Material No. 09-019 USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT
Material No. 11-026 Material No. 19-003 (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819
Material No. 19-010 LINT-FREE COTTON CLOTH (Ref. 20-31-00)USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
14 cotter pin 57-55-05 01 -060
14 cotter pin 57-55-05 01H-060
28 cotter pin 57-55-05 02 -020
50 cotter pin 57-55-05 04 -020
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)-
27-50-00-866-009 Retraction of the Flaps on the Ground
27-54-00-710-001 Operational Test of the Flap System
57-55-11-200-001 Check of the Flap Track Fairing Lateral Movement
57-55-11-991-023 Fig. 401
57-55-11-991-001 Fig. 402
57-55-11-991-002 Fig. 403
57-55-11-991-003 Fig. 404
57-55-11-991-004 Fig. 405
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3. Job Set-up
__________ Subtask 57-55-11-941-056
A. Safety Precautions
(1) Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flaps or slats.
(2) Make sure that the safety barriers are in position. Subtask 57-55-11-860-054
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is on the flap/slat control-lever.
(3)
Make sure that the adjustable access platform is in position below the applicable fairing at flap track 2, 3 or 4, zone 531(631), 532(632) or 533(633).
Subtask 57-55-11-865-053
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
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4. Procedure
_________
(Ref. Fig. 401/TASK 57-55-11-991-023, 402/TASK 57-55-11-991-001, 403/TASK
57-55-11-991-002, 404/TASK 57-55-11-991-003, 405/TASK 57-55-11-991-004) Subtask 57-55-11-420-072
A. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 57-55-11-420-050-A
B. Installation of the Flap Track Fairings
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(1) Install the applicable movable fairing as follows: WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME
_______ DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
NOTE : The weight of the fairing is approximately 18 kg (39.6831 lb).
____
(a)
Install the adjusters (42) and make sure that they are adjusted fully into their mountings.
(b)
Align the movable fairing at the forward pivot, then install the splined fittings (43).
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