(5)
 At the Nos. 5 and 6 slat tracks:

 (a)
 Remove and discard the cotter pins (23) from the nuts (32), (47),

 (55)
 and (56).

 (b)
 Loosen the nuts (32), (47), (55) and (56), but do not remove them.

 (c)
 Remove and discard the cotter pins (23) from the nuts (22), (24),

 (49)
 and (51).

 (d)
 Remove the items that follow:

 -
the nuts (22), (24), (49) and (51)

 -
the washers (21), (25), (48) and (50)

 -
the bolts (27), (30), (41) and (42)

 -
the bush (26).
 NOTE : The bush (26) is a part of the slat track and the slat

____
 track linkage assembly.

 (6) Lift the slat (30 kg (66.1386 lb)) from the slat tracks.
 (7) Move the slat with the hoist and lower it onto the support structure. **ON A/C ALL
 Subtask 27-84-64-942-050
 B. Removal of Equipment
 (1) If you are to install a new slat, remove the SLING-SLATS (Ref. TASK 27-80-00-000-001).
R 1EFF : ALL 1 27-84-64Page 411 1 1 May 01/04 1 1 1CES 1

 INTENTIONALLY BLANK

R 1 1

27-84-64Page 412
1 1 May 01/04 1 1 1CES 1 TASK 27-84-64-400-002

 Installation of the No. 2 Slat
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
 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 adjustable access platform No specific pneumatic wrench No specific safety barriers No specific warning notice No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804009001 1 SLING-SLATS 98D27804011000 1 BAR-TURNING 98D27804020000 1 BLOCK-SLAT GAPPING
 1EFF : ALL 1 27-84-64Page 413 1 1 Nov 01/03R 1 1 1CES 1

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
No specific lockwire, corrosion resistant steel 0.8 mm (0.032 in) dia Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 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. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
23 cotter pins  27-84-05 42A-077
 23 cotter pins  27-84-05 42T-077
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
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)-
R 24-42-00-861-001 Energize the Ground Service Network from the External
R  Power
R 24-42-00-862-001 De-energize the Ground Service Network Supplied from
R the External Power 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)

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-80-00-000-001 Removal of the Hoisting Sling 27-80-00-200-002 Check of the Permitted Aerodynamic Tolerances between
 the Slats 1 thru 5 27-80-00-400-001 Installation of the Hoisting Sling 27-80-00-866-004 Extending the Slats on the Ground 27-84-00-710-001 Operational Test of the Slat System 27-84-45-000-004 Removal of the Torque Shaft 6010CM(6060CM) 27-84-45-400-005 Installation of the Torque Shaft 6010CM(6060CM) 27-84-69-000-001 Removal of the Closing Plates for the Slat Tracks 1
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱8(127)