• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:37来源:蓝天飞行翻译 作者:航空
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

12-11-28-650-003  Pressure Refuel with Automatic Control
 28-10-00-910-001  Safety Procedures When You Do Work in a Fuel Tank
 28-10-00-910-002  Access to the Fuel Tanks and the Work Areas
 28-25-00-650-001  Pressure Defuel
 28-25-00-650-003  To Drain Remaining Fuel from the Wing Tanks and the
 Center Tank
 28-25-00-869-001  Fuel Transfer
 57-27-11-000-001  Removal of the Access Panel (540AB, 540BB, 540CB,
 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB,
 640DB, 640EB, 640FB, 640GB)
 57-27-11-400-001  Installation of the Access Panel (540AB, 540BB,
 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB,
 640CB, 640DB, 640EB, 640FB, 640GB)
 NTM  57-21-39 PART 6
 ASRM 572100  (for corrective action)
 57-21-00-991-022  Fig. 620
 3. Job Set-up__________
 Subtask 57-21-00-941-070
 A. Safety Precautions

 WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
 (1)
 You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (3)
 Put warning notices in the cockpit to tell persons not to operate the flaps or slats.

 (4)
 Put the safety barriers in position.


 1EFF : ALL 1 57-21-00Page A609 1 1 Nov 01/04R 1 1 1CES 1


 Subtask 57-21-00-650-074

 B. Fuel Configuration
 (1)
 Defuel the applicable fuel tank (Ref. TASK 28-25-00-650-001).

 (2)
 Drain the remaining fuel from the applicable fuel tank (Ref. TASK 28-25-00-650-003).


 Subtask 57-21-00-010-064
 C. Get Access
 (1)
 Put the adjustable access platform below the applicable wing fuel tank, zone 540(640).

 (2)
 Remove the applicable access panels (Ref. TASK 57-27-11-000-001) and (Ref. TASK 28-10-00-910-002):

 -
for the left wing, remove 540CB, 540DB, 540EB, 540FB, 540GB

 -
for the right wing, remove 640CB, 640DB, 640EB, 640FB, 640GB.

 


 4. Procedure
_________ (Ref. Fig. 620/TASK 57-21-00-991-022) Subtask 57-21-00-110-069
 A. Preparation for Inspection
 (1) Use a clean MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026), to clean the lower surfaces of the bottom skin in the area of the access panel cutouts (rib bays 8-9, 9-10, 10-11, 11-12 and 12-13).
 Subtask 57-21-00-280-050
 B. Inspection
 (1) Do a special detailed inspection of the upper and lower surfaces of the bottom skin. Inspect the areas of the access panel cutouts (rib bays 8-9, 9-10, 10-11, 11-12 and 12-13) (Ref. NTM 57-21-39 PART 6).
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 572100) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
 1EFF : ALL 1 57-21-00Page A610 1 1 Nov 01/04R 1 1 1CES 1


 Outer Wing Bottom Skin Rib Bay Cutouts Figure 620/TASK 57-21-00-991-022
 1EFF : 1 1R 1CES  ALL  1 11 1 57-21-00 Page A611 Nov 01/04


 5. Close-up
________

 Subtask 57-21-00-410-064
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panels (Ref. TASK 57-27-11-400-001) and (Ref. TASK 28-10-00-910-002):


 -for the left wing, install 540CB, 540DB, 540EB, 540FB, 540GB
 -for the right wing, install 640CB, 640DB, 640EB, 640FB, 640GB. Subtask 57-21-00-650-075
 B. Fuel Configuration
 (1) Refuel (Ref. TASK 12-11-28-650-003), defuel (Ref. TASK 28-25-00-650-001) or transfer fuel (Ref. TASK 28-25-00-869-001) as necessary.
 Subtask 57-21-00-942-069
 C. Removal of Equipment
 (1)
 Remove the warning notice(s).

 (2)
 Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.

 (3)
 Remove the safety barriers.

 (4)
 Remove the access platform(s).

 (5)
 Remove the ground support and maintenance equipment, the special and


 standard tools and all other items. R


R  TASK 57-21-00-200-021 
R  Detailed Inspection of Outer Wing, Bottom Skin Lower Surfaces, around Access 
R  Door Cutouts in all Bays, between Ribs 13 and 27 
 
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 WINGS 机翼1(143)