

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

Subtask 10-11-00-941-054

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).

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

R (4) Make sure that the THS pitch-trim control wheel is set to two degreesR aircraft nose up.

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

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

Subtask 10-11-00-650-058

D. Aircraft Configuration

(1) Energize the electrical circuits (Ref. TASK 24-41-00-861-002).

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



Subtask 10-11-00-281-059

A. Protection of the Fuel System

(1) Drain water from all the fuel tanks (Ref. TASK 12-32-28-281-001).

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

Subtask 10-11-00-680-055

B. 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)

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

(2) Toilet system

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

Subtask 10-11-00-620-060

C. 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 10-11-00-555-065

D. 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).

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Subtask 10-11-00-860-073

E. 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 24-38-51-000-001).

NOTE : If the batteries stay connected during parking, it is ____ necessary to do a check of the batteries 2PB1 and 2BP2 pushbutton switches on OFF position.

(3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862- 002).

5. Close-up ________

Subtask 10-11-00-942-055

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).

Subtask 10-11-00-555-066

B. 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).

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


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


TASK 10-11-00-555-008

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




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

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.




R No specific AR CHOCK - WHEEL 25-01-000 1 SUN SCREEN,SET-COCKPIT

B. Consumable Materials


Material No. 05-043 VARNISH P.T.F.E SPRAY (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)


C. Referenced Information


05-57-00-200-001 Aircraft Stability 10-11-00-200-002 Periodic Ground Check at 7-day Intervals 10-11-00-200-003 Periodic Ground Check at 15-day Intervals 10-11-00-200-004 Periodic Ground Check at 1-month Intervals 10-11-00-554-004 Return to Operation after Parking not more than 12 Weeks 10-11-00-555-012 Renewal of 12-Week Parking Period 10-11-00-555-013 Installation of the Aircraft Protection EquipmentR 10-11-00-555-015 Procedure for the Installation of Wheel Chocks onR Aircraft 10-20-00-556-001 Mooring of the Aircraft 12-11-28-650-003 Pressure Refuel with Automatic Control 12-11-28-650-004 Pressure Refuel with Manual Control 12-16-38-613-001 Servicing of the Toilet System 12-21-11-615-002 External Cleaning 12-21-12-100-002 Cleaning of the Cockpit Equipment/Furnishings 12-21-12-100-003 Cleaning of the Carpets and Non-Textile Floor Covering (NTF) 12-21-12-100-004 Cleaning of the Plastic Surfaces and Mirrors 12-21-12-100-005 Cleaning of the Seat Covers and the Curtains 12-21-12-100-006 Cleaning of the Light Alloy and Steel Components 12-21-12-100-007 Cleaning of the Cargo Compartments 12-21-12-100-008 Cleaning of the Cabin Monitors and Display Screens (if installed) 12-21-12-100-009 Cleaning of the Plastic Wash Basin in the Lavatories 12-22-52-640-002 Lubrication of the FWD and AFT Cargo-Compartment Doors 12-22-52-640-006 Lubrication of the External Control Handles of the FWD and AFT Passenger/Crew Doors 12-22-52-640-008 Lubrication of the Avionics Compartment-Door Handles 12-22-52-640-009 Lubrication of the FWD and AFT Cargo-Compartment Door Handle 12-22-52-640-014 Lubrication of Safety Pin Guide Fitting and Door Arming/Disarming Mechanism 12-22-52-640-016 Lubrication of the Hinge-Arm Support-Fitting Bearings 12-24-38-680-001 Draining of the Potable Water System (with Electrical Power) 12-31-21-660-001 Cold Weather Maintenance - Air Conditioning 12-31-24-660-001 Cold Weather Maintenance - Electrical Power 12-31-25-660-001 Cold Weather Maintenance - Equipment/Furnishings 12-31-27-660-001 Cold Weather Maintenance - Flight Controls



12-31-28-660-001 Cold Weather Maintenance - Fuel 12-31-31-660-001 Cold Weather Maintenance - Indicating/Recording systems and Navigation 12-31-32-660-001 Cold Weather Maintenance - Landing Gear 12-31-35-660-001 Cold Weather Maintenance - Oxygen System 12-31-38-660-001 Cold Weather Maintenance - Water/Waste 12-31-49-660-001 Cold Weather Maintenance - Auxiliary Power Unit 12-31-51-660-001 Cold Weather Maintenance - Structure 12-31-52-660-001 Cold Weather Maintenance - Doors 12-31-71-660-001 Cold Weather Maintenance - Power Plant 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination AnalysisR 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS) 49-00-00-860-003 APU Start by Batteries (GTCP 36-300) 49-00-00-860-004 APU Shutdown by Batteries (GTCP 36-300) 49-00-00-860-005 APU Start by Batteries (APS 3200) 49-00-00-860-006 APU Shutdown by Batteries (APS 3200) 49-00-00-860-008 APU Start by Batteries (131-9(A)) 49-00-00-860-009 APU Shutdown by Batteries (131-9(A))



52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 71-00-00-710-018 Discontinued Start, Restart and Shutdown Procedures 71-00-00-710-043 Normal Engine Automatic Start Procedure 78-31-00-710-041 Operational Test of the Thrust Reverser System with the CFDS

3. Job Set-up __________

Subtask 10-11-00-860-074

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) - moor the aircraft (Ref. TASK 10-20-00-556-001) 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), (Ref. TASK 12-31-24-660-001), (Ref. TASK 12-31-25-660-001), (Ref. TASK 12-31-27-660-001), (Ref. TASK 12-31-28-660-001), (Ref. TASK 12-31-31-660-001), (Ref. TASK 12-31-32-660-001), (Ref. TASK 12-31-35-660-001), (Ref. TASK 12-31-38-660-001), (Ref. TASK 12-31-49-660-001), (Ref. TASK 12-31-51-660-001), (Ref. TASK 12-31-52-660-001), (Ref. TASK 12-31-71-660-001).



Subtask 10-11-00-615-054



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

Subtask 10-11-00-941-055







Subtask 10-11-00-650-059



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

�� EFF : ALL � 4�� 10-11-00 � � May 01/09 � � � � WZZ


Subtask 10-11-00-281-060

A. Protection of the fuel system

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

(2) Do a preventive treatment:

(a) If premixed fuel is available: - refuel the wing tanks to 30% of the total capacity with fuelR premixed with kathon biocide (Ref. TASK 28-11-00-600-010) orR biobor biocide (Ref. TASK 28-11-00-600-010). - Refuel the center tank to 30% of the total capacity with fuelR premixed with Kathon Biocide (Ref. TASK 28-11-00-600-010) orR Biobor Biocide (Ref. TASK 28-11-00-600-010).

(b) If premixed fuel is not available: - Refuel the wing tanks to 30% of the total capacity with fuelR not premixed with kathon biocide (Ref. TASK 28-11-00-600-010)R or biobor biocide (Ref. TASK 28-11-00-600-010). - Refuel the center tank to 30% of the total capacity with noR fuel premixed with kathon biocide (Ref. TASK 28-11-00-600-010)R or biobor biocide (Ref. TASK 28-11-00-600-010).

(3) Drain water from all the fuel tanks (Ref. TASK 12-32-28-281-001)


(4) Close all the fuel system valves.

Subtask 10-11-00-710-056

B. Protection of the APU

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.

(1) Start the APU and operate it for at least 5 minutes at no load governed speed: - for a GTCP 36-300 APU: (Ref. TASK 49-00-00-860-003) - for an APS 3200 APU: (Ref. TASK 49-00-00-860-005) - for a 131-9(A) APU: (Ref. TASK 49-00-00-860-008)


(2) After protection of the engines, stop the APU: - for a GTCP 36-300 APU: (Ref. TASK 49-00-00-860-004) - for an APS 3200 APU: (Ref. TASK 49-00-00-860-006) - for a 131-9(A) APU: (Ref. TASK 49-00-00-860-009)

Subtask 10-11-00-710-057

C. Protection of the Engines

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.

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

(2) Do a thrust reverser full cycle (Ref. TASK 78-31-00-710-041).

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

Subtask 10-11-00-680-056

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).

(2) 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).

Subtask 10-11-00-170-055

E. Flushing of the Air Data System

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

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


(3) Drain and flush the standby static and standby total pressure lines of the Air Data Module (Ref. TASK 34-22-25-170-001).

Subtask 10-11-00-620-061

F. Protection of the Windows


(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 10-11-00-620-062

G. 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.

Subtask 10-11-00-620-063

H. Protection of the Doors

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

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

(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).

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

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

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

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


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

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

Subtask 10-11-00-555-067

J. Installation of the Protection Equipment

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

Subtask 10-11-00-860-075

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


5. Close-up ________

Subtask 10-11-00-942-056

A. Close-up.



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


(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.


Subtask 10-11-00-555-068

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

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

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


INTENTIONALLY BLANK

��R � � Page 220�� 10-11-00 � � Aug 01/08 � � � � WZZ

TASK 10-11-00-554-003

Return to Operation after Parking not more than 15 Days


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




No specific warning notice No specific 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE



R 10-11-00-555-014 Removal of the Aircraft Protection Equipment 12-14-32-614-003 Check Charge Pressure of Main Landing Gear Shock Absorber 12-14-32-614-004 Check NLG Shock Absorber Charge Pressure 12-21-11-615-002 External Cleaning 12-32-28-281-001 Drain Water Content 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-41-00-210-003 Inspection/Check of the Pressure of Tires 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS)

�� EFF : ALL � Page 221�� 10-11-00 � � Feb 01/08 � � � � WZZ

3. Job Set-up __________

Subtask 10-11-00-615-055

A. Safety Precautions

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

(2) Put a warning notice in position in the cockpit to tell persons not to operate the systems while you prepare the aircraft for operation again.


Subtask 10-11-00-860-076

A. Aircraft Configuration

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

R (a) 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

B. Removal of the Protection Equipment

R (1) Remove all the protection equipment from the engines, the APU and theR probes (Ref. TASK 10-11-00-555-014).


Subtask 10-11-00-860-077

C. Aircraft Maintenance Configuration

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

(2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

(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 10-11-00-281-061

D. Protection of the Fuel System


Subtask 10-11-00-210-065

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) - for the MLG (Ref. TASK 12-14-32-614-003)

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

Subtask 10-11-00-170-056

F. Flushing of the Air Data System

NOTE : Flush the Air Data System only if the parking period is more than ____ 7 days.





5. Close-up ________

Subtask 10-11-00-942-057

A. Close-up

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

(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.


TASK 10-11-00-554-004

Return to Operation after Parking not more than 12 Weeks


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




No specific warning notice No specific 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE



10-11-00-555-014 Removal of the Aircraft Protection Equipment 12-14-32-614-003 Check Charge Pressure of Main Landing Gear Shock Absorber 12-14-32-614-004 Check NLG Shock Absorber Charge Pressure 12-21-11-615-002 External Cleaning 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External PowerR 28-11-00-280-002 Structural Fuel Tank Leaks - General Information 29-10-00-200-001 Check Fluid Level on Reservoir Indicators 32-41-00-210-002 Inspection/Check of the Wheels and Tires 32-41-00-210-003 Inspection/Check of the Pressure of Tires 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS) 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump


3. Job Set-up __________

Subtask 10-11-00-615-051



(2) Put a warning notice in position in the cockpit to tell persons not to operate the systems while you prepare the aircraft for operation again.


Subtask 10-11-00-941-051

A. Aircraft Configuration


R (a) 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

B. Removal of the Protection Equipment

R (1) Remove all the protection equipment from the engines, the APU and theR probes (Ref. TASK 10-11-00-555-014).


Subtask 10-11-00-860-066

C. Aircraft Maintenance Configuration

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

(2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

(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 10-11-00-680-053

D. Protection of the fuel system




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

Subtask 10-11-00-210-062

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) - for the MLG (Ref. TASK 12-14-32-614-003)


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

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


Subtask 10-11-00-170-054

F. Flushing of the Air Data System

NOTE : Flush the Air Data System only if the parking period is more than ____ 7 Days




Subtask 10-11-00-010-055

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) and (Ref. TASK 52-10-00-410-001) - the FWD and AFT cargo compartments (Ref. TASK 52-30-00-860-002) and (Ref. TASK 52-30-00-860-002)

5. Close-up ________

Subtask 10-11-00-860-067

A. Close-up


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



TASK 10-11-00-555-011

Renewal of 15-Day Parking Period




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




10-11-00-200-002 Periodic Ground Check at 7-day Intervals 10-11-00-200-003 Periodic Ground Check at 15-day Intervals 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis

3. Job Set-up __________

Subtask 10-11-00-860-078

A. Not Applicable



Subtask 10-11-00-210-066

A. Protection of the fuel system

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






TASK 10-11-00-555-012

Renewal of 12-Week Parking Period

CAUTION : YOU MUST CONTINUE TO DO THE SCHEDULED MAINTENANCE DURING THE PARKING _______ PERIOD.


