B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 08-052 USA MIL-T-23397 AND/OR L-T-80B
SELF ADHESIVEALUMINIUM TAPE (Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-50-00-866-009 Retraction of the Flaps on the Ground
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-55-00-991-007 Fig. 403
**ON A/C 301-399,
57-55-00-991-007-A Fig. 403A
**ON A/C ALL
3. Job Set-up
__________
Subtask 57-55-00-941-056
A. Safety Precautions
(1)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2)
Put the safety barriers in position.
Subtask 57-55-00-860-054
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
Subtask 57-55-00-865-062
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 57-55-00-010-051
D. Get Access
(1) Put the adjustable access platform below the applicable flap track 2, 3 or 4, zone 531(631), 532(632) or 533(633).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 403/TASK 57-55-00-991-007)
**ON A/C 301-399,
(Ref. Fig. 403A/TASK 57-55-00-991-007-A)
Flap-Track Fairing Seals on Flap-Tracks 2 thru 4 - Location and Detail
Figure 403/TASK 57-55-00-991-007
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-00Page 426 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Flap-Track Fairing Seals on Flap-Tracks 2 thru 4 - Location and Detail R Figure 403A/TASK 57-55-00-991-007-A
1EFF : 301-399, 1 57-55-00Page 427 1 1 Feb 01/05 1 1 1CES 1
R **ON A/C ALL
R Subtask 57-55-00-040-053
R A. Preparation of the Aircraft for Flight After Damage to the Flap-Track
R Fairing Seals
R CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______
R EDGE:
R - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
R - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
R - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY.
R INCORRECT INSTALLATION CAN CAUSE DAMAGE.
R (1) To repair damage to the movable fairing seals:
R NOTE : Be careful not to damage the adjacent structure when you____
R remove loose or damaged seal.
R (a) Cut and remove loose or damaged pieces of the seal.
R NOTE : No more than half the seal length on each fairing can be____
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