Subtask 57-41-00-865-067
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
 Subtask 57-41-00-860-065
 C. Aircraft Maintenance Configuration
 (1)
 Install the slat tracks 5 thru 12 (Ref. TASK 27-84-62-400-001).

 (2)
 Install the No. 2 slat (Ref. TASK 27-84-64-400-002), the No. 3 slat (Ref. TASK 27-84-65-400-002), the No. 4 slat (Ref. TASK 27-84-66-400-002) and the No. 5 slat (Ref. TASK 27-84-67-400-002).

 Subtask 57-41-00-942-060
 D. 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.

 TASK 57-41-00-200-014 
R R  Detailed Inspection of Outer Wing, Fixed Leading Edge, Bottom Attachment Joint on Track Rib 1 to 12
 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: 574106-01
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific No specific  circuit breaker(s) safety clip(s)safety barrierswarning noticesadjustable access platform 4.0 m (13 ft. 1 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  Material No. 11-026 Material No. 19-003  GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)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
 ASRM 574000 (for corrective action)

R 57-41-00-991-015 Fig. 613
 3. Job Set-up
__________
 Subtask 57-41-00-941-060

 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 57-41-00-860-066

 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 is installed on the flap/slat control lever.

 Subtask 57-41-00-865-068
 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

 Subtask 57-41-00-010-052
 D. Get Access
 (1)
 Put the adjustable access platform in position below the applicable wing leading edge, zones 521 (621)and 522 (622).

 (2)
 Remove the applicable access panels:

 -
for the left wing, 521AB, 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB

 -
for the right wing, 621AB, 621CB, 621EB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB.

 4. Procedure
_________
 (Ref. Fig. 613/TASK 57-41-00-991-015)
 Subtask 57-41-00-110-050
 A. Preparation for Inspection R
R (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING R AGENTS (Material No. 11-026) to clean the upper and lower surfaces of:
 -the bottom-attachment joint of the track ribs 1 thru 12.
 Subtask 57-41-00-210-063
 B. Inspection
 (1) Examine the upper and lower surfaces of the bottom-attachment joint area of the track ribs 1 thru 12. Make sure that:
 -
there is no corrosion
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼2(121)