5. Close-up
________ Subtask 53-41-00-370-052
A. Repair of the Surface Protection
(1) If necessary, repair the paint coatings in the inspection areas (Ref. TASK 51-75-12-300-003) or (Ref. TASK 51-75-12-300-001).
EFF : ALL 53-41-00Page B695
Nov 01/04
R
CES Subtask 53-41-00-410-084
B. Close Access
(1)
If necessary, install the air distribution riser-ducts at FR54 and FR56 (Ref. TASK 21-20-00-410-001)
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Install the insulation blankets (Ref. TASK 25-80-00-400-001).
(4)
Install the right upper sidewall panels 252PW, 252LW, 252HW (Ref. TASK 25-23-43-400-001) and the right lower sidewall panels 252NW, 252KW (Ref. TASK 25-23-44-400-001).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL 53-41-00Page B696
Nov 01/04
R
CES TASK 53-41-00-220-005
Special Detailed Inspection of Lower Skin of Longitudinal Lap Joint in Crack Stopper Areas at Stringer 32 LH and between FR47 and FR53, External Surface
1. Reason for the Job
__________________
Refer to the MPD TASK: 534116-02
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific abrasive cloth, grade 280 No specific warning notice 98D27803000000 1 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. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-55-11-000-003 Removal of the Sidewall Panels in the AFT Cargo Compartment - FR47/FR59 25-55-11-400-003 Installation of the Sidewall Panels in the AFT Cargo
Compartment - FR47/FR59 25-80-00-000-001 Removal of the Insulation Blankets 25-80-00-400-001 Installation of the Insulation Blankets 51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and
Composite Material
EFF : ALL 53-41-00Page B697
Nov 01/04
R
CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only) 53-35-13-000-001 Removal of the Belly Fairing Access Panels 53-35-13-000-002 Removal of the Quick-Release Access Panels from the
Belly Fairing Structure 53-35-13-400-001 Installation of the Belly Fairing Access Panels 53-35-13-400-002 Installation of the Quick-Release Access Panels on
the Belly Fairing Structure
ASRM 51-11-00-001
ASRM 51-22-00-001
NTM 534116-Part.6
ASRM 51-73-00-001 (for corrective action)
ASRM 51-74-00-001 (for corrective action)
ASRM 53-41-11-101 (for corrective action)
ASRM 53-41-11-201 (for corrective action)
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
53-41-00-991-025 Fig. 608
R **ON A/C 151-199, 401-499,
53-41-00-991-025-A Fig. 608A
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-41-00-860-054
A. Aircraft Maintenance Configuration
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 flap/slat 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 flaps. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FUSELAGE 机身3(55)
