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时间:2011-03-27 12:43来源:蓝天飞行翻译 作者:航空
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 (2)
 Remove the access platform(s).


 (3) Fully retract the slats (Ref. TASK 27-80-00-866-005). Subtask 57-43-00-942-053
 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.

 


 Details of the Slat 2 Skin Connections in the area of the Lower Girder (Track Ribs 5 and 6) Figure 602/TASK 57-43-00-991-002- 12 (SHEET 1)


 Details of the Slat 2 Skin Connections in the area of the Lower Girder (Track Ribs 5 and 6) Figure 602/TASK 57-43-00-991-002- 22 (SHEET 2)


 TASK 57-43-00-200-003
 Special Detailed Inspection of Slat 2 Skin Connections in Area of Lower Girder at Track Rib Stations, 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: 574304-02
 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.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)


 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

R  NTM 57-43-04 PARTS 6 and 9 ASRM 574000 (for corrective action) 57-43-00-991-003 Fig. 603
 3. Job Set-up
__________
 Subtask 57-43-00-941-052

 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 57-43-00-860-054

 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 slats (Ref. TASK 27-80-00-866-004).

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


R (3) Put the adjustable access platform below the applicable wing leading R edge at slat 2, zone 522(622).


 Subtask 57-43-00-865-054

 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 4. Procedure_________
 (Ref. Fig. 603/TASK 57-43-00-991-003)
 Subtask 57-43-00-110-052
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the slat 2 skin connection in the area of the lower girder at track ribs 5 and 6.
 Subtask 57-43-00-280-051 
R  B. Inspection 
R R R  (1) Do a special detailed inspection of the slat 2 skin connections in the area of the lower girder (ribs 5 and 6) (Ref. NTM 57-43-04 PARTS6 and 9). 
R R R R  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 57-43-00-865-055
 
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