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Airbus A318 Instructions Manual

Airbus A318 Instructions Manual

Removal of the engine pump fire-valve
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** ON A/C ALL
TASK 29-11-52-000-001-A
Removal of the Engine Pump Fire-Valve
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN
CAUSE DAMAGE TO THE EQUIPMENT.
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS
POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
FIN : 1046GK
1.
Reason for the Job
Self explanatory
2
Job Set-up Information
A.
Fixtures, Tools, Test and Support Equipment
REFERENCE
No specific
No specific
No specific
No specific
No specific
No specific
No specific
B.
Consumable Materials
REFERENCE
(Material No. 14SBA1)
C. Work Zones and Access Panels
ZONE/ACCESS
574AB, 574BB
D. Referenced Information
REFERENCE
(Ref. 29-00-00-864-001-A).
Print Date: August 16, 2018
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
29-11-52-000-001-A - Removal of the Engine Pump Fire-Valve
QTY DESIGNATION
1
ACCESS PLATFORM 3M (10 FT)
AR CAP - BLANKING
1
CONTAINER 1 L (1/4 USGAL)
AR PLUG - BLANKING
AR SAFETY BARRIER(S)
AR SAFETY CLIP - CIRCUIT BREAKER
1
WARNING NOTICE(S)
DESIGNATION
Textile-Lint free Cotton -
ZONE DESCRIPTION
DESIGNATION
Put the Related Hydraulic System in the Depressurized Configuration
before Maintenance Action
Manual : AMM
Selected applicability : 0053-0053
Page 1 of 6

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Summary of Contents for Airbus A318

  • Page 1 574AB, 574BB D. Referenced Information REFERENCE DESIGNATION (Ref. 29-00-00-864-001-A). Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action Print Date: August 16, 2018 Page 1 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 2 ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Engine Pump Fire-Valve (1046GK) Print Date: August 16, 2018 Page 2 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 3 Figure 29-11-52-991-00100-00-A / SHEET 1/2 - Engine Pump Fire-Valve (1046GK) ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Print Date: August 16, 2018 Page 3 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 4 Figure 29-11-52-991-00100-00-A / SHEET 2/2 - Engine Pump Fire-Valve (1046GK) ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Print Date: August 16, 2018 Page 4 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 5 (4) Put a CONTAINER 1 L (1/4 USGAL) below the access door opening, to collect the hydraulic fluid. ** ON A/C ALL Procedure Print Date: August 16, 2018 Page 5 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 6: End Of Document

    (4) Compress the compensated slide (4) to decrease its length. Remove the engine pump fire-valve (5). (5) Put the PLUG-BLANKING in each disconnected line end. End of document Print Date: August 16, 2018 Page 6 of 6 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 7 (Material No. 14SBA1) Textile-Lint free Cotton - C. Work Zones and Access Panels ZONE/ACCESS ZONE DESCRIPTION 574AB, 574BB D. Referenced Information Print Date: August 16, 2018 Page 1 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 8 ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Engine Pump Fire-Valve (1046GK) Print Date: August 16, 2018 Page 2 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 9 Figure 29-11-52-991-00100-00-A / SHEET 1/2 - Engine Pump Fire-Valve (1046GK) ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Print Date: August 16, 2018 Page 3 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 10 Figure 29-11-52-991-00100-00-A / SHEET 2/2 - Engine Pump Fire-Valve (1046GK) ** ON A/C 0001-0004, 0007-0099, 0101-0107, 0109-0115, 0126-0199, 0204-0204, 0207-0207, 0209- 0249, 0251-0299, 0301-0399, 0401-0449, 0451-0470, 0501-0549, 0551-0559, 0601-0650, 0701-0749 Print Date: August 16, 2018 Page 4 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 11 (3) Make sure that the parts retained from the removed component are clean and in the correct condition. (4) Do an inspection of the component interfaces and the adjacent area. Print Date: August 16, 2018 Page 5 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 12 Depressurize the Hydraulic System WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. Print Date: August 16, 2018 Page 6 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 13 (4) Remove the access platform(s). (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items. End of document Print Date: August 16, 2018 Page 7 of 7 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

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