**ON A/C 001-049, 051-056,
 57-53-00-991-007 Fig. 606 
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
 57-53-00-991-007-A Fig. 606A 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 633 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 3. Job Set-up
__________ Subtask 57-53-00-941-056
 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 57-53-00-860-104
 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)
 Extend the flaps fully (Ref. TASK 27-50-00-866-008).
 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.
 **ON A/C 001-049, 051-056,
 Subtask 57-53-00-010-055
 C. Get Access
 (Ref. Fig. 606/TASK 57-53-00-991-007)
 (1)
 Put the access platform below the applicable wing trailing edge at flap track 3, zone 530 (630).
 (2)
 Remove the applicable access panels (Ref. TASK 57-55-11-000-001):
 -
for the left wing, remove 532AT, 532CB
 -
for the right wing, remove 632AT, 632CB.
 (3)
 Remove the applicable outboard flap leading-edge panel 2 (Ref. TASK 27-54-62-000-003).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 634 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
 Outboard Flap
 Figure 606/TASK 57-53-00-991-007
R 1EFF : 001-049, 051-056, 1 57-53-00Page 635 1 1 May 01/05 1 1 1CES 1
 **ON A/C 057-099, 101-105, 151-199, 201-214,
 Subtask 57-53-00-010-055-A
 C. Get Access
 (Ref. Fig. 606A/TASK 57-53-00-991-007-A)
 (1)
 Put the access platform below the applicable wing trailing edge at flap track 3, zone 530 (630).
 (2)
 Remove the applicable access panels (Ref. TASK 57-55-11-000-001):
 -
for the left wing, remove 532AT, 532CB
 -
for the right wing, remove 632AT, 632CB.
 (3)
 Remove and discard the covers from the applicable inspection holes.
R **ON A/C 106-149, 215-299, 401-499,
 Subtask 57-53-00-010-055-B
 C. Get Access
 (Ref. Fig. 606A/TASK 57-53-00-991-007-A)
 (1)
 Put the access platform below the applicable wing trailing edge at flap track 3, zone 530 (630).
 (2)
 Remove the applicable access panels (Ref. TASK 57-55-11-000-001):
 -
for the left wing, remove 532AT, 532CB
 -
for the right wing, remove 632AT, 632CB.
 (3)
 Remove and keep the rubber grommets from the applicable inspection holes.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-53-00-865-061
 D. 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 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page 636 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
 4. Procedure
_________
 **ON A/C 001-049, 051-056,
 (Ref. Fig. 606/TASK 57-53-00-991-007) 
R **ON A/C 057-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 606A/TASK 57-53-00-991-007-A) 
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-53-00-110-055
 A. Preparation for Inspection
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
 EDGE:
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
 
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4(76)