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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