-COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (Ref. 20-31-00)

 C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R 23-61-41-400-001 Installation of the Static Discharger 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 55-44-11-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 55-44-11-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that hydraulic systems are depressurized
 (Ref. TASK 29-00-00-864-001).

 (2)
 Make sure that the access platform is in position at Zone 360.

 (3)
 Make sure that the warning notice is in position in the cockpit to tell persons not to operate the flight controls.

 Subtask 55-44-11-865-052
 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/SEC1/NORM/SPLY 21CE1 B08 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 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 4. Procedure_________
 Subtask 55-44-11-420-050
 A. Install the Rudder Tip (Ref. Fig. 401/TASK 55-44-11-991-001)
 (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
 (2) Clean the component interface and/or the adjacent area.
 (3) Do an inspection of the component interface and/or the adjacent area.
 (4) Make sure that the work area is clean and clear of tool(s) and other items.
 (5) Put the rudder tip (1) in position. 
R  (6) Apply the SEALANTS (Material No. 09-018) to the screws (5) and (6). 
R  (7) Install and TORQUE the screws (6) to between 0.15 and 0.25 m.daN (13.27 and 22.12 lbf.in). 
R  (8) Install the screws (5), the washers (4) and the nuts (3).
 (9) Install the static discharger (2) (Ref. TASK 23-61-41-400-001). 
R R  (10) Apply the SEALANTS (Material No. 09-016) around the rudder tip assembly.
 5. Close-up________
 Subtask 55-44-11-942-050
 A. Close Access
 (1) Remove the access platform(s).
 (2) Remove the warning notice(s).

 (3) Remove the ground support and maintenance equipment, the special and

 standard tools and all other items.
 Subtask 55-44-11-865-051
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 19CE1, 19CE2, 19CE3, 5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 21CE1, 21CE2, 21CE3, 22CE.

 RUDDER ATTACH FITTINGS - DESCRIPTION AND OPERATION
__________________________________________________
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM STABILIZERS 安定面(116)