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53-12-00Page 801
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door
53-12-11-000-001 Removal of the Cockpit Floor Panels from FR1 Thru
FR12
53-12-11-400-001 Installation of the Cockpit Floor Panels from FR1
thru FR12
53-12-12-000-001 Removal of the Cabin Floor Panels from FR12 thru FR24
53-12-12-400-001 Installation of the Cabin Floor Panels from FR12 thru
FR24
53-12-13-000-001 Removal of the avionics compartment floor panels
53-12-13-400-001 Installation of the avionics compartment floor panels
53-12-00-991-001 Fig. 801
3. Job Set-up__________
Subtask 53-12-00-941-050
A. Get Access
(1) Put the access platform in position.
(2) Open the passenger/crew door (Ref. TASK 52-10-00-010-001). Subtask 53-12-00-020-050
B. Removal of the Panel
(1) Remove the damaged panel (Ref. TASK 53-12-11-000-001) or (Ref. TASK 53-12-12-000-001) or (Ref. TASK 53-12-13-000-001).
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53-12-00Page 802
4. Procedure
_________
Subtask 53-12-00-350-050
A. Repair Procedure
(Ref. Fig. 801/TASK 53-12-00-991-001)
(1) Cut out the damaged area of the corrosion-protection adhesive tape of the floor panel edge.
R WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ R THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(2)
Clean and degrease the damaged area with CLEANING AGENTS (Material No. 11-003) or CLEANING AGENTS (Material No. 11-004).
(3)
Prepare BONDING AND ADHESIVE COMPOUNDS (Material No. 08-032) (1) for the cutout limits.
(4)
Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-032) (1) to the damaged area.
5. Close-up
________
Subtask 53-12-00-420-050
A. Installation of the Panel
(1) Install the repaired panel (Ref. TASK 53-12-11-400-001) or (Ref. TASK 53-12-12-400-001) or (Ref. TASK 53-12-13-400-001).
Subtask 53-12-00-942-050
B. Close Access
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Close the passenger/crew door (Ref. TASK 52-10-00-010-001).
(3)
Remove the access platform(s).
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53-12-00Page 803
Repair of the Damaged Area of the Adhesive Tape
Figure 801/TASK 53-12-00-991-001
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May 01/00
CES
PANELS - COCKPIT FLOOR - REMOVAL/INSTALLATION
_____________________________________________
TASK 53-12-11-000-001
Removal of the Cockpit Floor Panels from FR1 Thru FR12
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 3.50 m (11 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 25-11-41-000-001 Removal of the Third Occupant Seat 25-11-51-000-001 Removal of the Captain/First Officer Seat (3MS, 4MS) 52-10-00-010-001 Opening of the Passenger/Crew Door 53-12-11-991-001 Fig. 401 53-12-11-991-002 Fig. 402 53-12-11-991-003 Fig. 403
3. Job Set-up
__________
Subtask 53-12-11-941-050
A. Get Access R (1) Put the access platform in position.
(2) Open the passenger/crew door (Ref. TASK 52-10-00-010-001).
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53-12-11Page 401
Subtask 53-12-11-020-052
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