May 01/04
R
CES
Fuselage Internal Structure below Cabin Floor Panels, including Cabin Floor
Structure between FR36 and FR46
Figure 631/TASK 53-31-00-991-042
EFF : ALL 53-31-00Page A665 May 01/04 R CES
(4) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE
PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material No. 15-006) or equivalent to the fuselage internal structure below the cabin floor panels, including the cabin floor structure between FR36 and FR46.
5. Close-up________
Subtask 53-31-00-410-090
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Release and fold down the insulation blankets and attach them in their initial positions.
(3)
Install the cabin air supply ducts, removed to gain access to the cabin floor structure between FR36 and FR46 (Ref. TASK 21-20-00-410-001).
(4)
Install the lower sidewall panels between FR42 and FR46 (Ref. TASK 25-23-44-400-001).
(5)
Install the floor panels 241HF, 241GF, 241FF, 241EF, 242FF, 242GF, 242HF, 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF (Ref. TASK 53-32-12-400-002).
(6)
Install the equipment and furnishing, removed to get access to the cabin floor panels.
(7)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 53-31-00Page A666
May 01/04
R
CES TASK 53-31-00-210-032
General Visual Inspection of Pressure Bulkhead AFT Face at FR35 and Lower Skin of Pressure Deck Lower Surface between FR35 and FR36
1. Reason for the Job
__________________
Refer to the MPD TASK: 533153-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform No specific lint free cloth No specific warning notice 98D27803000000 2 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (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. 15-005A 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 -------------------------------------------------------------------------------
53-35-13-000-002 Removal of the Quick-Release Access Panels from the
Belly Fairing Structure 53-35-13-400-002 Installation of the Quick-Release Access Panels on
the Belly Fairing Structure ASRM 53-31-14-001 (for corrective action) ASRM 53-31-16-001 (for corrective action) 53-31-00-991-043 Fig. 632
3. Job Set-up
__________
Subtask 53-31-00-010-093
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.
(1)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the slat/flap control lever when working near the flaps/slats.
(2)
Put the warning notice on the slat/flap control lever to tell persons not to operate the slats.
(3)
Put the adjustable access platform in position.
(4)
Remove the quick-release panels (Ref. TASK 53-35-13-000-002):
-191BB and 191EB from the left side,
-192EB and 192FB from the right side.
4. Procedure
_________
(Ref. Fig. 632/TASK 53-31-00-991-043)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 53-31-00-210-081
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身2(84)
