Hinge-Fitting of the Forward Cargo-Compartment Door, Fuselage and External
Attachment Area
Figure 607/TASK 53-21-00-991-003
EFF : ALL
53-21-00Page 641
May 01/05 R CES
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
Subtask 53-21-00-220-083
D. Inspection
(Ref. Fig. 607/TASK 53-21-00-991-003)
(1)
Do a detailed inspection of the structure along the full length of the hinge fitting and attachment rivets. This inspection is applicable on the open forward compartment door.
(2)
Make sure that there is no :
(a)
Corrosion damage :
-If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types of corrosion, inspection, removal and corrosion protection.
(b)
Other damage (cracks, scratches, stress, marks, dents, bumps,..) :
-If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
Subtask 53-21-00-916-068
E. Application of the Temporary Protection (limited to the inner side of the hinge fittings)
CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS.
_______ MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. -ON LUBRICATED SURFACES. -IN DRAIN VALVES OR OTHER ORIFICES. TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE.
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) on the equipment and fittings adjacent to the area.
EFF : ALL
53-21-00Page 642
May 01/05
R
CES
(2)
Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
(3)
Remove the masking tape or the masking paper.
5. Close-up
________ Subtask 53-21-00-410-088
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-004)
(3)
Remove the access platform(s).
EFF : ALL
53-21-00Page 643
May 01/05
R
CES TASK 53-21-00-200-004
Detailed Inspection of Forward Cargo Door Cutout Panels, Upper and Lower Corners, External Surface
1. Reason for the Job
__________________
Refer to the MPD TASK: 532137-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.00 m (9 ft. 10 in.)
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 -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump SRM 511100 P.Block 001 (for corrective action) SRM 512200 P.Block 001 (for corrective action) 53-21-00-991-004 Fig. 608
EFF : ALL
53-21-00Page 644
May 01/05
R
CES 3. Job Set-up
__________
Subtask 53-21-00-010-067
A. Aircraft Maintenance Configuration
(1) Put an access platform in position at the zone 825.
Subtask 53-21-00-110-057
B. Cleaning of the Structure
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
中國(guó)航空網(wǎng) m.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1(142)
