(b)
Install the cap (2) on the charging valve (3).
(c)
Loosen the body (4) and remove the charging valve (3) from the adapter (5).
(d)
Put blanking plugs in the open ports.
1EFF : ALL 1 32-44-13Page 404 1 1 Aug 01/05 1 1 1CES 1
Charging Valve 2586GM Figure 401/TASK 32-44-13-991-001
1EFF : 1 1R 1CES ALL 1 11 1 32-44-13 Page 405 Aug 01/05
TASK 32-44-13-400-001 Installation of the Charging Valve 2586GM WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
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. WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific corrosion-resistant steel lockwire 0.8 mm (0.032 in.) dia.
1EFF : ALL 1 32-44-13Page 406 1 1 Aug 01/05R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-14-32-614-002 29-10-00-864-002 29-23-00-860-001 29-23-00-860-002 32-12-00-410-001 32-44-13-991-001 Nitrogen Filling of the Yellow Hydraulic System, Brake Pressure AccumulatorDepressurize the Yellow Hydraulic SystemDisconnection of the Isolation Coupling of the Power Transfer Unit (PTU)Connection of the Isolation Coupling of the Power Transfer Unit (PTU)Close the Main Gear Doors after AccessFig. 401
3. Job Set-up__________
Subtask 32-44-13-860-051
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 Yellow hydraulic system is depressurized (Ref. TASK 29-10-00-864-002).
Subtask 32-44-13-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R 49VU L/G/Y BRK/PRESS/IND 61GG C10
R **ON A/C 401-499,
R 49VU ABCU &/Y BRK/PRESS IND 61GG C10
1EFF : ALL 1 32-44-13Page 407 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R **ON A/C ALL
R 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY
R 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL
R 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL
R 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY
R 121VU HYDRAULIC/PARK BRK/CTL/STBY
R 121VU HYDRAULIC/PARK BRK/CTL/NORM
R 121VU HYDRAULIC/HYD POWER/Y
R 121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG
R 121VU HYDRAULIC/Y HYD/PUMP ENG2/CTL
R 123VU Y HYD/ELEC/PUMP
R 123VU Y HYD/ELEC/ELEC PUMP/NORM
Subtask 32-44-13-941-051
C. Safety Precautions
4GG M36 3GG M35 1GG M34 2GG M33 71GG N37 70GG N36 3803GX N30 3700GD Q37 3701GD Q36 3802GX AB06 3801GX AB03 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 LANDING GEAR 起落架7(129)
