(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 32-44-13-420-050
B. Installation Charging Valve 2586GM
(1)
Remove the blanking plugs.
(2)
Install the charging valve (3) in the adapter (5).
1EFF : ALL 1 32-44-13Page 408 1 1 Aug 01/05 1 1 1CES 1
(3) TORQUE the body (4) to between 1.42 and 1.54 m.daN (10.47 and 11.35 lbf.ft).
WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,
_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
(4) Safety the body (4) with corrosion-resistant steel lockwire 0.8 mm
(0.032 in.) dia.
(5) Fill the accumulator (1) with nitrogen (Ref. TASK 12-14-32-614-002). Subtask 32-44-13-865-052
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3700GD, 3701GD, 3801GX, 3802GX, 3803GX, 1GG, 2GG, 3GG, 4GG, 61GG, 70GG, 71GG.
5. Close-up
________
(Ref. Fig. 401/TASK 32-44-13-991-001) Subtask 32-44-13-410-051
A. Close Access
(1)
Connect the PTU isolation coupling (Ref. TASK 29-23-00-860-002).
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
(5)
Close the right MLG door (Ref. TASK 32-12-00-410-001).
(6)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-44-13Page 409 1 1 Aug 01/05 1 1 1CES 1 GAGE - ACCUMULATOR PRESSURE (2585GM) - REMOVAL/INSTALLATION
___________________________________________________________
TASK 32-44-14-000-001
Removal of the Accumulator Pressure Gage 2585GM
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking plugs
No specific circuit breaker(s) safety clip(s)
No specific warning notices
No specific access platform 2 m (6 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU)
32-12-00-010-001 Open the Main Gear Doors for Access R 32-44-11-200-001 Check Nitrogen Charge Pressure On Parking/Emergency R Accumulator By Reading Gauge
32-44-14-991-001 Fig. 401
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3. Job Set-up__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
Subtask 32-44-14-860-050
A. Aircraft Maintenance Configuration
(1) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
(2) Push the pressure release button on the pressure relief valve 3067GM to depressurize the alternate brake system.
(3) Make sure that the pressure on the gauge 2585GM decreases to the fill pressure of the accumulator 2582GM (Ref. TASK 32-44-11-200-001).
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