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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
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R  B. Removal of the Component 
R  (1) Remove the captain/first officer seat (Ref. TASK 25-11-51-000-001). 
R  (2) Remove the third occupant seat (Ref. TASK 25-11-41-000-001). 
R  (3) Remove the cockpit carpet. 
R  (4) Remove the textile floor covering.
 4. Procedure_________
 Subtask 53-12-11-020-050
 A. Removal of the Panels from FR1 thru FR6 (Ref. Fig. 401/TASK 53-12-11-991-001, 402/TASK 53-12-11-991-002)
 (1) Remove the sealant from the screws.
 (2) Remove the screws (3).
 (3) Remove the panels (4).
 (4) Remove the screws (1).
 (5) Remove the floor panels (2).
 Subtask 53-12-11-020-051
 B. Removal of the Panels from FR6 thru FR12 (Ref. Fig. 401/TASK 53-12-11-991-001, 403/TASK 53-12-11-991-003)
 (1) Remove the screws (11).
 (2) Remove the panels (12).

 EFF : ALL

53-12-11Page 402


 Cockpit Floor Panels
 Figure 401/TASK 53-12-11-991-001
 EFF :  ALL  53-12-11 Page 403 
Feb 01/98
 CES 

 

 Floor Panels from FR1 thru FR6
 Figure 402/TASK 53-12-11-991-002
 EFF :  ALL  53-12-11 Page 404 
Feb 01/98
 CES 

 

R  Floor Panels from FR6 thru FR12 Figure 403/TASK 53-12-11-991-003
 EFF :  ALL  53-12-11 Page 405 Feb 01/01
 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)
 EFF : ALL

53-12-11Page 406


 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).
 EFF : ALL

53-12-11Page 407


 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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