EFF : ALL
53-51-00Page 607
Feb 01/99
(1)
Open the AFT cargo-compartment door (Ref. TASK 52-30-00-860-001) or (Ref. TASK 52-30-00-860-003).
(2)
Put an access platform in position below the cargo door.
(3)
Remove the partition 162DW (Ref. TASK 25-55-12-000-001). R
(4)
Clean the inspection area with CLEANING AGENTS (Material No. 11-003). R
4. Procedure
_________
(Ref. Fig. 602/TASK 53-51-00-991-004)
Subtask 53-51-00-210-055
A. Inspection:
(1) Examine the forward face of the rear pressure bulkhead below the cabin floor for corrosion.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535116000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-061
A. Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the inspection area (Ref. TASK 51-75-13-916-001).
Subtask 53-51-00-410-056
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the partition 162DW (Ref. TASK 25-55-12-400-001).
(3)
Remove the access platform(s).
(4)
Close the Aft cargo-compartment door (Ref. TASK 52-30-00-860-002) or (Ref. TASK 52-30-00-860-004).
EFF : ALL
53-51-00Page 608
Rear Pressure-Bulkhead Forward-Face below the Cabin Floor
Figure 602/TASK 53-51-00-991-004
EFF : ALL
53-51-00Page 609
Feb 01/98
CES
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF : ALL
53-51-00Page 610
TASK 53-51-00-210-003
Detailed Visual Inspection of the Ring Frame at the Circumferential Joint of the Rear Pressure Bulkhead Skin at FR70 AFT Face
1. Reason for the Job
__________________
Refer to the MPD TASK: 535107-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3 m (9 ft. 10 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-006 AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-13-916-001 Repair to a layer of Moisture-Removing Oil
ASRM 53-51-16-001 (for corrective action)
53-51-00-991-005 Fig. 603
EFF : ALL
53-51-00Page 611
3. Job Set-up
__________
Subtask 53-51-00-010-058
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
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.
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FUSELAGE 機(jī)身3(101)
