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 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/
 6030CM(6080CM)
 27-84-45-000-012  Removal of the Torque Shaft 6034CM(6084CM)
 27-84-45-000-013  Removal of the Torque Shaft 6046CM(6096CM)
 27-84-45-400-007  Installation of the Torque Shafts
 6014CM(6064CM)/6028CM(6078CM)/6036CM
 (6086CM)/6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)
 /6044CM(6094CM)
 27-84-45-400-008  Installation of the Torque Shafts
 6016CM(6066CM)/6020CM(6070CM)/6026CM
 (6076CM)/6030CM(6080CM)
 27-84-45-400-013  Installation of the Torque Shaft 6034CM(6084CM)
 27-84-45-400-014  Installation of the Torque Shaft 6046CM(6096CM)
 27-84-48-000-001  Removal of the Type A Actuators
 6013CM(6063CM)/6015CM(6065CM)
 27-84-49-000-001  Removal of the Type B Actuators
 6027CM(6077CM)/6029CM(6079CM)/6035CM
 (6085CM)/6039CM(6089CM)/6045CM(6095CM)
 27-84-49-400-001  Installation of the Type B Actuators
 6027CM(6077CM)/6029CM(6079CM)/6035CM
 (6085CM)/6039CM(6089CM)/6045CM(6095CM)

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 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
31-32-00-860-006  Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page
 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,
 27-84-49-991-001 Fig. 401 R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 27-84-49-991-001-A  Fig. 401A
 **ON A/C ALL
 3. Job Set-up
__________
 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,

 (Ref. Fig. 401/TASK 27-84-49-991-001) R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-84-49-991-001-A)
 **ON A/C ALL

 Subtask 27-84-49-941-054
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notice(s) are in the cockpit to tell persons not to operate the slat controls.

 

 Subtask 27-84-49-860-052
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the slats are retracted fully (Ref. TASK 27-80-00-866-005).

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

 (3)
 Make sure that the adjustable access platform is below the applicable torque shaft.

 (4)
 Make sure that the applicable torque shaft (3) is removed (Ref. TASK 27-84-45-000-006): FOR 6027CM

 -
the torque shaft 6028CM
 FOR 6029CM

 -
the torque shaft 6028CM
 FOR 6035CM

 -
the torque shaft 6036CM
 FOR 6039CM

 -
the torque shaft 6038CM
 FOR 6045CM

 -
the torque shaft 6044CM
 FOR 6077CM

 -
the torque shaft 6078CM
 FOR 6079CM

 -
the torque shaft 6078CM
 FOR 6085CM

 -
the torque shaft 6086CM
 FOR 6089CM

 -
the torque shaft 6088CM
 FOR 6095CM

 -
the torque shaft 6094CM.

 

 (5)
 Make sure that the applicable torque shaft (6) is removed:

 (a) (Ref. TASK 27-84-45-000-007)
 FOR 6027CM

 -
the torque shaft 6026CM
 FOR 6029CM

 -
the torque shaft 6030CM
 FOR 6077CM

 -
the torque shaft 6076CM
 FOR 6079CM

 -
the torque shaft 6080CM.

 1EFF : ALL 1 27-84-49Page 412 1 1 May 01/04R 1 1 1CES 1

 (b) (Ref. TASK 27-84-45-000-012)
 FOR 6035CM

 -
the torque shaft 6034CM
 FOR 6085CM

 -
the torque shaft 6084CM.

 (c) (Ref. TASK 27-84-45-000-006)
 FOR 6039CM

 -
the torque shaft 6040CM
 FOR 6089CM

 -
the torque shaft 6090CM.

 (d) (Ref. TASK 27-84-45-000-013)
 FOR 6045CM

 -
the torque shaft 6046CM
 FOR 6095CM

 -
the torque shaft 6096CM.

 (6)
 If the two actuators (2) have been removed from the slat, make sure that the TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3) is installed in each pinion.
　
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