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 -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft)
 1EFF : ALL 1 32-31-32Page 406 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-31-32Page 407 1 1 May 01/05 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 07-010  D  DA-4-653-91
 LACQUER OBSOLETE USE 16-047 (Ref. 20-31-00)
 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage 
R  and in the Wings (this does not include the tanks)-
24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 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
 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
 32-31-12-400-001  Installation of the L/G Selector Valve 40GA
 32-31-34-400-001  Installation of the L/G Door Selector Valve 41GA
 32-31-47-400-001  Installation of the Check Valve 2537GM
 51-75-13-916-002  Repair to a layer of Corrosion Preventive Compound
 32-31-32-991-001  Fig. 401

 3. Job Set-up
__________
 Subtask 32-31-32-860-051
 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 electrical circuits are de-energized (Ref. TASK 24-41-00-862-002)

 (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 32-31-32-865-051
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
　
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