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




10-11-00-554-004 Return to Operation after Parking not more than 12 Weeks 10-11-00-555-008 Parking Procedure in Flight-ready Condition (Parking of not more than 12 Weeks)R 10-11-00-555-013 Installation of the Aircraft Protection Equipment 32-33-00-720-001 Functional Check of Free-Fall Extension

3. Job Set-up __________

Subtask 10-11-00-860-065

A. Not Applicable


Subtask 10-11-00-210-061

A. 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).

Subtask 10-11-00-555-060

B. Procedure

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


Subtask 10-11-00-555-061

C. Parking Period

(1) The new parking period for 12 weeks starts from the end of this last flight.

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

5. Close-up ________

Subtask 10-11-00-555-062

A. 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).

R (2) Do the 12-week parking procedure (Ref. TASK 10-11-00-555-008)



TASK 10-11-00-555-013

R Installation of the Aircraft Protection Equipment

R WARNING : DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS, SENSORS (STATIC, _______R PITOT, TAT, AOA). USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OFR THE AIRCRAFT. THE SPECIFIED TOOLS:R - GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT,R - ARE EASY TO SEE FROM THE GROUND,R - ARE EASY TO REMOVE.R IF YOU USE TAPE, THERE IS A RISK THAT SOME TAPE, OR ADHESIVE FROM THER TAPE, WILL STAY ON THE PROBES, DUCTS OR SENSORS. THIS CAN CAUSER 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.


Self Explanatory




No specific 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE No specific 1 WARNING NOTICER IAE1N20008 2 COVER-COMMON NOZZLE IAE1N20400 2 COVER-INLET COWLR 98A10001005000 3 COVER-PITOT PROBER 98A10001013000 2 COVER-SLIP-ON,TOTAL TEMPERATURE SENSORR 98A10001500000 3 COVER-SLIP ON,ANGLE OF ATTACK SENSOR 98D10003001000 2 COVER-INLET COWL ENGINER 98D10003003000 3 COVER-SLIP-ON,AOAR 98D10007512000 1 COVER-EXHAUST DUCT,APUR 98D10007513000 1 COVER-OILCOOLER OUTLET,APU 98D10103500001 6 COVER-STATIC PROBE




R 10-11-00-991-001 Fig. 201R 10-11-00-991-004 Fig. 202R 10-11-00-991-007 Fig. 203R 10-11-00-991-006 Fig. 204R

3. Job Set-up __________

Subtask 10-11-00-941-056


R (1) On the panel 115VU:RR - Make sure that the ENG/MODE selector switch is in the NORMR position.RR - Make sure that the ENG/MASTER 1(2) control lever is in the OFFR position.

R (2) On the panel 25VU:R - make sure that the PROBE/WINDOW HEAT pushbutton switch is releasedR (the ON legend is off).

(3) Put a WARNING NOTICE 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.

R (5) Before installation of protection devices, make sure that the probes,R the engines and the APU are cool.



Subtask 10-11-00-555-069

A. Installation of the Protection Devices on the FuselageR (Ref. Fig. 201/TASK 10-11-00-991-001)

(1) Protection of the 2 total temperature sensors - Put the COVER-SLIP-ON,TOTAL TEMPERATURE 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-SLIP-ON,AOA (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. Installation of the Protection Devices on the EnginesR (Ref. Fig. 202/TASK 10-11-00-991-004, 203/TASK 10-11-00-991-007)

(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.

Subtask 10-11-00-555-071

C. Installation of the Protection Devices on the APU AreaR (Ref. Fig. 204/TASK 10-11-00-991-006)

(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.


Protective EquipmentR Figure 201/TASK 10-11-00-991-001


5. Close-up ________

Subtask 10-11-00-942-058

A. Close-up



TASK 10-11-00-555-014

Removal of the Aircraft Protection Equipment


Self Explanatory




No specific 1 ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE



R 10-11-00-991-001 Fig. 201R 10-11-00-991-004 Fig. 202R 10-11-00-991-007 Fig. 203R 10-11-00-991-006 Fig. 204R

3. Job Set-up __________

Subtask 10-11-00-941-057


(1) 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 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.



Subtask 10-11-00-555-075

A. Removal of the Protection Devices from the FuselageR (Ref. Fig. 201/TASK 10-11-00-991-001)

(1) Protection of the 2 total temperature sensors - Remove the COVER-SLIP-ON,TOTAL TEMPERATURE 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 (98D10003003000).

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

Subtask 10-11-00-555-076

B. Removal of the Protection Devices from the EnginesR (Ref. Fig. 202/TASK 10-11-00-991-004, 203/TASK 10-11-00-991-007)

(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

C. Removal of the Protection Devices from the APU AreaR (Ref. Fig. 204/TASK 10-11-00-991-006)

(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).


5. Close-up ________

Subtask 10-11-00-942-059

A. Close-up



R TASK 10-11-00-555-015

R Procedure for the Installation of Wheel Chocks on Aircraft

R 1. Reason for the Job __________________

R This task gives general recommendations about the location of wheel chocksR for different aircraft conditions.

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

R 2. Job Set-up Information ______________________

R A. Fixtures, Tools, Test and Support Equipment

R -------------------------------------------------------------------------------R REFERENCE QTY DESIGNATIONR -------------------------------------------------------------------------------

R No specific AR CHOCK - WHEEL

R B. Referenced Information

R -------------------------------------------------------------------------------R REFERENCE DESIGNATIONR -------------------------------------------------------------------------------

R 10-11-00-991-010 Fig. 205

R 3. Job Set-up __________

R Subtask 10-11-00-941-058

R A. Wheel Chock Specifications

R (1) Use CHOCK - WHEEL that agree with SAE AIR4905 standard.


R 4. Procedure _________

R Subtask 10-11-00-555-078

R A. Location of Wheel ChocksR (Ref. Fig. 205/TASK 10-11-00-991-010)

R (1) Aircraft in flight-ready condition

R (a) Put the CHOCK - WHEEL in front of and behind the outboard wheelR of the right and left MLG.

R (b) There must be a small distance between the tires and the CHOCK -R WHEEL.

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

R NOTE : If you put CHOCK - WHEEL at the NLG because of the local ____R regulations, make sure that they do not touch the tires.

R (c) If the aircraft is parked on a slope, also put CHOCK - WHEEL onR the down-slope side of the inboard wheel of each MLG. Make sureR that the down-slope chocks touch the wheels and that the up-slopeR chocks do not touch the wheels.

R NOTE : On slippery surfaces, we recommend to use more CHOCK - ____R WHEEL and to apply the parking brake.

R (2) Aircraft in flight-ready condition with wind speed more than 25 Kts

R (a) Put the CHOCK - WHEEL behind and in front of the NLG and MLGR wheels.



R (c) If the aircraft is parked on a slope, put the CHOCK - WHEELR against the tires of the down-slope wheels.

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


R Location of Wheel ChocksR Figure 205/TASK 10-11-00-991-010


R (3) Aircraft in parking or storage condition

R (a) Put the CHOCK - WHEEL behind and in front of the NLG and MLGR wheels.



R (c) If the aircraft is parked on a slope, put the CHOCK - WHEELR against the tires of the down-slope wheels.

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


PARKING - INSPECTION/CHECK __________________________

TASK 10-11-00-200-002

Periodic Ground Check at 7-day Intervals


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).




29-10-00-200-001 Check Fluid Level on Reservoir Indicators 32-41-00-210-003 Inspection/Check of the Pressure of Tires

R 3. Job Set-up __________

R Subtask 10-11-00-020-067

R A. Not Applicable


Subtask 10-11-00-210-063

A. Inspection


(a) Make sure that the protective equipments are correctly installed.

(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 contamination that is not usual.

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



R 5. Close-up ________

R Subtask 10-11-00-555-074

R A. Not Applicable


TASK 10-11-00-200-003



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).




10-11-00-555-013 Installation of the Aircraft Protection EquipmentR 10-11-00-555-015 Procedure for the Installation of Wheel Chocks onR AircraftR 12-32-28-281-001 Drain Water Content 12-33-21-618-001 Pre-conditioning with the APU 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-50-00-866-008 Extension of the Flaps/Slats on the Ground 27-92-41-710-001 Operational Test of the Side Stick Assembly 29-10-00-200-001 Check Fluid Level on Reservoir Indicators 30-11-00-710-001 Operational Test of the Wing Ice-Protection System 30-21-00-710-002 Operational Test of the Engine Air Intake Ice Protection (with the Engines in operation) 32-41-00-210-002 Inspection/Check of the Wheels and Tires 32-41-00-210-003 Inspection/Check of the Pressure of Tires 32-42-00-710-001 Operational Check of the Normal Braking System 32-43-00-710-001 Operational Check of Alternate Braking System 32-48-00-720-001 Functional Test of the Brake Fans 32-51-00-720-003 Functional Test of the Nose Wheel Steering with the Handwheel 32-51-00-720-004 Functional Test of the Nose Wheel Steering with the Pedals 36-11-00-710-003 Operational Test of the Bleed Air System 49-00-00-860-003 APU Start by Batteries (GTCP 36-300)



49-00-00-860-004 APU Shutdown by Batteries (GTCP 36-300) 49-00-00-860-005 APU Start by Batteries (APS 3200) 49-00-00-860-006 APU Shutdown by Batteries (APS 3200) 49-00-00-860-008 APU Start by Batteries (131-9(A)) 49-00-00-860-009 APU Shutdown by Batteries (131-9(A)) 71-00-00-710-018 Discontinued Start, Restart and Shutdown Procedures 71-00-00-710-043 Normal Engine Automatic Start Procedure 78-31-00-710-041 Operational Test of the Thrust Reverser System with the CFDS

3. Job Set-up __________

Subtask 10-11-00-020-066

A. Removal of Protections

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

Subtask 10-11-00-860-079

B. Aircraft Configuration

R (1) Install and connect the batteries 2PB1 and 2PB2 and make sure thatR the charge is correct (Ref. TASK 24-38-51-400-001).

R (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

R (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 : Make sure that the avionics ventilation continues to operate ____ correctly.

R



Subtask 10-11-00-210-067

A. Inspection

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


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


Subtask 10-11-00-700-052

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) (Ref. TASK 32-51-00-720-004).

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

R (3) Do the test of the brake fans (if installed) (Ref. TASK 32-48-00-720-R 001).R

Subtask 10-11-00-700-055

R C. Test of the APU, Engines and Systems

R (1) Start the APU:R - for a GTCP 36-300 APU: (Ref. TASK 49-00-00-860-003)R - for an APS 3200 APU: (Ref. TASK 49-00-00-860-005)R - for a 131-9(A) APU: (Ref. TASK 49-00-00-860-008)

R (2) Operate the air conditioning system (Ref. TASK 12-33-21-618-001)

R (3) Start the engines and let them become stable at ground idleR (Ref. TASK 71-00-00-710-043).


R (4) Stop the APU:R - for a GTCP 36-300 APU: (Ref. TASK 49-00-00-860-004)R - for an APS 3200 APU: (Ref. TASK 49-00-00-860-006)R - for a 131-9(A) APU: (Ref. TASK 49-00-00-860-009)

R (5) Do a thrust reverser full cycle (Ref. TASK 78-31-00-710-041).

R (6) Do the test of the bleed air system (Ref. TASK 36-11-00-710-003) andR make sure that the related BLEED PRESS and BLEED TEMP indications areR satisfactory.

R (7) Do the test of the wing ice-protection system (Ref. TASK 30-11-00-R 710-001).

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

R (8) Do the test of the engine air intake ice-protection (Ref. TASK 30-21-R 00-710-002).

R (9) Stop the engines (Ref. TASK 71-00-00-710-018).R

Subtask 10-11-00-866-054

R 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 0⁰ to FULL and back to extend and retract the slats and the flaps (Ref. TASK 27- 50-00-866-008).

(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).

(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 27-92-41-710-001).

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

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Subtask 10-11-00-281-062

R E. Inspection of the Fuel System


(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

R F. Movement of the Aircraft

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

(1) Remove the wheel chocks that you installed during the parking procedure.

NOTE : 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)

Subtask 10-11-00-860-081

R G. Aircraft Configuration

(1) 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).



