B. Consumable Materials -------------------------------------------------------------------------------
REFERENCE ------------------ DESIGNATION-------------------------------------------------------------
R Material No. 02-003 F NSA 307110 TYPE 4
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
R Material No. 02-003A F NSA 307110 TYPE 4
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
R Material No. 02-003B F NSA 307-110 TYPE 4
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
Material No. 02-003C F NSA 307-110 TYPE IV
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
R Material No. 02-003D F NSA 307-110 TYPE IV
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
C. Expendable Parts
---------FIG.ITEM --------- ---------------------------------|DESIGNATION --------------------------------- -------------------------------------|IPC-CSN-------------------------------------
5 packing 32-31-03 10A-220
5 packing 32-31-03 10B-220
12 packing 32-31-03 15A-040
D. Referenced Information
------------------REFERENCE -------------------------------------------------------------DESIGNATION
-------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 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) R 32-00-00-860-001 Flight Configuration Precautions with Electrical R Power R 32-00-00-860-002 Ground Configuration after Flight Configuration with R Electrical Power
1EFF : ALL 1 32-31-36Page 407 1 1 Feb 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 32-31-00-720-002 Functional Test of the Normal Extension and
Retraction of the Landing Gear 51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound 32-31-36-991-001 Fig. 401
3. Job Set-up
__________
Subtask 32-31-36-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the PTU isolation coupling is disconnected (Ref. TASK 29-23-00-860-001).
(2)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002)
(3)
Make sure that the flight configuration precautions were obeyed (Ref. TASK 32-00-00-860-001).
(4)
Make sure that the Green hydraulic system is depressurized (Ref. TASK 29-10-00-864-001).
(5)
Make sure that the reservoir of the Green hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).
Subtask 32-31-36-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 121VU HYDRAULIC/G HYD/PUMP ENG1/CTL 1701GK R35 121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
1EFF : ALL 1 32-31-36Page 408 1 1 May 01/00R 1 1 1CES 1
Subtask 32-31-36-941-051
C. Make sure that the warning notices are in position to tell persons not to pressurize the Green hydraulic system: - on the panel 40VU in the cockpit, - on the ground service panel of the Green hydraulic system.
Subtask 32-31-36-560-050
D. Preparation for Installation
(1) Preparation of the check valve 2519GM.
(a) Remove the blanking plugs.
R R R R (b) Apply HYDRAULIC FLUIDS (Material No. 02-003), HYDRAULIC FLUIDS (Material No. 02-003A), HYDRAULIC FLUIDS (Material No. 02-003B), HYDRAULIC FLUIDS (Material No. 02-003C) or HYDRAULIC FLUIDS (Material No. 02-003D) to the threads of the check valve (13).
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