Download Print this page
Airbus A318 Manual
Hide thumbs Also See for A318:

Advertisement

Quick Links

** ON A/C ALL
29-13-47 PB 401 CONF 00 - SLIDE - COMPENSATED - REMOVAL/INSTALLATION
TASK 29-13-47-000-001-A
Removal of the Compensated Slide
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 : 3010GM
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
B.
Work Zones and Access Panels
ZONE/ACCESS
674AB
C. Referenced Information
REFERENCE
(Ref. 29-00-00-864-001-A).
(Ref. 29-00-00-910-002-A).
(Ref. 29-14-00-614-001-A).
(Ref. 29-23-00-860-001-A).
Print Date: June 08, 2018
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
29-13-47 PB 401 CONF 00 - SLIDE - COMPENSATED - REMOVAL/INSTALLATION
QTY DESIGNATION
1
ACCESS PLATFORM 3M (10 FT)
1
CONTAINER 5 L (1.32 USGAL)
AR PLUG - BLANKING
AR SAFETY BARRIER(S)
AR WARNING NOTICE(S)
ZONE DESCRIPTION
DESIGNATION
Put the Related Hydraulic System in the Depressurized Configuration
before Maintenance Action
Safety Procedures of the Hydraulic System
Depressurization of the Hydraulic Reservoirs
Disconnection of the Isolation Coupling of the Power Transfer Unit
(PTU)
Manual : AMM
Selected applicability : 0059-0059
Page 1 of 9

Advertisement

loading
Need help?

Need help?

Do you have a question about the A318 and is the answer not in the manual?

Questions and answers

Subscribe to Our Youtube Channel

Summary of Contents for Airbus A318

  • Page 1 Safety Procedures of the Hydraulic System (Ref. 29-14-00-614-001-A). Depressurization of the Hydraulic Reservoirs (Ref. 29-23-00-860-001-A). Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) Print Date: June 08, 2018 Page 1 of 9 © 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 Compensated Slide SHEET 1 Print Date: June 08, 2018 Page 2 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 3 Figure 29-13-47-991-00100-00-A / SHEET 1/1 - Compensated Slide ** 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: June 08, 2018 Page 3 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 4 WARNING: DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO: - FLUSH IT AWAY WITH CLEAN WATER Print Date: June 08, 2018 Page 4 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 5 Non Aqueous Cleaner-General - - (Material No. 14SBA1) Textile-Lint free Cotton - C. Work Zones and Access Panels ZONE/ACCESS ZONE DESCRIPTION 674AB D. Referenced Information Print Date: June 08, 2018 Page 5 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 6 (4) Make sure that the ACCESS PLATFORM 3M (10 FT) is in position. (5) Make sure that the access panel 674AB is removed. Print Date: June 08, 2018 Page 6 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 7 (1) Connect the isolation coupling of the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860- 002) . Subtask 29-13-47-611-050-A D. Fill and Pressurize the Hydraulic Systems Print Date: June 08, 2018 Page 7 of 9 © 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 Figure 29-13-47-991-00100-00-A / SHEET 1/1 - Compensated Slide Print Date: June 08, 2018 Page 8 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
  • Page 9: End Of Document

    Selected applicability : 0059-0059 Rev. Date : May 01, 2018 29-13-47 PB 401 CONF 00 - SLIDE - COMPENSATED - REMOVAL/INSTALLATION End of document Print Date: June 08, 2018 Page 9 of 9 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

This manual is also suitable for:

A319A320A321