A320飞机维护手册 AMM STABILIZERS 安定面(79)

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R  A. Leading Edge Structure 
R R R R R R R  (1) The leading edge is divided into three sections to make replacement procedures easier. Each section is made of laminations of Glassfiber Reinforced Plastic (GFRP) over a honeycomb core. The fronts are made stronger to protect them against hail and bird impact damage. The outer surface has a coat of a special paint to prevent erosion. The sections are attached to the forward flanges of the side shells with countersunk screws. Ribs connect the sections to each other. 
R R R R R  (2) Each leading edge section has a hoisting point. Each hoisting point has a threaded sleeve, which is bonded into the section. When the hoisting points are not in use a plastic plug is fitted in the threaded sleave and the hoisting points are covered by a self adhesive disc which makes a smooth surface with the leading edge. 
R  **ON A/C ALL 
R  Post SB  55-1029 For A/C 051-099,
 A. Leading Edge Structure
 (1) The leading edge is divided into three sections to make replacement procedures easier. Each section is made of laminations of Glassfiber Reinforced Plastic (GFRP) over a honeycomb core. The fronts are made stronger to protect them against hail and bird impact damage. An erosion protection steel-cover is installed on the front of leading edge. The outer surface has a coat of a special paint to prevent erosion. The sections are attached to the forward flanges of the side shells with countersunk screws. Ribs connect the sections to each other.

 

R  Vertical Stabilizer Leading-Edge Figure 001
 1EFF : 1 1 1CES  ALL  1 111 55-32-00 Page 2 May 01/02

 

 (2) Each leading edge section has a hoisting point. Each hoisting point has a threaded sleeve, which is bonded into the section. When the hoisting points are not in use a plastic plug is fitted in the threaded sleave and the hoisting points are covered by a self adhesive disc which makes a smooth surface with the leading edge.

 LEADING EDGE - VERTICAL STABILIZER - REMOVAL/INSTALLATION
_________________________________________________________
 TASK 55-32-11-000-001
 Removal of the Vertical Stabilizer Leading-Edge
 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.
 CAUTION : MAKE SURE YOU DO NOT DAMAGE THE ANTENNA.

_______
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific access platform
 No specific circuit breaker(s) safety clip(s)
 No specific crane
 No specific warning notice
 98D55307531001 1 SLING - DORSAL FIN, LEADING EDGES, END CAP

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
29-00-00-864-001  Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action

R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 55-32-11-991-001-A  Fig. 401 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

**ON A/C 051-099,
 55-32-11-991-001 Fig. 401A

R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 55-32-11-991-003 Fig. 402
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 55-32-11-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------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 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
　
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