A320飞机维护手册 AMM FUSELAGE 机身3(145)

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 53-58-11-991-012-A Fig. 406A
 **ON A/C ALL
 53-58-11-991-013 Fig. 407
 53-58-11-991-014 Fig. 408
 3. Job Set-up
__________
 Subtask 53-58-11-864-053
 A. Make sure that the Green, Yellow and Blue hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-864-003).
 Subtask 53-58-11-865-053
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU APU/FUEL/BLOW OFF/PUMP 2QC B14 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 49VU AIR BLEED/X FEED/VALVE/BAT 2HV D13 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 APU/FUEL/BLOW OFF/CTL 1QC K39 121VU APU/FIRE AND OVHT/DET/LOOP B 2WG L44 121VU APU/FIRE AND OVHT/DET/LOOP A 1WG L43 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 121VU APU/AUTO/EXTIG/GND/TEST 30WF L40
 EFF : ALL
53-58-11Page 434

 -------------------------------------------------------------------------------
PANEL  DESIGNATION  IDENT. LOCATION
 -------------------------------------------------------------------------------
R  121VU APU/FIRE/EXTIG/SQUIB/B 121VU APU/FIRE/EXTIG/SQUIB/A 121VU APU/FIRE/LP VALVE/NORM 121VU APU/FIRE/LP VALVE/STBY 121VU APU/FUEL/LP VALVE/CTL 121VU APU/FUEL/LP VALVE/SPLY 121VU APU/FUEL/PUMP/CTL 121VU AUTO FLT/RUDDER/TRIM/IND 121VU AUTO FLT/FAC2/28VDC 121VU AUTO FLT/FAC2/26VAC 121VU FLIGHT CONTROLS/SEC3/SPLY 121VU FLIGHT CONTROLS/SEC2/SPLY 121VU FLIGHT CONTROLS/THS ACTR/MOT3 121VU FLIGHT CONTROLS/THS ACTR/MOT1 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY  2WF 1WF 4WF 3WF 1QF 2QF 3QC 15CC 5CC2 14CC2 21CE3 21CE2 19CE3 19CE1 15CE2  L39L38M42M41M40M39M38M20M19M18Q19Q18Q17Q16R20 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 
R R R  122VU APU GEN/EGIU2/28VDC 122VU GEN2/EGIU2/28VDC 122VU ELEC/APU/GCU  26XU2 24XU2 6XS  Y31 Y30 Y25 
R  **ON A/C ALL 
R R  122VU LIGHTING/EXT LT/NAV1/AND LOGO/LT 122VU AIR BLEED/X FEED VALVE/NORM  1LA 1HV  T03 Z20
 Subtask 53-58-11-865-055
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------
PANEL  SERVICE  IDENT.  LOCATION
 -------------------------------------------------------------------------------
2001VU LIGHT APU  2LJ  D08 

 CES  CES  **ON A/C ALL

 Subtask 53-58-11-869-053
 D. Aircraft Maintenance Configuration
 (1) Make sure that the aircraft is in the same configuration as for the removal task.
 (2) Make sure that the warning notice is in position to tell persons not to move the flight controls.
 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.
 4. Procedure_________ 
R  (Ref. Fig. 401/TASK 53-58-11-991-008, 402/TASK 53-58-11-991-009) 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, 
R  (Ref. Fig. 403/TASK 53-58-11-991-010) 
R  **ON A/C 301-399, 
R  (Ref. Fig. 403A/TASK 53-58-11-991-010-A) 
R  **ON A/C ALL 
R  (Ref. Fig. 404/TASK 53-58-11-991-016, 405/TASK 53-58-11-991-011) 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
 (Ref. Fig. 406/TASK 53-58-11-991-012) 
R  **ON A/C 106-149, 211-299, 301-399, 401-499,
 (Ref. Fig. 406A/TASK 53-58-11-991-012-A) 

 

 (Ref. Fig. 407/TASK 53-58-11-991-013, 408/TASK 53-58-11-991-014) Subtask 53-58-11-210-059
 A. Preparation for Installation.
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Examine the fuselage to tail-cone seal (65).

 (4)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
 Subtask 53-58-11-420-052
 B. Installation
　
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