• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:47来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (Ref. Fig. 624/TASK 53-21-00-991-027)

 (1)
 Do a detailed inspection of the cabin floor structure between FR24 and FR35.8. This inspection includes:

 -
the areas below and 0.5 m (1.64 ft.) around the galleys and the lavatories (if installed) and the emergency exit entrance,

 -
the seat tracks and cross beams.

 

 (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.
 EFF : 301-399, 53-21-00Page A651

May 01/05
R
 CES


 (b) Other damage (cracks, scratches, stress, marks, dents, bumps,...):
 -If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
 Subtask 53-21-00-916-058
 B. Application of the Temporary Protection
 (Ref. Fig. 624/TASK 53-21-00-991-027)

 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)
 Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) on the equipment and fittings adjacent to the area.

 (2)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) on the inspection area.

 (3)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-008) or STORAGE PRESERVATION (Material No. 15-007) on the inspection area.

 (4)
 Remove the masking tape or the masking paper.


 5. Close-up
________
 Subtask 53-21-00-410-074
 A. Close Access
 (1)
 Install the cabin floor panels from FR24 to FR35.8 (Ref. TASK 53-22-12-400-001).

 (2)
 Install the galleys, if removed (Ref. TASK 25-31-41-400-001) (Ref. TASK 25-31-41-400-002) (Ref. TASK 25-32-41-400-001).

 (3)
 Install the lavatories, if removed (Ref. TASK 25-41-41-400-001) (Ref. TASK 25-41-42-400-001) (Ref. TASK 25-42-41-400-001).

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.


 EFF : 301-399, 53-21-00Page A652

May 01/05
R
 CES


 (5)
 Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-

410-001).

 (6)
 Remove the access platform(s).


 EFF : 301-399, 53-21-00Page A653

May 01/05
R
 CES  TASK 53-21-00-200-025


 Special Detailed Inspection of Circumferential Joint at FR35.8, between Stringer 10LH and Stringer 10RH, External Side
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 532187-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 4 m (13 ft. 1 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 -------------------------------------------------------------------------------
51-75-12-300-001  Repair of Major Paint Damage on Light Alloy and
 Composite Material NTM 532186,P.Block-601 SRM 512300,P.Block-001 SRM 517500,P.Block-001 SRM 511100,P.Block 001 (for corrective action) SRM 512200,P.Block 001 (for corrective action) SRM 532111,P.Block 101 (for corrective action) SRM 533111,P.Block 101 (for corrective action) 53-21-00-991-043 Fig. 627
 EFF : 301-399,  53-21-00Page A654

May 01/05
R
 CES  3. Job Set-up


__________
 Subtask 53-21-00-941-071
 A. Get Access
 (1) Put an access platform in position at the zone 200.
 Subtask 53-21-00-110-078
 
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2(16)