5. Close-up ________

Subtask 10-11-00-555-072

A. 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).

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TASK 10-11-00-200-004

Periodic Ground Check at 1-month Intervals


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).




R 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis

3. Job Set-up __________

Subtask 10-11-00-860-082

A. Not Applicable


Subtask 10-11-00-281-063

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

R (4) Close all the fuel system valves.


STORAGE - MAINTENANCE PRACTICES _______________________________

TASK 10-12-00-553-005

Storage Procedures


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




10-12-00-200-006 Periodic Ground Check at 7-day Intervals 10-12-00-200-007 Periodic Ground Check at 15-day IntervalsR 10-12-00-200-008 Periodic Ground-Check at 1-month Interval 10-12-00-200-009 Periodic ground-check at 3-month interval 10-12-00-200-010 Periodic Ground Check at 6-month Intervals 10-12-00-553-006 Storage Procedure (Storage Not More than 6 Months) 10-12-00-553-007 Storage Procedure (Storage Not More than 2 Years) 10-12-00-553-008 Renewal for 6 Months Storage Period 10-12-00-553-009 Renewal for 2 Years Storage Period 10-30-00-554-005 Return to Operation after Storage Period

3. Job Set-up __________

Subtask 10-12-00-860-058

A. Not Applicable



Subtask 10-12-00-553-068

A. Procedure to store the aircraft with related procedures to do perodic ground checks, return to operation and renew the storage procedure

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

(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) - at 15-day intervals (Ref. TASK 10-12-00-200-007) - at 1-month interval (Ref. TASK 10-12-00-200-008) - at 3-month intervals (Ref. TASK 10-12-00-200-009).

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

(c) 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).

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

(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). - at 15-day intervals (Ref. TASK 10-12-00-200-007). - at 1-month interval (Ref. TASK 10-12-00-200-008). - at 3-month intervals (Ref. TASK 10-12-00-200-009). - at 6-month intervals (Ref. TASK 10-12-00-200-010).

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

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


TASK 10-12-00-553-006

Storage Procedure (Storage Not More than 6 Months)




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




No specific blanking caps No specific talcum No specific AR CHOCK - WHEEL No specific 1 WARNING NOTICE



Material No. 02-003 F NSA 307110 TYPE 4 NO LONGER AVAILABLE (Ref. 20-31-00) Material No. 03-001 USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00)R Material No. 04-001 F DCSEA 359/A WHEEL BEARING MINERAL GREASE (Ref. 20-31-00) Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)



R Material No. 04-011 USA SAE-AMS-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00) Material No. 05-005 USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) Material No. 05-027 RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) Material No. 05-043 VARNISH P.T.F.E SPRAY (Ref. 20-31-00)R Material No. 08-052 USA AMS-T-23397 AND/OR L-T-80BR SELF ADHESIVEALUMINIUM TAPE (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)



05-57-00-200-001 Aircraft Stability 10-11-00-555-013 Installation of the Aircraft Protection Equipment 10-11-00-555-015 Procedure for the Installation of Wheel Chocks on Aircraft 10-20-00-556-001 Mooring of the Aircraft 12-16-38-613-001 Servicing of the Toilet System 12-21-11-615-002 External Cleaning 12-21-12-100-002 Cleaning of the Cockpit Equipment/Furnishings 12-21-12-100-003 Cleaning of the Carpets and Non-Textile Floor Covering (NTF) 12-21-12-100-004 Cleaning of the Plastic Surfaces and Mirrors 12-21-12-100-005 Cleaning of the Seat Covers and the Curtains 12-21-12-100-006 Cleaning of the Light Alloy and Steel Components 12-21-12-100-007 Cleaning of the Cargo Compartments 12-21-12-100-008 Cleaning of the Cabin Monitors and Display Screens (if installed) 12-21-12-100-009 Cleaning of the Plastic Wash Basin in the Lavatories 12-22-27-640-003 Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut 12-22-27-640-004 Lubricate all Carriage Rollers on all Flap Tracks 12-22-27-640-005 Lubrication of Spoiler No.1 to 5 Servo Control Bearings



12-22-27-640-006 Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth 12-22-27-640-007 Lubrication of the THS Mechanical Control Chains 12-22-32-640-001 Lubrication of the MLG and Doors 12-22-32-640-002 Lubrication of the NLG and Doors 12-22-52-640-002 Lubrication of the FWD and AFT Cargo-Compartment Doors 12-22-52-640-006 Lubrication of the External Control Handles of the FWD and AFT Passenger/Crew Doors 12-22-52-640-008 Lubrication of the Avionics Compartment-Door Handles 12-22-52-640-009 Lubrication of the FWD and AFT Cargo-Compartment Door Handle 12-22-52-640-014 Lubrication of Safety Pin Guide Fitting and Door Arming/Disarming Mechanism 12-22-52-640-016 Lubrication of the Hinge-Arm Support-Fitting Bearings 12-22-53-640-001 Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004 12-22-55-640-001 Lubrication of Rudder Hinge Bearing No. 6 with Grease Mat. No. 04-004 12-24-38-680-001 Draining of the Potable Water System (with Electrical Power) 12-31-21-660-001 Cold Weather Maintenance - Air Conditioning 12-31-24-660-001 Cold Weather Maintenance - Electrical Power 12-31-25-660-001 Cold Weather Maintenance - Equipment/Furnishings 12-31-27-660-001 Cold Weather Maintenance - Flight Controls 12-31-28-660-001 Cold Weather Maintenance - Fuel 12-31-31-660-001 Cold Weather Maintenance - Indicating/Recording systems and Navigation 12-31-32-660-001 Cold Weather Maintenance - Landing Gear 12-31-35-660-001 Cold Weather Maintenance - Oxygen System 12-31-38-660-001 Cold Weather Maintenance - Water/Waste 12-31-49-660-001 Cold Weather Maintenance - Auxiliary Power Unit 12-31-51-660-001 Cold Weather Maintenance - Structure 12-31-52-660-001 Cold Weather Maintenance - Doors 12-31-71-660-001 Cold Weather Maintenance - Power Plant 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 12-34-24-869-002 Aircraft Grounding for the Maintenance Operations 23-71-35-000-001 Removal of the Cockpit Voice Recorder (CVR) 1RK 24-21-00-600-040 Preservation/Storage/Return to Service of the IDG 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2)



24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 26-21-41-000-004 Removal of the Cartridge of the Engine Fire-Extinguisher Bottle 26-22-41-000-001 Removal of the Fire Extinguisher Bottle (11WF) 26-23-41-000-004 Removal of the Cargo Fire-Extinguisher Bottle (4005WX) 27-54-00-710-002 Operational Test of the Flap and Slat Systems 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 30-45-00-040-002 Deactivation of the Rain Repellent System 31-33-55-000-001 Removal of the Digital Flight Data Recorder (DFDR) 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-40-00-200-001 Inspection/Check of the Wheels & Brakes 32-41-00-210-003 Inspection/Check of the Pressure of Tires



32-41-11-400-006 Installation of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-41-12-400-001 Installation of the NLG Wheel (2659GM,2660GM) 32-48-51-000-005 Removal of the Fan Assy (7GS,8GS,9GS,10GS) 33-51-38-000-002 Removal of the Battery of the Emergency Power-Supply Unit 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS) 49-20-00-200-001 Inspection/Check of the Engine (4005KM) (GTCP 36-300) 49-20-00-210-001 APU Power Plant Visual Inspection (APS 3200) 49-20-00-600-001 Preservation / Storage / De-preservation of the Engine (GTCP 36-300) 49-20-00-600-002 Preservation/Storage/Return to Service of APU (APS 3200) 49-20-00-600-003 Preservation/Storage/Return to Service of APU (131-9(A)) 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 53-59-00-210-001 Operational Check of Single Drain Pipe Aft of FR70 from Outside 54-50-00-200-001 General Visual Inspection of the Pylon Drain System 71-00-00-550-010 Preservation of the Power Plant

3. Job Set-up __________

Subtask 10-12-00-860-059

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

(b) If aircraft storage is in cold weather conditions: - do the cold weather maintenance procedures: (Ref. TASK 12-31-21-660-001), (Ref. TASK 12-31-24-660-001), (Ref. TASK 12-31-25-660-001), (Ref. TASK 12-31-27-660-001), (Ref. TASK 12-31-28-660-001), (Ref. TASK 12-31-31-660-001),


(Ref. TASK 12-31-32-660-001), (Ref. TASK 12-31-35-660-001), (Ref. TASK 12-31-38-660-001), (Ref. TASK 12-31-49-660-001), (Ref. TASK 12-31-51-660-001), (Ref. TASK 12-31-52-660-001), (Ref. TASK 12-31-71-660-001).


Subtask 10-12-00-615-054



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

Subtask 10-12-00-941-051








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


Subtask 10-12-00-650-053



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


Subtask 10-12-00-010-058

A. Get Access

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

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

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


Subtask 10-12-00-170-053

B. Flushing of the Air Data System




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Subtask 10-12-00-620-073

C. Protection of the Landing Gears and the Wheels

(1) Protection of the landing gears

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

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

(c) Apply talcum 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) - main landing gear (Ref. TASK 12-22-32-640-001).

(e) Clean all the actuator rods and apply a thin layer of HYDRAULIC FLUIDS (Material No. 02-003).

(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 used tires or wheels with used tires: - on the nose landing gear (Ref. TASK 32-41-12-400-001) - on the main landing gear (Ref. TASK 32-41-11-400-006).

(b) Lubricate the bearings with COMMON GREASE (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).

(d) Remove the debris guard, the impeller and the shroud of the brake fans (Ref. TASK 32-48-51-000-005) (If installed). - Apply SPECIAL MATERIALS (Material No. 05-027) on the removed parts.


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

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

Subtask 10-12-00-550-052


(1) Protection of the potable water system

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

(2) Protection of the toilet system

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

Subtask 10-12-00-281-053

E. Protection of the fuel system



(a) If premixed fuel is available: - Refuel the wing tanks to 30% of the total capacity with fuelR premixed with kathon biocide (Ref. TASK 28-11-00-600-010) orR biobor biocide (Ref. TASK 28-11-00-600-010). - Refuel the center tank to 30% of the total capacity with fuelR premixed with kathon biocide (Ref. TASK 28-11-00-600-010) orR biobor biocide (Ref. TASK 28-11-00-600-010).

(b) If premixed fuel is not available: - Refuel the wing tanks to 30% of the total capacity with fuelR not premixed with kathon biocide (Ref. TASK 28-11-00-600-010)R or biobor biocide (Ref. TASK 28-11-00-600-010). - Refuel the center tank to 30% of the total capacity with fuelR not premixed with kathon biocide (Ref. TASK 28-11-00-600-010)R or biobor biocide (Ref. TASK 28-11-00-600-010).





Subtask 10-12-00-620-074

F. Protection of the Flight Controls

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

Subtask 10-12-00-620-075

G. Protection of the Engines

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

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

Subtask 10-12-00-620-076

H. Protection of the APU

(1) Do an inspection of the APU for preservation: - for a GTCP 36-300 APU: (Ref. TASK 49-20-00-200-001) - for an APS 3200 APU: (Ref. TASK 49-20-00-210-001)

(2) Do the preservation of the APU: - for a GTCP 36-300 APU: (Ref. TASK 49-20-00-600-001) - for an APS 3200 APU: (Ref. TASK 49-20-00-600-002) - for a 131-9(A) APU: (Ref. TASK 49-20-00-600-003)


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

Subtask 10-12-00-210-069

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).

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

(c) On the engines.

(d) In all other locations.

Subtask 10-12-00-620-077

K. External Protection of the Aircraft

R (1) With STORAGE PRESERVATION (Material No. 15-002) and BONDING ANDR 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 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 outletR (trim and wing tanks) with fine nylon netting and BONDING ANDR 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

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.


R (5) Give external protection to the cockpit windows with STORAGER PRESERVATION (Material No. 15-002) and BONDING AND ADHESIVE COMPOUNDSR (Material No. 08-052) (or equivalent). Do not put BONDING ANDR ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent) on theR windows.

Subtask 10-12-00-620-079

M. Protection of the Doors


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




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



Subtask 10-12-00-620-080

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

P. Protection of the Rain Protection System

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

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

Subtask 10-12-00-020-061

Q. Removal of Equipment

(1) Remove the Digital Flight Data Recorder 1TU (Ref. TASK 31-33-55-000- 001).

(2) Remove the Cockpit Voice Recorder 1RK (Ref. TASK 23-71-35-000-001).

