(2)
Open the access door 312AR.
(3)
Get access to the inspection area.
(4)
Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and a lint-free cloth.
EFF : ALL
53-51-00Page 612
Feb 01/00
R
CES
4. Procedure
_________
(Ref. Fig. 603/TASK 53-51-00-991-005)
Subtask 53-51-00-210-057
A. Inspection:
R (1) Examine the ring frame at the circumferential joint of the rear R pressure-bulkhead skin at FR70 for:
-corrosion,
-cracks. R NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-51-16-001) for
____
the correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-051
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 53-51-00-410-057
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access door 312AR.
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-51-00Page 613
Circumferential Joint of the Rear Pressure-Bulkhead Skin
Figure 603/TASK 53-51-00-991-005
EFF : ALL
53-51-00Page 614
Feb 01/98
CES
TASK 53-51-00-210-004
Detailed Visual Inspection of Fuselage Skin at Horizontal Stabilizer Cutout at Forward Upper and Lower Corners LH/RH
1. Reason for the Job__________________
Refer to the MPD TASK: 535113-01
2. Job Set-up Information______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-005 Material No. 15-006 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-13-916-001 55-15-11-000-001 55-15-11-400-001 ASRM 535111000 53-51-00-991-003 Repair to a layer of Moisture-Removing OilRemoval of the Apron 333AT/333AB/343AT/343ABInstallation of the Apron 333AT/333AB/343AT/343AB(for corrective action)Fig. 604
3. Job Set-up__________
Subtask 53-51-00-010-056
A. Get Access
R R R R R R 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.
R (1) Remove the THS aprons (Ref. TASK 55-15-11-000-001).
EFF : ALL 53-51-00 Page 615 Feb 01/99
CES
4. Procedure
_________
(Ref. Fig. 604/TASK 53-51-00-991-003) Subtask 53-51-00-210-054
A. Inspection:
(1) Examine the fuselage skin at the THS forward corner cutouts for:
-cracks,
-skin distortion.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535111000) for the
____
correct repair procedure.
(2) 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).
5. Close-up
________ Subtask 53-51-00-410-055
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the THS aprons (Ref. TASK 55-15-11-400-001).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-51-00Page 616
Feb 01/99
R
CES
THS Forward Corner Cutouts
Figure 604/TASK 53-51-00-991-003
EFF : ALL 53-51-00 Page 617
Feb 01/98
CES
TASK 53-51-00-210-005
Detailed Visual Inspection of FR74, Splices at STGR12 and STGR19 LH/RH,
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(102)
