-
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 plastic spatula
No specific warning notices
No specific access platform 2.5 m (8 ft. 2 in.)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
(Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
-------------------------------------------------------------------------------
REFERENCE ------------------------ DESIGNATION-------------------------------------------------------
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 spherical bearing
1 spherical bearing
2 nut
2 nut
3 tab washer
3 tab washer
4 spherical bearing
4 spherical bearing
5 nut
5 nut
6 tab washer
6 tab washer
7 spherical bearing
7 spherical bearing
8 nut
8 nut
9 nut
9 nut
10 tab washer
10 tab washer
11 tab washer
11 tab washer
12 spherical bearing
12 spherical bearing
57-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-01057-42-21 02 -010A57-42-21 02A-010
1EFF : ALL 1 57-42-21Page 406 1 1 May 01/01R 1 1 1CES 1
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-84-00-710-001 Operational Test of the Slat System
27-84-63-000-001 Removal of the No. 1 Slat
27-84-63-400-002 Installation of the No. 1 Slat
57-42-21-991-001 Fig. 401
3. Job Set-up
__________
Subtask 57-42-21-941-051
A. Safety Precautions
R (1) Make sure warning notices are in position in the cockpit to tell R persons not to operate the flaps or slats.
(2) Make sure that the safety barriers are in position.
Subtask 57-42-21-860-050
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position below the applicable slat 1, zone 511(611).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is installed on the slat/flap control lever.
(3)
Make sure that the No. 1 slat has been removed (Ref. TASK 27-84-63-000-001).
Subtask 57-42-21-865-051
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
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