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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump
20-23-21-911-001 Removal/Installation of the Bobbins from their
Housings and Installation of O-rings, Square Seals,
and Back-up Rings on the Bobbins
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
27-92-17-000-002 Removal of the Flight Control Pressure Switch (10CE3)
27-92-17-400-002 Installation of the Flight Control Pressure Switch
(10CE3)
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
29-00-00-910-002 Safety Procedures of the Hydraulic System
29-10-00-863-002 Pressurize the Yellow Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-13-32-000-001 Removal of the Pressure Relief Valve of the Yellow
Hydraulic System (3063GM)
29-13-32-400-001 Installation of the Pressure Relief Valve of the
Yellow Hydraulic System (3063GM)
29-13-34-000-001 Removal of the Fluid Sampling Valve of the Yellow
Hydraulic System (3187GM)
29-13-34-400-001 Installation of the Fluid Sampling Valve of the
Yellow Hydraulic System (3187GM)
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector
29-19-51-000-003 Removal of the Leakage-Measurement Solenoid Valve
(3150GP)
29-19-51-400-003 Installation of the Leakage-Measurement Solenoid
Valve (3150GP)
29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-23-00-860-002 Connection of the Isolation Coupling of the Power
Transfer Unit (PTU)
29-32-11-000-003 Removal of the Hydraulic Pressure Transducer (3065GN)
29-32-11-400-003 Installation of the Hydraulic Pressure Transducer
(3065GN)
29-32-12-000-003 Removal of the System Pressure Switch (3151GN)
29-32-12-400-003 Installation of the System Pressure Switch (3151GN)
31-60-00-860-001 EIS Start Procedure
1EFF : ALL 1 29-13-14Page 410 1 1 May 01/05R 1 1 1CES 1
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REFERENCE DESIGNATION
-------------------------------------------------------------------------------
31-60-00-860-002 EIS Stop Procedure
**ON A/C 001-049, 051-058, 101-101,
29-13-14-991-001 Fig. 401 R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
29-13-14-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 29-13-14-860-053
A. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1)
Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(3)
Make sure that the reservoir of the Yellow hydraulic system is depressurized. (Ref. TASK 29-14-00-614-001).
(4)
Make sure that the warning notices are in position to tell persons not to pressurize the Yellow hydraulic system:
-In the cockpit on the hydraulic section 40VU of the overhead panel,
-On the ground service panel of the Yellow hydraulic system.
(5)
Make sure that the access door 198CB is open.
(6)
Make sure that the access door 196BB is open.
(7)
Make sure that the isolation coupling of the Power Transfer Unit (PTU) is disconnected (Ref. TASK 29-23-00-860-001).
(8)
Make sure that the container is in position below the location of the HP manifold.
Subtask 29-13-14-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD/PRESS/XMTR 1841GN C11 121VU HYDRAULIC/SOL VALVES/G/Y/B/LEAK/TST 1881GP N35 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
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