• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:43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

 1EFF : ALL 1 57-42-00Page 614 1 1 May 01/05R 1 1 1CES 1


 4. Procedure
_________ (Ref. Fig. 603/TASK 57-42-00-991-005) Subtask 57-42-00-110-060
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the area. Clean the slat 1 skin connection in the area of the lower girder at track ribs 1 thru 4.
 Subtask 57-42-00-280-050
 B. Inspection
 (1) Do a special detailed inspection of the slat 1 skin connections in the area of the lower girder (ribs 1 thru 4) (Ref. NTM 57-42-04 PART 9).
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
 5. Close-up
________ Subtask 57-42-00-865-059
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 57-42-00-860-054
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the access platform(s).

 (3)
 Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.

 (4)
 Fully retract the slats (Ref. TASK 27-80-00-866-005).


 1EFF : ALL 1 57-42-00Page 615 1 1 May 01/05R 1 1 1CES 1


 Details of the Slat 1 Skin Connection in the area of the Lower Girder (Ribs 1 thru 4) Figure 603/TASK 57-42-00-991-005- 12 (SHEET 1)


 Details of the Slat 1 Skin Connection in the area of the Lower Girder (Ribs 1 thru 4) Figure 603/TASK 57-42-00-991-005- 22 (SHEET 2)


 Subtask 57-42-00-942-059

 C. Removal of Equipment
 (1)
 Remove the warning notice(s).

 (2)
 Remove the safety barriers.

 (3)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 1EFF : ALL 1 57-42-00Page 618 1 1 May 01/05R 1 1 1CES 1

 TASK 57-42-00-200-006


 Detailed Visual Inspection of Slat 1 Trailing Edge, Lower Face, LH/RH
 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.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.

 1. Reason for the Job
__________________
 Refer to the MPD TASK: 574205-01
 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 safety barriers No specific warning notices No specific adjustable access platform 3.5 m (11 ft. 6 in.) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
 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)
 1EFF : ALL 1 57-42-00Page 619 1 1 May 01/05R 1 1 1CES 1


 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground 27-80-00-866-005 Retracting the Slats on the Ground ASRM 574000 (for corrective action) 57-42-00-991-006 Fig. 604
 3. Job Set-up
__________ Subtask 57-42-00-941-055
 A. Safety Precautions
 (1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
 (2) Put the safety barriers in position. Subtask 57-42-00-860-055
 B. Aircraft Maintenance Configuration
 (1)
 Fully extend the slats (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.

 (3)
 Put the adjustable access platform below the applicable wing leading edge at slat 1, zone 521 (621).
 
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3(28)