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Cockpit Floor Panels
Figure 401/TASK 53-12-11-991-001
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Feb 01/98
CES
Floor Panels from FR1 thru FR6
Figure 402/TASK 53-12-11-991-002
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Feb 01/98
CES
R Floor Panels from FR6 thru FR12 Figure 403/TASK 53-12-11-991-003
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CES
TASK 53-12-11-400-001
Installation 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 non metallic scraper R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 08-004 USA MIL-A-25457 ADHESIVE SEALANT (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 11-021 ADHESIVE REMOVER CARBON STRUCTURE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 25-11-41-400-001 Installation of the Third Occupant Seat 25-11-51-400-001 Installation of the Captain/First Officer Seat (3MS,
4MS)
52-10-00-010-001 Opening of the Passenger/Crew Door
53-12-00-300-001 Repair of the Damaged Area of the Adhesive Tape
53-12-11-991-001 Fig. 401
53-12-11-991-002 Fig. 402
53-12-11-991-003 Fig. 403
53-12-11-991-004 Fig. 404
3. Job Set-up
__________
Subtask 53-12-11-869-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position.
(2)
Make sure that the passenger/crew door is open (Ref. TASK 52-10-00-010-001).
Subtask 53-12-11-160-050
R B. Clean Component Interface and/or Adjacent Area
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.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Remove the adhesive of the old strips with CLEANING AGENTS (Material No. 11-021).
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Subtask 53-12-11-210-050
C. Inspection of the Component
(1) Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) Do an inspection of the component interface and/or the adjacent area.
(3) Make sure that the seal is in the correct condition.
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