• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:44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

R  right and left sides. 
R  (2) Make sure that there is no: 
R  (a) Corrosion damage: 
R  - If you find corrosion damage, refer to the Structural Repair 
R  Manual (Ref. SRM 512200,P.Block 001) for types, inspection, 
R  removal and corrosion protection.

 CES  CES


R  (b) Other damage (cracks, scratches, stress, marks, dents, 
R  bumps,...): 
R  - If you find other damage, refer to the Structural Repair Manual 
R  (Ref. SRM 511100,P.Block 001) for damage classification and 
R  corrective action. 
R  Subtask 53-11-00-916-073 
R  B. Application of the Temporary Protection 
R  CAUTION : DO NOT APPLY TEMPORARY PROTECTION ON THE OXYGEN SYSTEMS._______ 
R  MAKE SURE THAT THE TEMPORARY PROTECTION DOES NOT GET: 
R  -ON COMPOSITE PARTS, CONTROL CABLES, PULLEYS,TEFLON BEARINGS. 
R  -ON LUBRICATED SURFACES. 
R  -IN DRAIN VALVES OR OTHER ORIFICES. 
R  TEMPORARY PROTECTION ON OR IN THESE PARTS CAN CAUSE DAMAGE. 
R  (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS 
R  (Material No. 08-074) on the equipment and fitting adjacent to the 
R  area. 
R  (2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or 
R  STORAGE PRESERVATION (Material No. 15-006) to the inspection area. 
R  (3) Apply a layer of STORAGE PRESERVATION (Material No. 15-008) or 
R  STORAGE PRESERVATION (Material No. 15-007) to the inspection area. 
R  (4) Remove the masking tape or the masking paper. 
R  5. Close-up________ 
R  Subtask 53-11-00-420-067 
R  A. Installation of the component 
R  (1) Install the girt-bar fitting blanking-plates (Ref. TASK 52-11-31-400-
R  005). 
R  Subtask 53-11-00-410-104 
R  B. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
R  410-001).

 

R (3) Remove the access platform(s).

 

 PROTECTIVE SHIELDS - FR1 - REMOVAL/INSTALLATION
_______________________________________________
 TASK 53-11-41-000-001 Removal of the Protective Shields - FR1 CAUTION : DO NOT USE THE LOCALIZER ANTENNA AT THE BOTTOM OF THE RADOME AS A
_______ SUPPORT.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 3.5 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 53-15-11-010-001 Opening of the Radome 110AL 53-11-41-991-001 Fig. 401 53-11-41-991-002 Fig. 402
 3. Job Set-up
__________ Subtask 53-11-41-861-050
 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

 EFF : ALL


53-11-41Page 401


 Subtask 53-11-41-865-050
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU COM NAV/RADAR/1 5SQ1 K13
R **ON A/C 051-099,
R 121VU COM NAV/RADAR/2 5SQ2 K14 R **ON A/C ALL
 Subtask 53-11-41-010-050
 C. Get Access
 (1)
 Put an access platform in position below the radome in the zone 110.

 (2)
 Open the radome 110AL (Ref. TASK 53-15-11-010-001). WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35


_______
 KNOTS.

 NOTE : Two persons are necessary to open the radome.
____
 4. Procedure
_________
 Subtask 53-11-41-020-050

 A. Removal of the Protective Shields (Ref. Fig. 401/TASK 53-11-41-991-001, 402/TASK 53-11-41-991-002)
 
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1(87)