A. Put the aircraft back to its initial configuration.
 (1) Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

R (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-R 002).
 Subtask 32-42-34-410-050
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access door 811.

 (3)
 Remove the access platform(s).

 1EFF : ALL 1 32-42-34Page 408 1 1 May 01/05 1 1 1CES 1 SAFETY VALVE - NORM BRAKE - SERVICING

_____________________________________
 TASK 32-42-36-860-001
 Reactivation of the Normal-Brake Safety-Valve
 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 : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific bleed hose No specific safety barriers No specific warning notice No specific 1 l (1 US quart) container No specific access platform 2.5 m (8 ft. 2 in.) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft)
 1EFF : ALL 1 32-42-36Page 301 1 1 May 01/05R 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001  Installation of the Safety Devices on the Landing
 Gears 32-42-00-710-001 Operational Check of the Normal Braking System 32-42-00-870-001 Bleeding of the Normal Braking at the Brake Units
R **ON A/C 001-002, 051-052,
 32-42-36-991-002  Fig. 301
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 32-42-36-941-051
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 1EFF : ALL 1 32-42-36Page 302 1 1 May 01/05 1 1 1CES 11EFF : ALL 1 32-42-36Page 303 1 1 May 01/05 1 1 1CES 1

 (3) On the panel 400VU: - make sure that the landing-gear control-lever 6GA is in the DOWN position - put a warning notice in position to tell persons not to operate the landing gear.
 (4) Put a warning notice in the cockpit, to tell persons not to pressurize the Green hydraulic system.
 Subtask 32-42-36-860-058
 B. Aircraft Maintenance Configuration
 (1) Put the access platform in position below the applicable zone 731(741).
 (2) Put the 1 l (1 US quart) container in an applicable position below the normal-brake safety-valve to be removed.
 4. Procedure_________ 
R  **ON A/C 001-002, 051-052,
 (Ref. Fig. 301/TASK 32-42-36-991-002)
 Subtask 32-42-36-870-051 
R  A. Reactivation of the Normal-Brake Safety-Valve
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES._______
 WARNING : DO NOT LET OIL STAY ON YOUR SKIN FOR A LONG TIME AS IT CAN_______ CAUSE INJURY. 
R R R  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.
 CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT_______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
R  (1) Remove the dust cap (1) from the applicable normal-brake safety-valve. 
　
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