Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (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 -------------------------------------------------------------------------------
cotter pin 27-54-44 01 -010
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-54-00-710-001 Operational Test of the Flap System
27-54-45-000-004 Removal of the Torque Shaft 6208CM(6258CM)
R 27-54-45-000-007 Removal of the Torque Shafts R 6214CM(6264CM)/6220CM(6270CM)
27-54-45-400-004 Installation of the Torque Shaft 6208CM(6258CM) R 27-54-45-400-007 Installation of the Torque Shafts R 6214CM(6264CM)/6220CM(6270CM)
27-54-44-991-001 Fig. 401 3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-54-44-991-001)
Subtask 27-54-44-941-054
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 landing-gear doors.
(3)
Make sure that the warning notice is on panel 114VU to tell persons not to operate the flap/slat controls.
Subtask 27-54-44-860-052
B. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is below the applicable torque shaft.
(2)
Make sure that the applicable torque shafts (1) are removed (Ref. TASK 27-54-45-000-004), (Ref. TASK 27-54-45-000-007):
-
FOR 6207CM
the torque shaft 6208CM
-
FOR 6257CM
the torque shaft 6258CM
-
FOR 6213CM
the torque shaft 6214CM
-
FOR 6263CM
the torque shaft 6264CM.
(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on panel 114VU.
(4)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on a flap torque-shaft outboard of the removed component (Ref. TASK 27-50-00-400-003).
1EFF : ALL 1 27-54-44Page 407 1 1 Aug 01/99R 1 1 1CES 1
Subtask 27-54-44-865-050
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
R -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure_________
(Ref. Fig. 401/TASK 27-54-44-991-001)
R R R R R R 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 27-54-44-420-054
A. Preparation for Installation
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) Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-004).
(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 27-54-44-420-052
B. Installation of the Steady Bearing Assembly
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