Closing Plates for Tracks 1 thru 12 - Detail and Location
Figure 402/TASK 27-84-69-991-001
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-84-69Page 405 1 1 May 01/05 1 1 1CES 1
Closing Plates for Tracks 1 thru 12 - Detail and Location
Figure 402A/TASK 27-84-69-991-001-A13 (SHEET 1)
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-69Page 406 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
Closing Plates for Tracks 1 thru 12 - Detail and Location
Figure 402A/TASK 27-84-69-991-001-A23 (SHEET 2)
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-69Page 407 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
Closing Plates for Tracks 1 thru 12 - Detail and Location
Figure 402A/TASK 27-84-69-991-001-A33 (SHEET 3)
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-84-69Page 408 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
-
the screws (4)
-
the closing plate (3).
1EFF : ALL 1 27-84-69Page 409 1 1 Feb 01/01R 1 1 1CES 1
TASK 27-84-69-400-001
Installation of the Closing Plates for the Slat Tracks 1 thru 12
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
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 pneumatic wrench No specific safety barriers No specific warning notice No specific adjustable access platform 4.0 m (13 ft. 1 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 07-003 ABRASION RESISTANT COATING (TEFLON POLYURET) (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 27-84-69Page 410 1 1 Feb 01/01R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-80-00-866-005 Retracting the Slats on the Ground
27-84-45-000-004 Removal of the Torque Shaft 6010CM(6060CM)
27-84-45-400-005 Installation of the Torque Shaft 6010CM(6060CM)
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-84-69-991-002 Fig. 403 R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-84-69-991-002-A Fig. 403A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-84-69-941-053
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in the cockpit to tell persons not to operate the slat controls.
Subtask 27-84-69-860-052
B. Aircraft Maintenance Configuration
(1)
Make sure the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is installed on the flap/slat control lever.
(2)
Make sure that the slats are fully retracted (Ref. TASK 27-80-00-866-005).
(3)
Make sure that the applicable torque shafts have been removed (Ref. TASK 27-84-45-000-004).
(4)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft (Ref. TASK 27-50-00-400-003).
(5)
Make sure that the ADAPTOR-DRIVE, SLAT (AND FLAP) is on the applicable gearbox.
(6)
Make sure that the adjustable access platform is in position below the applicable slat track.
Subtask 27-84-69-865-050
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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