(3) Remove: - all the EPSU batteries (Ref. TASK 33-51-38-000-002) - the emergency locator beacon.

(4) If the external temperature is more than 70 DEG.C (158.00 DEG.F), remove: - the cargo fire-extinguishing bottles and cartridges (Ref. TASK 26- 23-41-000-004). - the engine fire-extinguishing bottles and cartridges (Ref. TASK 26- 21-41-000-004). - the APU extinguishing-bottle and cartridge (Ref. TASK 26-22-41-000- 001).


(5) Put blanking caps on the disconnected electrical connectors.

Subtask 10-12-00-555-056

R. Installation of the Protection Equipment

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

R (2) Keep all external protection equipment flags in position with BONDINGR AND ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent).

Subtask 10-12-00-860-060

S. Aircraft Maintenance Configuration



5. Close-up ________

Subtask 10-12-00-942-056

A. Close-up




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

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

R (6) Seal with STORAGE PRESERVATION (Material No. 15-002) and BONDING ANDR ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent) all theR openings that give access to: - the passenger compartment, - the cockpit,


- the cargo compartment, - the APU, - the engines, - the landing gears.

R (7) Seal with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-052) (orR 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), (Ref. TASK 29-24-00-864-001), (Ref. TASK 29-10-00-864-003).



(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.


TASK 10-12-00-553-007

Storage Procedure (Storage Not More than 2 Years)




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




No specific blanking caps No specific talcum No specific AR CHOCK - WHEEL No specific 1 WARNING NOTICE



Material No. 02-003 F NSA 307110 TYPE 4 NO LONGER AVAILABLE (Ref. 20-31-00) Material No. 03-001 USA MIL-PRF-7870 MINERAL OIL (LOW TEMP) (Ref. 20-31-00)R Material No. 04-001 F DCSEA 359/A WHEEL BEARING MINERAL GREASE (Ref. 20-31-00) Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)



R Material No. 04-011 USA SAE-AMS-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00) Material No. 05-005 USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) Material No. 05-027 RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) Material No. 05-043 VARNISH P.T.F.E SPRAY (Ref. 20-31-00)R Material No. 08-052 USA AMS-T-23397 AND/OR L-T-80BR SELF ADHESIVEALUMINIUM TAPE (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)



05-57-00-200-001 Aircraft Stability 10-11-00-555-013 Installation of the Aircraft Protection Equipment 10-11-00-555-015 Procedure for the Installation of Wheel Chocks on Aircraft 10-20-00-556-001 Mooring of the Aircraft 12-13-27-612-005 Drain and Refill Flap Actuator Assemblies with Semi-fluid 12-16-38-613-001 Servicing of the Toilet System 12-21-11-615-002 External Cleaning 12-21-12-100-002 Cleaning of the Cockpit Equipment/Furnishings 12-21-12-100-003 Cleaning of the Carpets and Non-Textile Floor Covering (NTF) 12-21-12-100-004 Cleaning of the Plastic Surfaces and Mirrors 12-21-12-100-005 Cleaning of the Seat Covers and the Curtains 12-21-12-100-006 Cleaning of the Light Alloy and Steel Components 12-21-12-100-007 Cleaning of the Cargo Compartments 12-21-12-100-008 Cleaning of the Cabin Monitors and Display Screens (if installed) 12-21-12-100-009 Cleaning of the Plastic Wash Basin in the Lavatories 12-22-27-640-003 Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut 12-22-27-640-004 Lubricate all Carriage Rollers on all Flap Tracks



12-22-27-640-005 Lubrication of Spoiler No.1 to 5 Servo Control Bearings 12-22-27-640-006 Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth 12-22-27-640-007 Lubrication of the THS Mechanical Control Chains 12-22-32-640-001 Lubrication of the MLG and Doors 12-22-32-640-002 Lubrication of the NLG and Doors 12-22-52-640-002 Lubrication of the FWD and AFT Cargo-Compartment Doors 12-22-52-640-006 Lubrication of the External Control Handles of the FWD and AFT Passenger/Crew Doors 12-22-52-640-008 Lubrication of the Avionics Compartment-Door Handles 12-22-52-640-009 Lubrication of the FWD and AFT Cargo-Compartment Door Handle 12-22-52-640-014 Lubrication of Safety Pin Guide Fitting and Door Arming/Disarming Mechanism 12-22-52-640-016 Lubrication of the Hinge-Arm Support-Fitting Bearings 12-22-53-640-001 Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004 12-22-55-640-001 Lubrication of Rudder Hinge Bearing No. 6 with Grease Mat. No. 04-004 12-22-56-600-001 Lubrication of the Cockpit Sliding Window Tracks 12-24-38-680-001 Draining of the Potable Water System (with Electrical Power) 12-31-21-660-001 Cold Weather Maintenance - Air Conditioning 12-31-24-660-001 Cold Weather Maintenance - Electrical Power 12-31-25-660-001 Cold Weather Maintenance - Equipment/Furnishings 12-31-27-660-001 Cold Weather Maintenance - Flight Controls 12-31-28-660-001 Cold Weather Maintenance - Fuel 12-31-31-660-001 Cold Weather Maintenance - Indicating/Recording systems and Navigation 12-31-32-660-001 Cold Weather Maintenance - Landing Gear 12-31-35-660-001 Cold Weather Maintenance - Oxygen System 12-31-38-660-001 Cold Weather Maintenance - Water/Waste 12-31-49-660-001 Cold Weather Maintenance - Auxiliary Power Unit 12-31-51-660-001 Cold Weather Maintenance - Structure 12-31-52-660-001 Cold Weather Maintenance - Doors 12-31-71-660-001 Cold Weather Maintenance - Power Plant 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 12-34-24-869-002 Aircraft Grounding for the Maintenance Operations 20-24-11-100-001 Cleaning and Protection of the Cables



23-71-35-000-001 Removal of the Cockpit Voice Recorder (CVR) 1RK 24-21-00-600-040 Preservation/Storage/Return to Service of the IDG 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 26-21-41-000-004 Removal of the Cartridge of the Engine Fire-Extinguisher Bottle 26-22-41-000-001 Removal of the Fire Extinguisher Bottle (11WF) 26-23-41-000-004 Removal of the Cargo Fire-Extinguisher Bottle (4005WX) 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Biobor Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - With Fuel Mixed with Kathon Biocide 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Biobor Biocide With a Metered Injection Rig 28-11-00-600-010 Biocidal Preventative Treatment for Aircraft in Long-Term Storage - Using Kathon Biocide With a Metered Injection Rig 29-00-00-790-001 Check of the External Leaks of the Hydraulic Components 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 30-45-00-040-002 Deactivation of the Rain Repellent System 30-45-52-000-002 Removal of the Wiper Arm (306DM, 307DM) 30-45-53-000-001 Removal of the Wiper Blade 31-33-55-000-001 Removal of the Digital Flight Data Recorder (DFDR) 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears



32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-40-00-200-001 Inspection/Check of the Wheels & Brakes 32-41-00-210-003 Inspection/Check of the Pressure of Tires 32-41-11-400-006 Installation of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-41-12-400-001 Installation of the NLG Wheel (2659GM,2660GM) 32-48-51-000-005 Removal of the Fan Assy (7GS,8GS,9GS,10GS) 33-51-38-000-002 Removal of the Battery of the Emergency Power-Supply Unit 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS) 49-20-00-200-001 Inspection/Check of the Engine (4005KM) (GTCP 36-300) 49-20-00-210-001 APU Power Plant Visual Inspection (APS 3200) 49-20-00-600-001 Preservation / Storage / De-preservation of the Engine (GTCP 36-300) 49-20-00-600-002 Preservation/Storage/Return to Service of APU (APS 3200) 49-20-00-600-003 Preservation/Storage/Return to Service of APU (131-9(A)) 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 53-59-00-210-001 Operational Check of Single Drain Pipe Aft of FR70 from Outside 54-50-00-200-001 General Visual Inspection of the Pylon Drain System 71-00-00-550-010 Preservation of the Power Plant


3. Job Set-up __________

Subtask 10-12-00-860-061

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

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


Subtask 10-12-00-615-055



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


Subtask 10-12-00-941-052







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


Subtask 10-12-00-650-054





Subtask 10-12-00-010-059

A. Get Access

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

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

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



Subtask 10-12-00-170-054

B. Flushing of the Air Data System




Subtask 10-12-00-620-082

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

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

(d) Apply talcum 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) - main landing gear (Ref. TASK 12-22-32-640-001)

(f) Clean all the actuator rods and apply a thin layer of HYDRAULIC FLUIDS (Material No. 02-003).

(g) 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 used tires or wheels with used tires: - on the nose landing gear (Ref. TASK 32-41-12-400-001) - on the main landing gear (Ref. TASK 32-41-11-400-006)

(b) Lubricate the bearings with COMMON GREASE (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).

(d) Remove the debris guard, the impeller and the shroud of the brake fans (Ref. TASK 32-48-51-000-005) (If installed). - Apply SPECIAL MATERIALS (Material No. 05-027) on the removed parts.

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

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

Subtask 10-12-00-550-053


(1) Protection of the potable water system

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

(2) 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 12-16-38-613-001).


Subtask 10-12-00-620-083-A

E. Protection of the Flight Controls

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

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

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

Subtask 10-12-00-620-084

R F. Protection of the fuel system



(a) If premixed fuel is available: - Refuel the wing tanks to 30% of the total capacity with fuel premixed with biocide (Ref. TASK 28-11-00-600-010) or (Ref. TASK 28-11-00-600-010) - Refuel the center tank to 30% of the total capacity with fuel premixed with biocide (Ref. TASK 28-11-00-600-010) or (Ref. TASK 28-11-00-600-010).

(b) If premixed fuel is not available: - Refuel the wing tanks to 30% of the total capacity with fuel not premixed with biocide (Ref. TASK 28-11-00-600-010) or (Ref. TASK 28-11-00-600-010) - Refuel the center tank to 30% of the total capacity with fuel not premixed with biocide (Ref. TASK 28-11-00-600-010) or (Ref. TASK 28-11-00-600-010).





Subtask 10-12-00-620-085

G. Protection of the Engines

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

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

Subtask 10-12-00-620-086

H. Protection of the APU

(1) Do an inspection of the APU for preservation: - for a GTCP 36-300 APU: (Ref. TASK 49-20-00-200-001) - for an APS 3200 APU: (Ref. TASK 49-20-00-210-001)

(2) Do the preservation of the APU: - for a GTCP 36-300 APU: (Ref. TASK 49-20-00-600-001) - for an APS 3200 APU: (Ref. TASK 49-20-00-600-002) - for a 131-9(A) APU: (Ref. TASK 49-20-00-600-003)

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

Subtask 10-12-00-210-070

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).

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

(c) On the engines.

(d) In all other locations.


Subtask 10-12-00-620-087

K. External Protection of the Aircraft

R (1) With STORAGE PRESERVATION (Material No. 15-002) and BONDING ANDR 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.

R (2) Seal with fine nylon netting and BONDING AND ADHESIVE COMPOUNDSR (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

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.



Subtask 10-12-00-620-096

M. Protection of the Doors


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




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


Subtask 10-12-00-620-089

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).

��R �EFF : ALL � Page 230�� 10-12-00 � � May 01/09 � � � � WZZ

Subtask 10-12-00-620-090

P. Protection of the Rain Protection System

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

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

(3) Remove the wiper blades (Ref. TASK 30-45-53-000-001) and the wiper arms (Ref. TASK 30-45-52-000-002).

Subtask 10-12-00-620-091

Q. Protection of the Windows

(1) Lubricate the sliding windows (Ref. TASK 12-22-56-600-001).


R (3) Give external protection to the cockpit and cabin windows withR STORAGE PRESERVATION (Material No. 15-002) and BONDING AND ADHESIVER COMPOUNDS (Material No. 08-052) (or equivalent). Do not put BONDINGR AND ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent) on theR windows.


Subtask 10-12-00-020-062

R. Removal of Equipment

(1) Remove the Digital Flight Data Recorder 1TU (Ref. TASK 31-33-55-000- 001).

(2) Remove the Cockpit Voice Recorder 1RK (Ref. TASK 23-71-35-000-001).

(3) Remove the batteries of: - all the EPSU (Ref. TASK 33-51-38-000-002), - the megaphones, - the flashlights.

(4) Remove the emergency locator beacon.


