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REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
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REFERENCE  DESIGNATION
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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) 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 27-80-00-866-005 Retracting 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 thru 12 27-84-69-400-001 Installation of the Closing Plates for the Slat Tracks 1 thru 12 57-41-37-000-006 Removal of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) 57-41-37-400-006 Installation of the Access Panels 522FB(622FB), 522JB(622JB), 522KB(622KB), 522LB(622LB), 522NB(622NB), 522QB(622QB), 522SB(622SB), 522UB(622UB) 27-84-67-991-001 Fig. 401

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REFERENCE DESIGNATION
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**ON A/C 001-049, 051-061, 101-105, 201-203,
 27-84-67-991-002 Fig. 402 R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 27-84-67-991-002-A Fig. 402A
 **ON A/C ALL
 27-84-67-991-003 Fig. 403
 27-84-67-991-004 Fig. 404
 27-84-67-991-005-A Fig. 405

 3. Job Set-up
__________
 Subtask 27-84-67-941-051

 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 27-84-67-860-051
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the adjustable access platform is in position below the applicable zone 510(610):

 (2)
 Make sure that the applicable access panel has been removed (Ref. TASK 57-41-37-000-006):

 -
for the left wing, remove 522NB

 -
for the right wing, remove 622NB.

 (3)
 Make sure that the slats are extended fully (Ref. TASK 27-80-00-866-004).

 (4)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever on panel 114VU.

 (5)
 Make sure that the safety collar is removed from the circuit breakers 9CV and 11CV.

 (6)
 Make sure that the applicable torque shaft has been removed (Ref. TASK 27-84-45-000-004).

 (7)
 Make sure that the ADAPTOR-DRIVE, SLAT (AND FLAP) and a pneumatic wrench are on the applicable bevel gearbox.

 (8)
 Make sure that the slat closing plate has been removed (Ref. TASK 27-84-69-000-001).

 Subtask 27-84-67-865-053
 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/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-84-67-991-001)
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 (Ref. Fig. 402/TASK 27-84-67-991-002)
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
　
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