C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-41-00-010-002 52-41-00-410-002 SRM 511100 P.Block 001 SRM 512200 P.Block 001 52-41-12-991-002
3. Job Set-up
__________Open the Avionics Compartment Doors for AccessClose the Avionics Compartment Doors after Access(for corrective action)(for corrective action)Fig. 601
Subtask 52-41-12-010-051
A. Get Access
R (1) Put an access platform in position at zone 812.
R R (2) Open the lateral left avionics-compartment door 812 (Ref. TASK 52-41-00-010-002).
Subtask 52-41-12-865-053
R B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
Subtask 52-41-12-110-050
R C. Cleaning of the Structure
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.
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(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure_________
Subtask 52-41-12-220-050
A. Inspection (Ref. Fig. 601/TASK 52-41-12-991-002)
(1) Do a detailed inspection of the internal structure of the lateral left avionics-compartment access door 812.
(2) Make sure that there is no :
R R (a) Corrosion damage : - If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types of corrosion, inspection, removal and corrosion protection.
R R (b) Other damage (cracks, scratches, stress, marks, dents, bumps,...). - If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
Subtask 52-41-12-916-051
R B. Application of Temporary Protection
CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS._______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. -ON LUBRICATED SURFACES. -IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE.
R R (1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) on the equipment and fittings adjacent to the area.
R R (2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) on the inspection area.
(3) Remove the masking paper or the masking tape.
R Lateral Left Avionics-Compartment Access Door - Internal Structure Figure 601/TASK 52-41-12-991-002
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5. Close-up________
Subtask 52-41-12-865-054
R A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 46WV
Subtask 52-41-12-410-052
R B. Close Access
R (1) Close the lateral left avionics-compartment door 812 (Ref. TASK 52-41-00-410-002).
(2) Make sure that the work area is clean and clear of tool(s) and other items.
(3) Remove the access platform(s).
DOOR - AVIONICS COMPARTMENT, LATERAL RIGHT - REMOVAL/INSTALLATION
_________________________________________________________________ TASK 52-41-13-000-001 Removal of the Avionics-Compartment Lateral-Right Door
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 1.80 m (5 ft. 11 in.)
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