(5) If the external temperature is more than 70 DEG.C (158.00 DEG.F), remove: - the cargo fire-extinguishing bottles and cartridges (Ref. TASK 26- 23-41-000-004). - the engine fire-extinguishing bottles and cartridges (Ref. TASK 26- 21-41-000-004). - the APU extinguishing-bottle and cartridge (Ref. TASK 26-22-41-000- 001).

(6) Put blanking caps on the disconnected electrical connectors.

Subtask 10-12-00-620-092

S. Protection of the Hydraulic System

(1) Do a check of the hydraulic components for external leakage (Ref. TASK 29-00-00-790-001).

Subtask 10-12-00-555-057

T. Installation of the Protection Equipment

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

R (2) Keep all external protection equipment flags in position with BONDINGR AND ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent).

Subtask 10-12-00-860-062

U. Aircraft Maintenance Configuration




5. Close-up ________

Subtask 10-12-00-942-057

A. Close-up




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

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

R (6) Seal with STORAGE PRESERVATION (Material No. 15-002) and BONDING ANDR ADHESIVE COMPOUNDS (Material No. 08-052) (or equivalent) all theR openings that give access to: - the passenger compartment, - the cockpit, - the cargo compartment, - the APU, - the engines, - the landing gears.

R (7) Seal with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-052) (orR equivalent): - the passenger/crew door handles, - the emergency exit door handles, - the FWD and aft cargo door handles, - the avionics-compartment door handles.




(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.


INTENTIONALLY BLANK

��R � � Page 234�� 10-12-00 � � May 01/09 � � � � WZZ

TASK 10-12-00-553-008

Renewal for 6 Months Storage Period


This procedure lets the operator do the storage procedure for 6 months again one time.




No specific 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE



10-12-00-200-006 Periodic Ground Check at 7-day Intervals 10-12-00-200-007 Periodic Ground Check at 15-day Intervals 10-12-00-200-008 Periodic Ground-Check at 1-month Interval 10-12-00-200-009 Periodic ground-check at 3-month interval 12-22-27-640-003 Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut 12-22-27-640-004 Lubricate all Carriage Rollers on all Flap Tracks 12-22-27-640-005 Lubrication of Spoiler No.1 to 5 Servo Control Bearings 12-22-27-640-006 Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth 12-22-27-640-007 Lubrication of the THS Mechanical Control Chains 12-22-32-640-001 Lubrication of the MLG and Doors 12-22-32-640-002 Lubrication of the NLG and Doors 12-22-53-640-001 Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004R 12-22-55-640-001 Lubrication of Rudder Hinge Bearing No. 6 with GreaseR Mat. No. 04-004 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 20-24-11-100-001 Cleaning and Protection of the Cables


3. Job Set-up __________

Subtask 10-12-00-941-056

A. Get Access



Subtask 10-12-00-553-070

A. Ground Check

(1) Do the periodic ground checks at: - 7-day intervals (Ref. TASK 10-12-00-200-006) - 15-day intervals (Ref. TASK 10-12-00-200-007) - 1-month intervals (Ref. TASK 10-12-00-200-008) - 3-month intervals (Ref. TASK 10-12-00-200-009).

Subtask 10-12-00-620-095

B. Protection

(1) Lubrication of the mechanical control chains of the THS (Ref. TASK 12-22-27-640-007) and the actuator ball screw nut (Ref. TASK 12-22- 27-640-003).

(2) Clean and put protection on the flight control cables (Ref. TASK 20- 24-11-100-001).

(3) Lubrication of the rollers of the flap tracks (Ref. TASK 12-22-27- 640-004).

(4) Lubrication of all the rollers and pinions of the slat tracks (Ref. TASK 12-22-27-640-006).

(5) Lubrication of spoiler servo-control bearings (Ref. TASK 12-22-27- 640-005).

(6) Lubrication of the hinges and the attach fittings of the horizontal stabilizer (Ref. TASK 12-22-53-640-001).

(7) Lubrication of the rudder bearing No. 6 (Ref. TASK 12-22-55-640-001).


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

Subtask 10-12-00-281-054

C. Protection of the fuel





Subtask 10-12-00-020-063

D. Removal of Components

(1) Remove all the batteries of: - the megaphones - the flashlights.

5. Close-up ________

Subtask 10-12-00-942-061

A. Put the aircraft back to its initial configuration.



TASK 10-12-00-553-009

Renewal for 2 Years Storage Period


Self Explanatory




10-12-00-553-007 Storage Procedure (Storage Not More than 2 Years) 10-30-00-554-005 Return to Operation after Storage Period

3. Job Set-up __________

Subtask 10-12-00-860-064

A. Not Applicable


Subtask 10-12-00-210-080

A. Preparation of the Aircraft

(1) Do the full return to operation after storage (Ref. TASK 10-30-00- 554-005).

Subtask 10-12-00-554-050

B. Non-revenue Flight

(1) Do a short non-revenue flight within the aircraft standard envelope.

Subtask 10-12-00-553-071

C. Store the Aircraft

(1) Do the storage procedure (Ref. TASK 10-12-00-553-007).

��R �EFF : ALL � Page 238�� 10-12-00 � � Feb 01/08 � � � � WZZ

STORAGE - INSPECTION/CHECK __________________________

TASK 10-12-00-200-006



To do a check of the condition of the aircraft during the storage period.





R B. Referenced Information

R -------------------------------------------------------------------------------R REFERENCE DESIGNATIONR -------------------------------------------------------------------------------

R 71-00-00-550-010 Preservation of the Power Plant

3. Job Set-up __________

Subtask 10-12-00-941-053

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


Subtask 10-12-00-210-071

A. Visual Inspection


(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

R B. Inspection of the Engine Humidity Indicator

R (1) For engines PRE-SB72-0369R Examine the indicators. If one or more of the indicators show tooR much humidity, replace the indicator and desiccant and do the engine preservation procedure again (Ref. TASK 71-00-00-550-010).

R (2) For engines POST-SB72-0369R Only examine the indicators after the first 7 days. If one or more ofR the indicators show too much humidity, replace the indicator andR desiccant and do the engine preservation procedure again (Ref. TASKR 71-00-00-550-010).

5. Close-up ________

Subtask 10-12-00-942-058

A. Remove the access platform(s).


TASK 10-12-00-200-007










R 10-11-00-555-015 Procedure for the Installation of Wheel Chocks onR Aircraft 12-24-34-600-001 Bleeding of the Standby Air Data System 12-32-28-281-001 Drain Water Content 32-41-00-210-002 Inspection/Check of the Wheels and Tires 32-41-00-210-003 Inspection/Check of the Pressure of Tires

3. Job Set-up __________

Subtask 10-12-00-941-054

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



Subtask 10-12-00-553-069

A. Move the Aircraft

NOTE : if old 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.

R (3) Put the wheel chocks in position: (Ref. TASK 10-11-00-555-015)R

Subtask 10-12-00-210-072

B. Visual Inspection

(1) 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).

(3) Do a tire pressure check, if necessary inflate the tires (Ref. TASK 32-41-00-210-003).

Subtask 10-12-00-170-055

C. Drain the Standby Static Line

(1) Remove the water from the standby static line (Ref. TASK 12-24-34- 600-001).

Subtask 10-12-00-680-055

D. Inspection of the Fuel Tanks

(1) Drain water from the fuel tanks (Ref. TASK 12-32-28-281-001).


5. Close-up ________

Subtask 10-12-00-942-059


(1) Remove the access platform(s).


TASK 10-12-00-200-008

Periodic Ground-Check at 1-month Interval


Self Explanatory


A. Consumable Materials


Material No. 05-043 VARNISH P.T.F.E SPRAY (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)



R 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 21-26-00-710-001 Operational Check of System via MCDU 21-28-00-710-006 Operational Test of the AFT Cargo-Compartment Ventilation-System 21-28-00-720-003 Functional Test of the FWD Cargo-Compartment Ventilation-System 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM (13QM) 30-11-00-710-001 Operational Test of the Wing Ice-Protection System 30-21-00-710-001 Operational Test of the Anti Ice System Fault Warning 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-22-00-010-001 Opening of the Emergency Exit Doors from the Passenger Compartment



52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 71-00-00-550-010 Preservation of the Power Plant

3. Job Set-up __________

Subtask 10-12-00-010-060

A. Get Access

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

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

(3) Open the emergency exit doors (Ref. TASK 52-22-00-010-001).

Subtask 10-12-00-860-063

B. Aircraft Configuration

(1) 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).

(3) On the overhead panel 25VU, on the CABIN PRESS section: - release the DITCHING pushbutton switch to open the avionics ventilation skin- valves.




Subtask 10-12-00-620-094

A. 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

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

R (4) Close all the fuel system valves.

Subtask 10-12-00-210-082

C. 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).

Subtask 10-12-00-710-071

D. Do these Tests:

(1) Do a test of the avionics equipment ventilation (Ref. TASK 21-26-00- 710-001).

(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).

(3) If the FWD cargo-compartment ventilation-system is installed, do a test of the FWD cargo-compartment ventilation-system (Ref. TASK 21- 28-00-720-003).


(4) Do a test of the wing ice-protection system (Ref. TASK 30-11-00-710- 001).

(5) Do a test of the anti ice system fault warning (Ref. TASK 30-21-00- 710-001).

(6) Do a test of the ENG 1(2) LP fuel valve 12MQ(13MQ) (Ref. TASK 28-24- 00-710-002).

5. Close-up ________

Subtask 10-12-00-410-059

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.



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

(5) Close the emergency exit doors (Ref. TASK 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.



TASK 10-12-00-200-009

Periodic ground-check at 3-month interval









R Material No. 04-011 USA SAE-AMS-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00) Material No. 05-005 USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) Material No. 05-027 RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) Material No. 11-002 USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)




05-27-10-200-001 Zonal Inspection of Nose Gear and Nose Gear Doors 05-27-30-200-001 Zonal Inspection of LH/RH Main Landing Gear 07-12-00-582-001 Jacking for Nose Gear Wheel Change 07-12-00-582-002 Jacking for Main Gear Wheel Change 10-20-00-556-001 Mooring of the Aircraft 12-21-11-615-002 External Cleaning 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 27-14-00-710-001 Operational Test of the Aileron and Hydraulic Actuation 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-34-00-710-001 Operational Test of the Elevator and Hydraulic Actuation 27-54-00-710-001 Operational Test of the Flap System 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 27-84-00-710-001 Operational Test of the Slat System 28-23-00-720-001 Operational Test of Crossfeed Valve Using Individual Motors: ... 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM (13QM) 28-29-00-710-001 Operational Test of the APU Low Pressure Fuel Valve using each individual Motor in turn 29-10-00-200-001 Check Fluid Level on Reservoir Indicators 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 32-31-00-710-002 Operational Test of the Landing Gear Doors (With False Targets) 51-74-11-300-001 Repair of Corroded Areas 53-59-00-210-001 Operational Check of Single Drain Pipe Aft of FR70 from Outside



54-50-00-200-001 General Visual Inspection of the Pylon Drain System

3. Job Set-up __________

Subtask 10-12-00-941-055

A. Get Access



Subtask 10-12-00-210-073


(1) 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 - the frame around the doors

(g) the external handle of the passenger/crew doors

(h) the drains:

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


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

3 In all other locations. _

(i) the toilet areas

(j) all steel parts for corrosion.

(2) If you find corrosion, remove it (Ref. TASK 51-74-11-300-001).

Subtask 10-12-00-615-056


(1) 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).

Subtask 10-12-00-650-055

C. Aircraft Configuration

(1) Energize the aircraft electrical circuits from the external power (Ref. TASK 24-41-00-861-002).

(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.



Subtask 10-12-00-710-070

D. Do these Tests:

(1) Do a test of the crossfeed valves (Ref. TASK 28-23-00-720-001).

(2) Do a test the engine LP-fuel shut-off valve (Ref. TASK 28-24-00-710- 002).

(3) Do a test of the APU shut-off valve (Ref. TASK 28-29-00-710-001).


(4) Do a test of the aileron and its hydraulic system (Ref. TASK 27-14- 00-710-001).

(5) Do a test of the elevator and its hydraulic system (Ref. TASK 27-34- 00-710-001).

(6) Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710- 001).

(7) Do a test of the flap system (Ref. TASK 27-54-00-710-001).

(8) Do a test of the spoiler hydraulic system (Ref. TASK 27-64-00-710- 001).

(9) Do a test of the slat system (Ref. TASK 27-84-00-710-001).

(10) Do a test of the landing gear doors (Ref. TASK 32-31-00-710-002).

