• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  (a) Apply the new erosion-protective tape SPECIAL MATERIALS (Material 
R  No. 05-065) to the leading edge surface (Ref. ASRM 51-75-12-001). 
R  (5) Application of the bonding and adhesive compound: 

R  (a) Wait 1 hour after you applied the erosion-protective tape before 
R  you do step (b). 
R  (b) Apply a layer of the BONDING AND ADHESIVE COMPOUNDS (Material No. 
R  08-017A) to the edges of the erosion-protective tape and the 
R  leading edge surface. 
R  NOTE : Refer to the manufacturers data for the time necessary for____ 
R  the bonding and adhesive compound to cure. 
R  NOTE : It is recommended that you apply the bonding and adhesive____ 
R  compound but it is not mandatory.
 5. Close-up________
 Subtask 55-32-11-942-053
 A. Close Access
 (1) Remove the access platform(s).
 (2) Remove the warning notice(s).

 

 Subtask 55-32-11-865-055

 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.


 VERTICAL STABILIZER TRAILING EDGE - DESCRIPTION AND OPERATION
_____________________________________________________________
 1.
 General

_______ The trailing-edge of the vertical stabilzer has four access panels installed on each side. The access panels are attached to the rudder hinge arms, the panel support frames and to flanges on the spar-box side shells.

 2.
 Component location

__________________
 (Ref. