** ON A/C ALL
29-32-12 PB 401 CONF 00 - PRESSURE SWITCH - SYSTEM - REMOVAL/INSTALLATION
TASK 29-32-12-000-001-A
Removal of the System Pressure Switch
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
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 : 1151GN
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
B.
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).
(Ref. 32-12-00-010-001-A).
System Pressure Switch of the Green and Yellow Hydraulic Systems SHEET 1
Print Date: July 05, 2018
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : CSN
Type : A318/A319/A320/A321
Rev. Date : May 01, 2018
29-32-12 PB 401 CONF 00 - PRESSURE
SWITCH - SYSTEM - REMOVAL/INSTALLATION
QTY DESIGNATION
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
1
CAP - BLANKING
1
CONTAINER - HYDRAULIC FLUID RESISTANT
AR PLUG - BLANKING
AR SAFETY CLIP - CIRCUIT BREAKER
2
WARNING NOTICE(S)
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)
Open the Main Gear Doors for Access
Manual : AMM
Selected applicability : 0054-0054
Page 1 of 19
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