R **ON A/C ALL
R (Ref. Fig. 403/TASK 27-84-61-991-004) Subtask 27-84-61-020-054
A. Removal of the Side-Rollers - Slat Tracks 1 thru 4
(1) Remove and discard the lockwire from the applicable bolts (26). (2) Remove the bolts (26), the applicable side-rollers (25) and the shims (27).
TASK 27-84-61-400-003
Installation of the Side-Rollers - Slat Tracks 1 thru 4
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
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 external micrometer No specific safety barriers No specific warning notices 98D27804021000 1 GAUGE-SLAT TRACK SETTING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-024 AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT (Ref. 20-31-00)
1EFF : ALL 1 27-84-61Page 433 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-010 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 and in the Wings (this does not include the tanks)-
27-84-48-000-001 Removal of the Type A Actuators
6013CM(6063CM)/6015CM(6065CM)
27-84-48-400-001 Installation of the Type A Actuators
6013CM(6063CM)/6015CM(6065CM) 27-84-61-000-001 Removal of the Slat Tracks 1 thru 4 27-84-61-400-004 Installation of the Slat Tracks 1 thru 4 27-84-63-400-002 Installation of the No. 1 Slat 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-84-61-991-003-A Fig. 402
**ON A/C 301-399,
27-84-61-991-003 Fig. 402A
**ON A/C ALL
27-84-61-991-005 Fig. 405 3. Job Set-up
__________ Subtask 27-84-61-941-057
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 notices are in position.
(4)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed.
Subtask 27-84-61-860-055
B. Aircraft Maintenance Configuration
(1)
Make sure that the applicable access panels have been removed:
-
for the left wing, 521AB, 521BB, 521CB, 521EB
-
for the right wing, 621AB, 621BB, 621CB, 621EB.
(2)
For track 2 and 3, make sure that the applicable actuators have been removed (Ref. TASK 27-84-48-000-001).
(3)
Make sure that the applicable track has been removed (Ref. TASK 27-84-61-000-001).
Subtask 27-84-61-865-062
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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