TASK 27-84-45-400-011
 Installation of the Torque Shaft 6024CM(6074CM)
 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
__________________
R R Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 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) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
 GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)

 Material No. 04-022  USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 11-026  GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)

 Material No. 15-007  AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R R R  27-50-00-000-003 27-50-00-400-003 27-80-00-866-004 27-80-00-866-005 27-84-00-710-001 57-41-37-000-003 57-41-37-000-004 57-41-37-400-002 57-41-37-400-003 27-84-45-991-001 27-84-45-991-002  Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Extending the Slats on the GroundRetracting the Slats on the GroundOperational Test of the Slat System Removal of the Access Panel 522AT(622AT) Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB) Installation of the Access Panel 522AT(622AT)Fig. 401Fig. 402
 3. Job Set-up__________
 (Ref. Fig. 401/TASK 27-84-45-991-001)
 Subtask 27-84-45-941-067
 A. Safety Precautions
 (1) Make sure that the safety barriers are in position.
 (2) Make sure that the warning notice is in position to tell persons not to operate the slat controls.

 Subtask 27-84-45-860-060
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the slats are extended fully (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on panel 114VU.

 (3)
 Make sure that the access platform is in position below the applicable zone 522(622).

R (4) Make sure that the applicable access panels have been removed R (Ref. TASK 57-41-37-000-003), (Ref. TASK 57-41-37-000-004):
 -
FOR 6024CM
 panels 522AT, 522AB, 521HB

 -
FOR 6074CM
 panels 622AT, 622AB, 621HB.

 (5) Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the removed component - on the torque shaft, outboard of the removed component.
 Subtask 27-84-45-865-084
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21

 4. Procedure
　
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