Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING SEALANT
 (Ref. 20-31-00)

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

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-007  AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (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. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-869-002 Table of the Maximum Permitted Resistance Values 20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage R and in the Wings (this does not include the tanks)-
27-84-49-000-001  Removal of the Type B Actuators
 6027CM(6077CM)/6029CM(6079CM)/6035CM
 (6085CM)/6039CM(6089CM)/6045CM(6095CM)

 27-84-49-000-002  Removal of the Type B Actuators
 6033CM(6083CM)/6037CM(6087CM)/6041CM (6091CM)

 27-84-49-400-001  Installation of the Type B Actuators
 6027CM(6077CM)/6029CM(6079CM)/6035CM
 (6085CM)/6039CM(6089CM)/6045CM(6095CM)

 27-84-49-400-002  Installation of the Type B Actuators
 6033CM(6083CM)/6037CM(6087CM)/ 6041CM(6091CM) 27-84-64-000-001 Removal of the No. 2 Slat 27-84-64-400-002 Installation of the No. 2 Slat 27-84-65-000-001 Removal of the No. 3 Slat 27-84-65-400-002 Installation of the No. 3 Slat 27-84-66-000-001 Removal of the No. 4 Slat 27-84-66-400-002 Installation of the No. 4 Slat 27-84-67-000-001 Removal of the No. 5 Slat 27-84-67-400-002 Installation of the No. 5 Slat 27-84-68-400-001 Installation of the Slat-Track Pinion Assembly 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

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 27-84-62-991-001 Fig. 401

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-84-62-991-002 Fig. 402
 **ON A/C 301-399,
 27-84-62-991-002-A Fig. 402A
 **ON A/C ALL
 27-84-62-991-003 Fig. 403
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 27-84-62-991-007 Fig. 404 R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 27-84-62-991-007-A Fig. 404A
 **ON A/C ALL
 27-84-62-991-017 Fig. 405 3. Job Set-up

__________
 Subtask 27-84-62-941-055
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 Make sure that the warning notice(s) is in the cockpit to tell persons not to operate the slat controls.

 (4)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever.

 Subtask 27-84-62-865-050
 B. 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
 Subtask 27-84-62-860-051
 C. Aircraft Maintenance Configuration
 (1)
 Make sure that the adjustable access platform is below the applicable zone 510 or 610.

 (2)
 Make sure that the applicable closing plates have been removed (Ref. TASK 27-84-69-000-001).

 (3)
 Make sure that the applicable slats have been removed:

 -
for the slat tracks 5 and 6 (Ref. TASK 27-84-64-000-001)

 -
for the slat tracks 7 and 8 (Ref. TASK 27-84-65-000-001)

 -
　
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