1EFF : ALL 1 57-26-00Page 660 1 1 May 01/04R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(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. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 cotter pin 57-51-33 02B-010 5 cotter pin 57-51-33 02C-010 R 5 cotter pin 57-51-33 02D-010
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and
4
ASRM 572600 (for corrective action)
57-26-00-991-010 Fig. 610
3. Job Set-up
__________
Subtask 57-26-00-941-059
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-26-00-866-060
B. Aircraft Maintenance Configuration
(1)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever.
Subtask 57-26-00-865-060
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-26-00-010-059
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(2)
Remove the applicable flap track fixed fairing access panels (Ref. TASK 57-55-11-000-001):
-
for flap track 2, remove 531AB, 531BB, 631AB, 631BB
-
for flap track 3, remove 532AB, 532BB, 632AB, 632BB
-
for flap track 4, remove 533AB, 533BB, 633AB, 633BB.
R **ON A/C 301-399,
R Subtask 57-26-00-010-059-A
R D. Get Access
R R (1) Put the access platform below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
R R R R R (2) Remove the applicable flap track fixed fairing access panels (Ref. TASK 57-55-11-000-004): - for flap track 2, remove 531CB, 531EB, 631CB, 631EB - for flap track 3, remove 532CB, 532EB, 632CB, 632EB - for flap track 4, remove 533CB, 533EB, 633CB, 633EB.
R **ON A/C ALL
4. Procedure_________
(Ref. Fig. 610/TASK 57-26-00-991-010)
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______ EDGE: - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS. - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS. - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 57-26-00-110-059
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