the cutout valve (3).

 1EFF : ALL 1 32-33-12Page 405 1 1 Feb 01/98 1 1 1CES 1 TASK 32-33-12-400-001

 Installation of the L/G Free-Fall Cutout-Valve 2515GM
 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK AREA WHEN
_______ YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 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) No specific Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft) 98DNSA20208060 2 RIGGING PIN
 1EFF : ALL 1 32-33-12Page 406 1 1 Feb 01/98 1 1 1CES 1 B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Material No. 05-002 Material No. 07-010
C. Expendable Parts
corrosion-resistant steel lockwire 0.8 mm (0.032
 in.) dia.
USA MIL-P-8116
 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
D DA-4-653-91
 LACQUER OBSOLETE USE 16-047 (Ref. 20-31-00)

 -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
10  cotter pin  32-33-03 20 -050
 13  cotter pin  32-33-03 01 -170
 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001  Fill the Hydraulic Fluid Reservoir with a Hand Pump
 24-41-00-861-002  Energize the Aircraft Electrical Circuits 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)
 32-00-00-860-001  Flight Configuration Precautions
 32-00-00-860-002  Ground Configuration after Flight Configuration
 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
 32-33-00-720-001  Functional Test of the Free-Fall Extension
 51-75-13-916-002  Repair to a layer of Corrosion Preventive Compound
 32-33-12-991-001  Fig. 401

 1EFF : ALL 1 32-33-12Page 407 1 1 Feb 01/98 1 1 1CES 1 -------------------------------------------------------------------------------

REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
32-33-12-991-002 Fig. 402
 3. Job Set-up
__________
 Subtask 32-33-12-860-051
 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 aircraft electrical circuits are Energized (Ref. TASK 24-41-00-861-002)
　
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