(3)
Install the floor panels 162GF, 162HF, 162KF and 162LF (Ref. TASK 53-42-17-400-001).
(4)
Install the sidewall panels 162BW and 162EW (Ref. TASK 25-55-11-400-001).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R EFF : 001-049, 051-099, 101-149, 221-221, 53-41-00Page 685 224-224, 228-228, May 01/05
CES **ON A/C ALL
TASK 53-41-00-210-027
Detailed Visual Inspection of Lower Skin of Longitudinal Lap Joints in Crack Stopper Areas at Stringer 6 LH/RH between FR47 and FR70, External Surface
1. Reason for the Job
__________________
Refer to the MPD TASK: 534102-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
No specific adjustable platform 5 m (16 ft. 5 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 53-41-11-101 (for corrective action) 53-41-00-991-002 Fig. 621
EFF : ALL
53-41-00Page 686
Feb 01/02
R
CES 3. Job Set-up
__________ Subtask 53-41-00-941-051
A. Get Access
(1) Put the adjustable platform in position. 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.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
4. Procedure
_________ (Ref. Fig. 621/TASK 53-41-00-991-002) Subtask 53-41-00-210-052
A. Inspection
(1) Examine the lap joint along STGR6 for cracks. NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the correct repair procedure.
5. Close-up
________ Subtask 53-41-00-942-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-41-00Page 687
Feb 01/02
R
CES
Lap Joint FR47 thru FR70 Figure 621/TASK 53-41-00-991-002
R EFF : ALL 53-41-00 Page 688 Feb 01/02
CES
R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
TASK 53-41-00-210-028
Detailed Visual Inspection of Fuselage Internal Structure around Bulk Cargo Door Cutout from FR59 to FR63 and between STGR23 and STGR38
1. Reason for the Job
__________________
Refer to the MPD TASK: 534164-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific lint-free cloth
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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)
R EFF : 001-049, 051-099, 101-149, 221-221, 53-41-00Page 689 224-224, 228-228, May 01/05
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(9)