• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:52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

 Subtask 57-53-00-860-073
 C. Aircraft Configuration
 (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
 (2) Fully retract the flaps (Ref. TASK 27-50-00-866-009). Subtask 57-53-00-942-088
 D. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

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


 1EFF : 301-399, 1 57-53-00Page B634 1 1 Nov 01/04R 1 1 1CES 1


 TASK 57-53-00-210-008
 Detailed Visual Inspection of Outboard Double Slotted Flap, Tab Articulation at Track 4, 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: 575341-01
 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 spark-proof lamp No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 1EFF : 301-399, 1 57-53-00Page B635 1 1 Nov 01/04R 1 1 1CES 1


 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and
 4 ASRM 575300 (for corrective action) 57-53-00-991-039 Fig. 635
 3. Job Set-up
__________ Subtask 57-53-00-941-092
 A. Safety Precautions
 (1) Put a warning notice on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
 (2) Put the safety barriers in position. Subtask 57-53-00-860-074
 B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1)
 Fully extend the flaps (Ref. TASK 27-50-00-866-008).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.


 Subtask 57-53-00-865-131
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 1EFF : 301-399, 1 57-53-00Page B636 1 1 Nov 01/04R 1 1 1CES 1


 Subtask 57-53-00-010-086
 D. Get Access
 (1)
 Put the access platform in position below the flap track 4 at zone 587(687).

 (2)
 Remove the applicable flap track fairing (Ref. TASK 57-55-11-000-004):

 -
for the left wing, remove 533AT, 533CB

 -
for the right wing, remove 633AT, 633CB.

 

 (3)
 Put the spark-proof lamp adjacent to the inspection area.


 4. Procedure
_________
 (Ref. Fig. 635/TASK 57-53-00-991-039)
 Subtask 57-53-00-110-090
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the tab bracket, aft flap bracket, drive strut, tab forward link and tab rear link.
 Subtask 57-53-00-210-077
 
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5(24)