R **ON A/C 001-049, 051-058, 101-101,
29-13-15-991-001-A Fig. 401 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
29-13-15-991-001-C Fig. 401A
**ON A/C 001-049, 051-061, 101-105, 151-152, 201-206,
Post SB 29-1094 For A/C 001-049,051-061,101-105,151-152,201-206,
29-13-15-991-002 Fig. 402
**ON A/C ALL
3. Job Set-up
__________
Subtask 29-13-15-860-053
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 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.
(3)
Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(4)
Make sure that the reservoir of the Yellow hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).
(5)
Make sure that the main doors of the main gear are open (Ref. TASK 32-12-00-010-001).
(6)
Make sure that the access platform is in position at the main doors of the main gear.
(7)
Make sure that the container is in position below the location of the PTU manifold.
(8)
Make sure that the isolation coupling of the Power Transfer Unit (PTU) is disconnected (Ref. TASK 29-23-00-860-001).
Subtask 29-13-15-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU HYDRAULIC/HYD POWER/Y 3803GX N30 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
4. Procedure
_________
**ON A/C 001-049, 051-058, 101-101,
(Ref. Fig. 401/TASK 29-13-15-991-001-A) R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 29-13-15-991-001-C)
**ON A/C 001-049, 051-058, 101-101,
Subtask 29-13-15-560-050-A
A. Preparation of the Replacement Component
(1)
Remove the components which are attached to the removed manifold (7) as follows:
(a)
Remove the PTU solenoid valve 3012GL (Ref. TASK 29-23-51-000-002).
(b)
Remove the priority valve 3064GM (Ref. TASK 29-13-33-000-001).
(c)
Remove the bobbins (9),(30) (Ref. TASK 20-23-21-911-001).
(d)
Remove and discard the following items from the bobbins:
-square section seals (10),(31),
-back-up rings (36), (37), (39), (40) and
-O-rings (35), (38).
(e)
Put the bobbins (9),(30) into plastic bags to keep them clean.
(f)
Remove the check valve 3093GM and discard the O-ring (23).
(g)
Remove the check valve 3094GM as follows:
(h)
Remove the coupling half (46) and discard the packing (47).
(i)
If necessary, remove the reducer (5) and discard the packing (52).
(j)
If necessary, remove the union (13) and discard the packing (53).
(k)
Install the blanking plugs on the open ports of the manifold (7).
(l)
Install the blanking plugs on all of the removed components.
(2)
Install the removed components on the replacement manifold (7) as follows:
(a)
Remove the blanking plugs from the manifold (7) and the components.
(b)
Lubricate the new O-rings and the threads of the components with HYDRAULIC FLUIDS (Material No. 02-003).
(c)
If removed, install the union (13) with a new packing (53).
(d)
TORQUE the union (13) to between 6.265 and 6.835 m.daN (46.20 and
50.40 lbf.ft).
(e)
If removed, install the reducer (5) with a new packing (52).
(f) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM HYDRAULIC POWER 液压3(117)