Subtask 10-12-00-210-074

E. Inspection of the Landing Gear

(1) Do a general visual inspection: - of the NLG (Ref. TASK 05-27-10-200-001) - of the MLG (Ref. TASK 05-27-30-200-001)

(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) - for MLG (Ref. TASK 07-12-00-582-002)

(4) Put the aircraft on its wheels.

(5) Put the aircraft in mooring condition (Ref. TASK 10-20-00-556-001).

(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

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

Subtask 10-12-00-210-075

G. Inspection of the Hydraulic System

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

(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

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

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


5. Close-up ________

Subtask 10-12-00-942-060


(1) 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.



(4) Install STORAGE PRESERVATION (Material No. 15-002) with new adhesive tape to prevent film hardening and paint removal.



TASK 10-12-00-200-010

Periodic Ground Check at 6-month Intervals


This procedure prevents the damage of the landing gears seals.




32-31-00-720-002 Functional Test of the Normal Extension and Retraction of the Landing Gear

3. Job Set-up __________

Subtask 10-12-00-860-065

A. Not Applicable


Subtask 10-12-00-700-050

A. Test of the Landing Gear

(1) Do a test of extension and retraction of the landing gear (Ref. TASK 32-31-00-720-002)

5. Close-up ________

Subtask 10-12-00-942-062




MOORING - MAINTENANCE PRACTICES _______________________________

TASK 10-20-00-556-001

Mooring of the Aircraft

WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING _______ GEAR.

R

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.


R The function of mooring is to prevent damage to the aircraft on the groundR in high wind conditions and icing conditions.R




R No specific 1 CHOCK - WHEELR




05-57-00-200-001 Aircraft Stability 10-11-00-555-007 Parking Procedure in Flight-ready Condition (Parking of not more than 15 Days)R 10-11-00-555-015 Procedure for the Installation of Wheel Chocks onR AircraftR 12-34-24-869-002 Aircraft Grounding for the Maintenance Operations 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-41-00-210-002 Inspection/Check of the Wheels and Tires 32-47-15-000-001 Removal of the Brake Temperature Sensor (4GW,5GW,6GW,7GW) 32-47-15-400-001 Installation of the Brake Temperature Sensor (4GW,5GW,6GW,7GW)R 10-20-00-991-007 Fig. 201R 10-20-00-991-005 Fig. 202R 10-20-00-991-003 Fig. 203R 10-20-00-991-002-A Fig. 204R 10-20-00-991-006 Fig. 205

3. Job Set-up __________

R Subtask 10-20-00-941-050

R A. Wind Conditions

R (1) For wind speeds of less than 50 Kts:R - Mooring is not necessary if the aircraft configuration is in theR limits given in chapter 05-57-00.

R (2) If the wind speed is between 50 and 70 Kts and stable (no gusts andR the wind direction does not change by more than +/- 30 degrees ) andR the aircraft points into the wind:R - Moor the aircraft at the NLG only.

R NOTE : If it is not possible to point the aircraft into the wind, see ____R para (3).


R (3) If the wind speed is between 50 and 70 Kts and not stable, with theR direction that changes more than +/- 30 degrees:R - Point the aircraft into the primary wind direction (if possible)R and moor at the NLG and the MLG.

R (4) If the wind speed is between 70 Kts and the upper limits defined in:R (Ref. Fig. 201/TASK 10-20-00-991-007)R - Make sure that the aircraft variant mass is sufficient for theR necessary wind speedR - Point the aircraft into the primary wind direction (if possible)R and moor at the NLG and MLG.

R NOTE : If you cannot obtain the necessary aircraft variant mass, you ____R must move the aircraft into a hangar.

R (5) If the wind speed is more than the maximum limits given in:R (Ref. Fig. 201/TASK 10-20-00-991-007)R - You must move the aircraft into a hangar.

R Subtask 10-20-00-941-051

R B. Icing Conditions

R (1) For a temperature of less than -5 deg.C (+23.00 deg.F):R - Move the aircraft into a hangar.

R (2) For a temperature of more than -5 deg.C (+23.00 deg.F):R - If there is ice or if ice is possible, Airbus recommends that youR put salt around and below the tires.R - If there is thick ice or compacted snow, remove the ice or snow, orR move the aircraft into a hangar.

Subtask 10-20-00-860-050

R C. Aircraft Maintenance Configuration

(1) 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.R Make sure that the ground rings are in the ground-ring position area.R (Ref. Fig. 202/TASK 10-20-00-991-005, 203/TASK 10-20-00-991-003)

R (2) In relation to the wind speed, make sure that the aircraft is stable.R Refer to the aircraft stability procedure (Ref. TASK 05-57-00-200- 001).


R Mooring Wind Speed LimitsR Figure 201/TASK 10-20-00-991-007


Position of the Ground RingsR Figure 202/TASK 10-20-00-991-005


Position of the Mooring RopesR Figure 203/TASK 10-20-00-991-003


(3) Make sure that the landing-gear safety devices are in position (Ref. TASK 32-00-00-481-001).

(4) Electrically ground the aircraft (Ref. TASK 12-34-24-869-002).

R (5) Put the CHOCK - WHEEL in position (Ref. TASK 10-11-00-555-015).R

(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) in relation to weather conditions.

R (11) Make sure the aircraft variant weight is commensurate with the windR speed expectedR (Ref. Fig. 201/TASK 10-20-00-991-007)R .

(12) Remove the brake temperature sensors and cables (Ref. TASK 32-47-15- 000-001).


R Subtask 10-20-00-481-050-A

R A. Mooring of the Nose Landing Gear

R (1) With the mooring items that follow:R (Ref. Fig. 204/TASK 10-20-00-991-002-A)


R Nose Landing Gear - Installation of the Mooring ItemsR Figure 204/TASK 10-20-00-991-002-A13 (SHEET 1)


R -------------------------------------------------------------------------------R | DESCRIPTION | ITEM | QUANTITY | LENGTH | MIN ULTIMATE |R | | | | | FAILURE LOAD |R -------------------------------------------------------------------------------R | Textile Roundsling| 1 | 2 | 2000 mm | 12945 daN |R | | | | 78.74 in | 29101 lbf |R ------------------------------|-------------|----------------|-----------------R | Joker | 2 | 2 | / | 24271 daN |R | | | | | 54563 lbf |R ------------------------------|-------------|----------------|-----------------R | Polyester Lashing | | | | |R | Strap with Ratchet| | | | |R | Mechanism (with | 4 & 7 | 4 | as necessary | 9807 daN |R | the ratchet | | | | 22047 lbf |R | mechanism in the | | | | |R | center of the | | | | |R | lash) | | | | |R ------------------------------|-------------|----------------|-----------------R | Steel Bow Shackle | 5 | 4 | / | 7845 daN |R | | | | | 17636 lbf |R -------------------------------------------------------------------------------R | Master Link | 3 | 2 | / | 24271 daN |R | | | | | 54563 lbf |R -------------------------------------------------------------------------------R | Ground Ring (set | 6 | 4 | / | 15691 daN |R | into ground) | | | | 35275 lbf |R -------------------------------------------------------------------------------R | NOTE : The manufacturer of the mooring equipment (shown in the table above) |R | can possibly also supply a Minimum Ultimate Failure Load or a Safe |R | Working Load with a Safety Factor for the equipment. |R | The Minimum Ultimate Failure Load is the load at which equipment |R | failure will occur. The Safe Working Load is lower than the Minimum |R | Ultimate Failure Load. To calculate the Safe Working Load, you must |R | use a special safety factor applicable for the initial function of |R | the equipment. |R | If a Safe Working Load is shown on the equipment, you can multiply |R | this load by the Safety Factor given by the manufacturer to get the |R | Minimum Ultimate Failure Load of the equipment. |R | You must then make sure that the calculated Minimum Ultimate Failure |R | Load is equal to or more than the value given in the table above for |R | the related equipment. |R | |R | Here is an example: |R | A textile roundsling has a Safe Working Load of 5000 daN. |R | A Safety Factor of 7 is given by the manufacturer. |R | Minimum Ultimate Failure Load = 5000 daN x 7 |R | = 35000 daN |


R | The minimum permitted failure load of the textile roundsling for |R | this configuration (as shown in the above table) is 12945 daN. The |R | equipment is thus serviceable. |R -------------------------------------------------------------------------------

R NOTE : Roundslings are continuous loops. The Roundsling Minimum ____R Failure Load relates to the Roundsling load as a single loop.

R NOTE : It is not necessary to use the bow shackle in the system. If ____R you do not use the bow shackle, use the ratchet mechanism toR attach the two ends of the lashing strap together. But weR recommend that you use the bow shackle to make installationR easier.

R (a) Wind two roundslings (1) around the NLG sliding tube and belowR the axles.

R (b) Pull each roundsling (1) to a point that is in line with theR centerline of the sliding tube (make sure that each section ofR roundslings is of equal length). Then attach them to theR roundsling joker hook (2).

R (c) Attach the joker (2) to the master link (3).

R (d) Get one lash with the integral ratchet mechanism assembly (4) andR put one of its ends through the ground ring (6).

R (e) Put the other end of the lash (4) through the master link (3).R Move the two loose ends of the lash (4) to a point in the middleR between the ground ring (6) and the master link (3).

R (f) Connect the two ends of the lash (4) together with a bow shackleR (5).

R (g) Do steps (d) thru (f) again for each ground position.

R (h) Use the integral ratchet (7) to lightly pull each lash (4) soR that it is not loose. Make sure that the last lateral position ofR the master link (3) is in the axis of the centerline of theR sliding tube.

R NOTE : The function of the ratchet (7) is to make sure that the ____R lashes (4) are not loose but not to put tension in theR system.


R (i) Make sure that the polyester lash axes are in the ground-ringR position area.R (Ref. Fig. 202/TASK 10-20-00-991-005)

R (2) Post Mooring InspectionR Because wind speed is not constant or predictable, it is necessary toR examine the landing gear for damage. This is to prevent the possibleR effects of too much wind speed and thus a possible landing gearR overload. Because of this, you must do the inspections that followR after the mooring configuration is removed (when high winds stop).

R (a) Do a visual inspection of the roundsling interfaces on theR sliding tube and axle for signs of damage to the landing-gearR surface finish (chrome detachment, scratches or flaking paint).

R (b) Do a check of the tires for flat spots and signs of increasedR wear (Ref. TASK 32-41-00-210-002).

R (c) Do an inspection of the NLG/fuselage attachments and make sureR that:R - There are no cracks.R - There is no damage to the paint and sealant.

Subtask 10-20-00-481-052

B. Mooring of the Main Landing Gear

R (1) With the mooring items that follow:R (Ref. Fig. 205/TASK 10-20-00-991-006)


Main Landing Gear - Installation of the Mooring ItemsR Figure 205/TASK 10-20-00-991-006- 13 (SHEET 1)


R -------------------------------------------------------------------------------R | DESCRIPTION | ITEM | QUANTITY | LENGTH | MIN ULTIMATE |R | | | | | FAILURE LOAD |R -------------------------------------------------------------------------------R | Textile Roundsling| 1 | 4 | 2000 mm | 12945 daN |R | | | | 78.74 in | 29101 lbf |R ------------------------------|-------------|----------------|-----------------R | Joker | 2 | 4 | / | 24271 daN |R | | | | | 54563 lbf |R ------------------------------|-------------|----------------|-----------------R | Polyester Lashing | | | | |R | Strap with Ratchet| | | | |R | Mechanism (with | 4 & 7 | 8 | as necessary | 9807 daN |R | the ratchet | | | | 22047 lbf |R | mechanism in the | | | | |R | center of the | | | | |R | lash) | | | | |R ------------------------------|-------------|----------------|-----------------R | Steel Bow Shackle | 5 | 8 | / | 7845 daN |R | | | | | 17636 lbf |R -------------------------------------------------------------------------------R | Master Link | 3 | 4 | / | 24271 daN |R | | | | | 54563 lbf |R -------------------------------------------------------------------------------R | Ground Ring (set | 6 | 8 | / | 15691 daN |R | into ground) | | | | 35275 lbf |R -------------------------------------------------------------------------------R | NOTE : The manufacturer of the mooring equipment (shown in the table above) |R | can possibly also supply a Minimum Ultimate Failure Load or a Safe |R | Working Load with a Safety Factor for the equipment. |R | The Minimum Ultimate Failure Load is the load at which equipment |R | failure will occur. The Safe Working Load is lower than the Minimum |R | Ultimate Failure Load. To calculate the Safe Working Load, you must |R | use a special safety factor applicable for the initial function of |R | the equipment. |R | If a Safe Working Load is shown on the equipment, you can multiply |R | this load by the Safety Factor given by the manufacturer to get the |R | Minimum Ultimate Failure Load of the equipment. |R | You must then make sure that the calculated Minimum Ultimate Failure |R | Load is equal to or more than the value given in the table above for |R | the related equipment. |R | |R | Here is an example: |R | A textile roundsling has a Safe Working Load of 5000 daN. |R | A Safety Factor of 7 is given by the manufacturer. |R | Minimum Ultimate Failure Load = 5000 daN x 7 |R | = 35000 daN |


R | The minimum permitted failure load of the textile roundsling for |R | this configuration (as shown in the above table) is 12945 daN. The |R | equipment is thus serviceable. |R -------------------------------------------------------------------------------

R NOTE : Roundslings are continuous loops. The Roundsling Minimum ____R Failure Load relates to the Roundsling load as a single loop.

