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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 52-41-13-220-050
A. Inspection (Ref. Fig. 601/TASK 52-41-13-991-002)
(1) Do a detailed inspection of the internal structure of the lateral right avionics-compartment access door 822.
(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 damage, 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 52-41-13-916-051
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 Right Avionics-Compartment Access Door 822 - Internal Structure Figure 601/TASK 52-41-13-991-002
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5. Close-up________
Subtask 52-41-13-865-054
R A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 46WV
Subtask 52-41-13-410-052
R B. Close Access
R (1) Close the lateral right avionics-compartment door 822 (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, AFT - REMOVAL/INSTALLATION
_______________________________________________________ TASK 52-41-14-000-001 Removal of the Avionics-Compartment Aft 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.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-41-14-991-001 Fig. 401
3. Job Set-up
__________ Subtask 52-41-14-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
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