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  container
 No specific  tie wraps
 No specific  warning notice
 No specific access platform 3.0 m (9 ft. 10 in.) R No specific 1 ACCESS PLATFORM 3M (10 FT) R No specific 1 CONTAINER 5 L(1 1/2 USGAL) R No specific 1 WARNING NOTICE
 No specific  Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) 98D27504005000 2 PIN RIGGING-FLAPS (TRACK 1)
R  98D27504006000 2 PIN RIGGING FLAPS 98D27504030001 3 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  lockwire, corrosion-resistant steel, dia. 0.8 mm
 (0.032 in.)
R Material No. 02-003  F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
 Material No. 04-018
 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
 Material No. 05-005 USA MIL-C-16173 GRADE II
 CORROSION PREVENTIVE (Ref. 20-31-00)

 Material No. 09-013  USA MIL-PRF-81733 TYPE I CLASS A
 CORROSION INHIBITING BRUSH CONSISTENCY
 (Ref. 20-31-00)

 Material No. 11-002  USA MIL-PRF-680
 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
 (Ref. 20-31-00)

 Material No. 16-003  F ASNB70720
 COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cotter pins  27-54-03 04 -050
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart
 20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
27-00-00-080-002  Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000) -------------------------------------------------------------------------------

REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) 27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001) 27-50-00-866-009 Retraction of the Flaps on the Ground 27-51-00-820-001 Manual Adjustment of the Position Pick-Off Units 27-54-00-710-001 Operational Test of the Flap System 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
 F/CTL Page
 32-12-00-010-001 Open the Main Gear Doors for Access
 32-12-00-410-001 Close the Main Gear Doors after Access
 27-54-51-991-001 Fig. 401
 27-54-51-991-002 Fig. 402

 3. Job Set-up
__________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-54-51-860-053
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the flaps are retracted to the 0 degree position (Ref. TASK 27-50-00-866-009).
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(136)