A320飞机维护手册 AMM Communications 通讯3(12)

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23-61-00-200-001 - Check Resistance of Tip to Retainer - Check Bonding
 of Retainer to Structure 23-61-41-000-001 Removal of the Static Discharger 23-61-41-400-001 Installation of the Static Discharger 23-61-42-991-002 Fig. 401 23-61-42-991-003 Fig. 402 23-61-42-991-004 Fig. 403 23-61-42-991-005 Fig. 404 23-61-42-991-006 Fig. 405
 3. Job Set-up
__________
 Subtask 23-61-42-941-052
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.

 Subtask 23-61-42-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
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 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 23-61-42-860-051
 C. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is in position below the applicable static discharge retainer.

 (2)
 Make sure that the applicable static discharger is removed (Ref. TASK 23-61-41-000-001).

 4. Procedure
_________
 Subtask 23-61-42-560-050
 A. Preparation for a Replacement Component
 (1)
 Preparation for replacement of the static discharger retainers zones 324 (Tailplane), 326 (Rudder). (Ref. Fig. 401/TASK 23-61-42-991-002)

 (a)
 Put the applicable static discharger retainer (2), (4) or (6) in the correct position on the aircraft structure.

 (b)
 Use a drill to make holes in the applicable static discharger retainer (2), (4) or (6). Make sure that the holes align with the related holes in the aircraft structure.

 

 (2)
 Preparation for replacement of the static discharger retainers zone 330 (340) (Trimmable Horizontal Stabilizer). (Ref. Fig. 401/TASK 23-61-42-991-002)

 (a)
 Put the applicable static discharger retainer (24), (27), (29) or

 (31) in the correct position on the aircraft structure.

 (b)
 Use a drill to make holes in the applicable static discharger retainer (24), (27), (29) or (31). Make sure that the holes align with the related holes in the aircraft structure.

 

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 (3)
 Preparation for replacement of the static discharger retainers zone 470 (480) (Engine Pylon). (Ref. Fig. 402/TASK 23-61-42-991-003)

 (a)
 Put the static discharger retainer (21) in the correct position on the aircraft structure.

 (b)
 Use a drill to make holes in the applicable static discharger retainer (21). Make sure that the holes align with the related holes in the aircraft structure.

 

 (4)
 Preparation for replacement of the static discharger retainers zone 531 (631), 532 (632), 533 (633) (Flap Track Fairings). (Ref. Fig. 402/TASK 23-61-42-991-003)

 (a)
 Put the static discharger retainer (17) in the correct position on the aircraft structure.

 (b)
 Use a drill to make holes in the applicable static discharger retainer (17). Make sure that the holes align with the related holes in the aircraft structure.

 

 (5)
 Preparation for replacement of the static discharger retainers zone 590 (690) (Ailerons). (Ref. Fig. 403/TASK 23-61-42-991-004)

 (a)
 Put the applicable static discharger retainer (10) or (14) in the correct position on the aircraft structure.

 (b)
 Use a drill to make holes in the applicable static discharger retainer (10) or (14). Make sure that the holes align with the related holes in the aircraft structure.

 

 (6)
 Preparation for replacement of the static discharger retainer zone 534 (634) (Wing-Tip). (Ref. Fig. 404/TASK 23-61-42-991-005)
　
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