R NOTE : It is not necessary to use the bow shackle in the system. If ____R you do not use the bow shackle, use the ratchet mechanism toR attach the two ends of the lashing strap together. But weR recommend that you use the bow shackle to make installationR easier.

R

R (a) Wind two roundslings (1) around the left MLG sliding tube andR below the axles.

R (b) Pull each roundsling (1) to a point that is in line with theR centerline of the sliding tube (make sure that each section ofR roundslings is of equal length). Then attach them to theR roundslings joker hooks (2).

R (c) Attach the joker (2) to the master link (3).

R (d) Get one lash with the integral ratchet mechanism assembly (4) andR put one of its ends through the ground ring (6).

R (e) Put the other end of the lash (4) through the master link (3).R Move the two loose ends of the lash (4) to a point in the middleR between the ground ring (6) and the master link (3).

R (f) Connect the two ends of the lash (4) together with a bow shackleR (5).

(g) Do steps (d) thru (f) again for each ground position.

(h) Use the integral ratchet (7) to lightly pull each lash (4) soR that it is not loose. Make sure that the last lateral position ofR the master link (3) is in the axis of the centerline of the sliding tube.

R NOTE : The function of the ratchet (7) is to make sure that the ____R lashes (4) are not loose but not to put tension in theR system.


(i) Do steps (a) thru (h) again for the right MLG.

R (j) Make sure that the polyester lash axes are in the ground-ringR position area.R (Ref. Fig. 202/TASK 10-20-00-991-005)R .

(2) Post Mooring InspectionR Because wind speed is not constant or predictable, it is necessary toR 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 32-41-00-210-002).

R (c) If there was possible interference between the roundslings andR MLG dressings, do a detailed visual inspection of the MLGR 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.

R (f) If you find damage during inspections, replace or repair theR damaged component (refer to the applicable manuals SRM, AMM, CMM)R and make sure that the adjacent area has no damage.

5. Close-up ________

Subtask 10-20-00-942-050


(1) After removal of the mooring equipment, install the brake temperature sensors and cables (Ref. TASK 32-47-15-400-001).



(3) Make sure that the work area is clean and clear of tool(s) and other items.


RETURN TO SERVICE - INSPECTION/CHECK ____________________________________

TASK 10-30-00-554-005

Return to Operation after Storage Period


Self Explanatory




No specific 1 ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE No specific 1 WARNING NOTICE



R Material No. 04-004 USA MIL-PRF-23827 TYPE IR SYNTH.ESTER BASED GREASE HIGH PRESSURER (Ref. 20-31-00)R Material No. 05-005 USA MIL-C-16173 GRADE IIR CORROSION PREVENTIVE (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)




10-11-00-555-014 Removal of the Aircraft Protection Equipment 12-13-27-612-002 Oil Replenishment of the Flap PCU (6201CM) Gearbox 12-13-27-612-003 Oil Replenishment of the Slat PCU (6001CM) Gearbox 12-13-27-612-005 Drain and Refill Flap Actuator Assemblies with Semi-fluid 12-13-80-600-011 Drain and Replenish Oil System 12-13-80-600-011 Drain and Replenish Oil System 12-14-32-614-001 Nitrogen Filling of the Tires 12-21-11-615-002 External Cleaning 12-22-27-640-003 Lubrication of Trimmable Horizontal Stabilizer Actuator Ball Screw Nut 12-22-27-640-004 Lubricate all Carriage Rollers on all Flap Tracks 12-22-27-640-005 Lubrication of Spoiler No.1 to 5 Servo Control Bearings 12-22-27-640-006 Lubrication of all Slat Track Rollers, Pinion Bearings, Pinions and Rack Teeth 12-22-27-640-007 Lubrication of the THS Mechanical Control Chains 12-22-32-640-001 Lubrication of the MLG and Doors 12-22-32-640-002 Lubrication of the NLG and Doors 12-22-53-640-001 Lubrication of Trimmable Horizontal Stabilizer Bearings and Attachment Fittings with Grease Mat. No. 04-004R 12-22-55-640-001 Lubrication of Rudder Hinge Bearing No. 6 with GreaseR Mat. No. 04-004 12-32-28-281-001 Drain Water Content 12-32-28-281-003 Sample Fuel for Microbiological Contamination Analysis 12-32-29-281-001 Hydraulic Fluid Sample of Green, Blue and Yellow Systems for Analysis 20-24-11-100-001 Cleaning and Protection of the Cables 21-21-41-920-002 Scheduled Replacement of the Recirculation Filter 4012HM (4013HM) 21-26-00-710-001 Operational Check of System via MCDU 21-26-00-710-001 Operational Check of the Avionics Equipment Ventilation (without the CFDS) 21-28-00-720-003 Functional Test of the FWD Cargo-Compartment Ventilation-System 21-28-00-720-004 Functional Test of the AFT Cargo-Compartment Ventilation-System 23-61-00-200-001 - Check Resistance of Tip to Retainer - Check Bonding of Retainer to Structure



23-71-35-400-001 Installation of the Cockpit Voice Recorder (CVR) 1RK 24-21-00-600-040 Preservation/Storage/Return to Service of the IDG 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 26-12-00-710-001 Operational Check of Loop/Squib 26-21-00-710-002 Operational Check of Bottle Low Pressure Indicating Circuit 26-21-00-720-003 Check Distribution Piping for Leakage and Obstruction 26-21-41-400-004 Installation of the Cartridge of the Engine Fire-Extinguisher Bottle 26-22-00-210-001 Inspection of the APU Fire-Extinguishing Distribution Piping 26-22-00-710-001 Operational Test of the APU Fire-Extinguishing Loop/Squib 26-22-00-710-003 Operational Test of the Low-Pressure Indicating Circuit of the APU Fire-Extinguishing Bottle 26-22-41-400-001 Installation of the Fire Extinguisher Bottle (11WF) 26-23-00-200-001 Check Fire Extinguisher Lines for Leakage and Obstruction 26-23-00-710-001 Operational Test of the Cargo-Compartment Fire-Extinguishing System 26-23-41-400-004 Installation of the Cargo Fire-Extinguisher Bottle (4005WX) 26-24-00-210-001 Inspection/Check of the Portable Fire Extinguishers 26-25-00-200-005 Visual Check of Fire Extinguisher Bottle Pressure Reading 27-14-00-710-001 Operational Test of the Aileron and Hydraulic Actuation 27-24-00-710-002 Operational Test of the Rudder Servocontrols with Individual Hydraulic System 27-34-00-710-001 Operational Test of the Elevator and Hydraulic Actuation 27-54-00-200-001 Detailed Visual Inspection of the Transmission Assembly (Including Part of the Transmission in Zone 140) 27-54-00-710-001 Operational Test of the Flap System 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 27-84-00-200-001 Detailed Visual Inspection of the Slat Transmission SystemR 28-11-00-280-002 Structural Fuel Tank Leaks - General Information



28-11-00-600-008 Biocidal Shock Treatment for Moderate Contamination - With Fuel Mixed with Biobor Biocide 28-11-00-600-008 Biocidal Shock Treatment for Moderate Contamination - With Fuel Mixed with Kathon Biocide 28-11-00-600-008 Biocidal Shock Treatment for Moderate Contamination - Using Biobor Biocide With a Metered Injection Rig 28-11-00-600-008 Biocidal Shock Treatment for Moderate Contamination - Using Kathon Biocide With a Metered Injection Rig 28-11-00-600-009 Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Biobor Biocide 28-11-00-600-009 Biocidal Shock Treatment for Heavy Contamination - With Fuel Mixed with Kathon Biocide 28-11-00-600-009 Biocidal Shock Treatment for Heavy Contamination - Using Biobor Biocide With a Metered Injection Rig 28-11-00-600-009 Biocidal Shock Treatment for Heavy Contamination - Using Kathon Biocide With a Metered Injection Rig 28-23-00-720-001 Operational Test of Crossfeed Valve Using Individual Motors: ... 28-24-00-710-002 Operational Test of the ENG 1(2) LP Fuel Valve 12QM (13QM) 28-29-00-710-001 Operational Test of the APU Low Pressure Fuel Valve using each individual Motor in turn 29-10-00-200-001 Check Fluid Level on Reservoir Indicators 29-10-00-710-001 Operational Check of Hydraulic Fire Shut Off Valves and Associated Indicating System 30-11-00-710-001 Operational Test of the Wing Ice-Protection System 30-21-00-710-002 Operational Test of the Engine Air Intake Ice Protection (with the Engines in operation) 30-45-00-440-002 Reactivation of the Rain Repellent System 30-45-52-400-002 Installation of the Wiper Arm (306DM, 307DM) 30-45-53-400-001 Installation of the Wiper Blade 31-21-00-750-002 Procedure to set the Clock 31-33-55-400-002 Installation of the Digital Flight Data Recorder (DFDR) 32-11-00-200-001 Inspection/Check of the Main Gear 32-21-00-200-002 General Visual Inspection of the Nose Landing Gear 32-31-00-720-002 Functional Test of the Normal Extension and Retraction of the Landing Gear 32-33-00-720-001 Functional Check of Free-Fall Extension 32-41-00-210-002 Inspection/Check of the Wheels and Tires 32-41-00-210-003 Inspection/Check of the Pressure of Tires 32-41-11-000-006 Removal of the MLG Wheel (2649GM,2650GM,2651GM,2652GM)



32-41-11-400-006 Installation of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-41-12-000-001 Removal of the NLG Wheel (2659GM,2660GM) 32-41-12-400-001 Installation of the NLG Wheel (2659GM,2660GM) 32-42-00-710-001 Operational Check of the Normal Braking System 32-43-00-710-001 Operational Check of Alternate Braking System 32-48-51-400-005 Installation of the Fan Assy (7GS,8GS,9GS,10GS) 32-51-00-720-003 Functional Test of the Nose Wheel Steering with the Handwheel 32-51-00-720-004 Functional Test of the Nose Wheel Steering with the Pedals 33-51-38-400-002 Installation of the Battery of the Emergency Power-Supply Unit 34-10-00-170-001 Flushing of the Principal Total Pressure Lines 34-10-00-170-002 Flushing of the Principal Static Pressure Lines 34-22-25-170-001 Draining and Flushing of the Standby Static and Standby Total Pressure lines (ISIS) 35-10-00-200-001 Inspection of Oxygen Pressure for the Flight Crew 35-12-41-710-001 Operational Test of the Full Face/Quick Donning Oxygen Masks (5757HM,5758HM,5759HM,5760HM) 35-30-00-210-004 Check Pressure on Portable Oxygen Cylinders Gauge 36-11-00-710-003 Operational Test of the Bleed Air System 38-13-00-710-001 Operational Test of the Quantity Indicating System 38-31-00-710-009 Operational Test of the Toilet Unit 38-32-00-710-002 Operational Test of the Waste/Water Drain System 49-11-11-400-001 Installation of the Auxiliary Power Unit (APU) - 4005KM (GTCP 36-300) 49-11-11-400-003 Installation of the Power Plant (APU) (APS 3200) 49-11-11-400-004 Installation of the Power Plant (APU) (131-9(A)) 49-20-00-600-001 Preservation / Storage / De-preservation of the Engine (GTCP 36-300) 49-20-00-600-002 Preservation/Storage/Return to Service of APU (APS 3200) 49-20-00-600-003 Preservation/Storage/Return to Service of APU (131-9(A)) 51-74-11-300-001 Repair of Corroded Areas 53-59-00-210-001 Operational Check of Single Drain Pipe Aft of FR70 from Outside 54-50-00-200-001 General Visual Inspection of the Pylon Drain System 71-00-00-550-011 Depreservation of the Power Plant 71-00-00-710-012 Test No.3 : Idle Leak Check 71-00-00-710-012 Test No.3 : Idle Leak Check 71-00-00-710-018 Discontinued Start, Restart and Shutdown Procedures



71-00-00-710-043 Normal Engine Automatic Start Procedure 71-00-00-710-047 Normal Engine Manual Start Procedure 71-00-20-400-040 Installation of the Power Plant

3. Job Set-up __________

Subtask 10-30-00-941-053



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


Subtask 10-30-00-210-074


(1) 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 external skin of: - the passenger/crew doors - the cargo doors - the frame around the doors.


(g) the external handle of the passenger/crew doors

(h) the drains

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

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

3 In all other locations. _

(i) the toilet areas

(j) all steel parts for corrosion.

(2) If you find corrosion, remove it (Ref. TASK 51-74-11-300-001).

(3) Make sure that: - the communication and navigation antennas are correctly installed - the static dischargers are correctly installed and in correct condition (Ref. TASK 23-61-00-200-001).

(4) Do a check of the avionics compartment.

Subtask 10-30-00-615-051


(1) 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).

Subtask 10-30-00-420-067

C. Aircraft Configuration

R (1) Install and connect the batteries 2PB1 and 2PB2 and make sure thatR the charge is correct (Ref. TASK 24-38-51-400-001).

R (2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).


R (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.


R

Subtask 10-30-00-554-053

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).

(2) Remove the protection from the cockpit, the passenger seats and the carpets.

Subtask 10-30-00-710-118

E. Inspection of the Doors

(1) Make sure that the doors open and close correctly.

Subtask 10-30-00-420-068

F. Installation of the Equipment Removed

(1) Install the Digital Flight Data Recorder (Ref. TASK 31-33-55-400- 002).

(2) Install the Cockpit Voice Recorder (Ref. TASK 23-71-35-400-001).

(3) Install the debris guard, the impeller and the shroud of the brake fans (Ref. TASK 32-48-51-400-005).

(4) Install the fire-extinguisher bottles and cartridges if removed of: - the cargo compartment (Ref. TASK 26-23-41-400-004) - the engines (Ref. TASK 26-21-41-400-004) - the APU (Ref. TASK 26-22-41-400-001).


(5) Install the batteries of: - the EPSU if removed (Ref. TASK 33-51-38-400-002) - the flashlights if removed and make sure that they operate correctly - the megaphones if removed and make sure that they operate correctly.

(6) Install the emergency locator beacon.

(7) Install the wiper blades (Ref. TASK 30-45-53-400-001) and the wiper arms (Ref. TASK 30-45-52-400-002), if removed.

(8) Do the reactivation of the rain repellent system (Ref. TASK 30-45-00- 440-002).

Subtask 10-30-00-170-050

G. Flushing of the Air Data System




Subtask 10-30-00-710-120

H. Inspection and Test of Fire Protection

(1) Engine fire protection

(a) Do a test of the engine fire-extinguishing system (Ref. TASK 26- 12-00-710-001).

(b) Do a check of the engine extinguishing distribution-piping (Ref. TASK 26-21-00-720-003).

(c) Do a check of the engine low-pressure indicating (Ref. TASK 26- 21-00-710-002).

(2) APU fire protection

(a) Do a test of the APU fire-extinguishing system (Ref. TASK 26-22- 00-710-001).


(b) Do a check of the APU extinguishing distribution-piping (Ref. TASK 26-22-00-210-001).

(c) Do a check of the APU low-pressure indicating (Ref. TASK 26-22- 00-710-003).

(3) Cargo-Compartment fire protection

(a) Do a test of the cargo-compartment fire-extinguishing system and low pressure indicating (Ref. TASK 26-23-00-710-001).

(b) Do a check of the cargo-compartment extinguishing distribution-piping (Ref. TASK 26-23-00-200-001).

(4) Lavatory fire protection

(a) Do a check of the fire extinguisher bottle pressure (Ref. TASK 26-25-00-200-005).

(5) Portable fire-extinguishing

(a) Do a check of all the portable fire-extinguishing bottles (Ref. TASK 26-24-00-210-001).

Subtask 10-30-00-710-121

J. Inspection and Test of the Oxygen System

(1) 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).

(b) Do a test of the full-face masks (Ref. TASK 35-12-41-710-001).

(2) Portable oxygen cylinders

(a) Do a check of the pressure of all portable oxygen cylinders (Ref. TASK 35-30-00-210-004).


Subtask 10-30-00-710-132

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).

(2) Do a test of the waste/water drain system (Ref. TASK 38-32-00-710- 002).

(3) Do a test of the toilet system (Ref. TASK 38-31-00-710-009).

Subtask 10-30-00-710-122

L. Protection of the fuel system


(2) If you find contamination, do a shock treatment: - if premixed fuel with biocide is available (Ref. TASK 28-11-00-600- 008), (Ref. TASK 28-11-00-600-009), (Ref. TASK 28-11-00-600-008) or (Ref. TASK 28-11-00-600-009). - if premixed fuel with biocide is not available (Ref. TASK 28-11-00- 600-008), (Ref. TASK 28-11-00-600-009), (Ref. TASK 28-11-00-600- 008) or (Ref. TASK 28-11-00-600-009).



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

(5) Do a test of the engine LP fuel shut-off valve (Ref. TASK 28-24-00- 710-002).

(6) Do a test of the APU shut-off valve (Ref. TASK 28-29-00-710-001).

(7) Do a test of the crossfeed valves (Ref. TASK 28-23-00-720-001).


Subtask 10-30-00-710-123

M. Inspection and Test of the Hydraulic System

(1) Do an analysis of the hydraulic fluid (Ref. TASK 12-32-29-281-001).

(2) Do a check of the fluid level in the hydraulic reservoirs (Ref. TASK 29-10-00-200-001).

(3) Do a test of the hydraulic shut-off valves (Ref. TASK 29-10-00-710- 001).

Subtask 10-30-00-710-124

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).

(2) Do an inspection of the main landing gear (Ref. TASK 32-11-00-200- 001).

(3) Lubricate all the landing gears: - lubrication of the NLG (Ref. TASK 12-22-32-640-002) - lubrication of the MLG (Ref. TASK 12-22-32-640-001).

(4) Do a test of: - the extension and retraction of the landing gear (Ref. TASK 32-31- 00-720-002) - the free-fall extension (Ref. TASK 32-33-00-720-001).

(5) Do a test of: - the nose wheel steering with the handwheel (Ref. TASK 32-51-00-720- 003) - the nose wheel steering with the rudder pedals (Ref. TASK 32-51-00- 720-004).

Subtask 10-30-00-710-125

P. Inspection and Operational Test of the Wheels and the Brakes

(1) If the aircraft was in storage with used tires:

(a) Install new tires on the nose landing gear (Ref. TASK 32-41-12- 400-001).


(b) Install new tires on the main landing gear (Ref. TASK 32-41-11- 400-006).

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

(d) If necessary, inflate the tires (Ref. TASK 12-14-32-614-001).

(2) If the aircraft was in storage with new 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) - for the main landing gear (Ref. TASK 32-41-11-000-006).

(b) Put the tires back to the nominal pressure (Ref. TASK 12-14-32- 614-001).

(c) Make sure that there are no cracks in the tires (Ref. TASK 32-41- 00-210-002).

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

Subtask 10-30-00-710-126

Q. Inspection and Test of the APU

(1) Install the APU, if removed: - for the GTCP 36-300 APU: (Ref. TASK 49-11-11-400-001) - for the APS 32000 APU: (Ref. TASK 49-11-11-400-003) - for the 131-9(A) APU: (Ref. TASK 49-11-11-400-004)

(2) Do the APU depreservation: - for the GTCP 36-300 APU: (Ref. TASK 49-20-00-600-001) - for the APS 32000 APU: (Ref. TASK 49-20-00-600-002) - for the 131-9(A) APU: (Ref. TASK 49-20-00-600-003)

Subtask 10-30-00-710-119

R. Inspection and Test of the Ventilation System

(1) Discard the recirculation filters (Ref. TASK 21-21-41-920-002).

(2) Do a test of the ventilation system of the avionics compartment (Ref. TASK 21-26-00-710-001) or (Ref. TASK 21-26-00-710-001).


(3) If the aft cargo-compartment ventilation system is installed, do a test of the aft cargo-compartment ventilation system (Ref. TASK 21- 28-00-720-004).

(4) If the FWD cargo-compartment ventilation system is installed, do a test of the FWD cargo-compartment ventilation system (Ref. TASK 21- 28-00-720-003).

Subtask 10-30-00-710-127

S. Inspection and Test of the Engine

(1) Install the engine if removed (Ref. TASK 71-00-20-400-040).

(2) Do the engine depreservation if it is not removed (Ref. TASK 71-00- 00-550-011).

(3) Do the depreservation of the IDG (Ref. TASK 24-21-00-600-040)

(4) Change the oil of the pneumatic starter (Ref. TASK 12-13-80-600-011) or (Ref. TASK 12-13-80-600-011).

(5) Start the engines, make them turn for one minute (Ref. TASK 71-00-00- 710-043) or (Ref. TASK 71-00-00-710-047).

(6) Do an engine run-up for the two engines (Ref. TASK 71-00-00-710-012) or (Ref. TASK 71-00-00-710-012).

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

(8) After shutdown, do a check of the engines for oil, hydraulic and fuel leakage.

Subtask 10-30-00-710-133

T. Test of the Bleed System

(1) Do a test of the bleed system (Ref. TASK 36-11-00-710-003).


Subtask 10-30-00-710-128

U. Protection of the Flight Controls

(1) Do the lubrication of: - the mechanical control chains of the THS (Ref. TASK 12-22-27-640- 007)R - the THS-actuator ball-screw nut (Ref. TASK 12-22-27-640-003) - the rudder bearings No. 6 (Ref. TASK 12-22-55-640-001)R - the trimmable-horizontal-stabilizer bearings and attachmentR fittings (Ref. TASK 12-22-53-640-001) - the roller bearings of the flap tracks (Ref. TASK 12-22-27-640-004) - the roller and the pinion bearings of the slat tracks (Ref. TASK 12-22-27-640-006) - all the spoiler servo-control bearings (Ref. TASK 12-22-27-640- 005).

R (2) Cleaning and protection of the flight control cables

R (a) If the aircraft storage period is less than 6 months, it is notR necessary to do a check of the rudder and THS cables.

R (b) If the aircraft storage period is more than 6 months, do a checkR of the rudder and THS cables in these areas:R - between FR71 and the THS actuator and the rear rudderR mechanical controlR - in the avionics compartment and the FWD and AFT cargoR compartments.

R 1 If there is corrosion on the cables or if there is no _R protection with SPECIAL MATERIALS (Material No. 05-005) orR COMMON GREASE (Material No. 04-004), clean and put protectionR along the full length of the cables (Ref. TASK 20-24-11-100- 001).

R (3) Do a detailed inspection of the flap transmission assembly (Ref. TASK 27-54-00-200-001).

(4) Do a detailed inspection of the slat transmission system (Ref. TASK 27-84-00-200-001).

(5) Drain and fill the flap rotary actuators (Ref. TASK 12-13-27-612- 005).

R (6) Do a check of the fluid level of the flap power-control-unit. IfR necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-002).


R (7) Do a check of the fluid level of the slat power-control-unit. IfR necessary, fill the PCU with oil (Ref. TASK 12-13-27-612-003).

(8) Do a test of the spoiler hydraulic control (Ref. TASK 27-64-00-710- 001).

(9) Do a test of the aileron and its hydraulic control (Ref. TASK 27-14- 00-710-001).

(10) Do a test of the elevator and its hydraulic control (Ref. TASK 27-34- 00-710-001).

(11) Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710- 002).

(12) Do a test of the flap and slat system (Ref. TASK 27-54-00-710-001). Operate the flap system a minimum of ten times.

Subtask 10-30-00-710-129

V. Tests of the Ice Protection Systems

(1) Do a test of the wing ice-protection system (Ref. TASK 30-11-00-710- 001).

(2) Do a test of the ice protection system of the air intakes (Ref. TASK 30-21-00-710-002).

Subtask 10-30-00-750-050

W. Set of the Clock

(1) Set the clock (Ref. TASK 31-21-00-750-002).

5. Close-up ________

Subtask 10-30-00-860-050



(2) Remove the warning notice(s).


Subtask 10-30-00-410-057

B. Close Access

(1) Make sure that the work area is clean and clear of tools and other items.



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Documents

highlights page

affected pages

revised procedure

c reason

change effectivity pages

axle stiffness mod

landing gear mlg

record of revisions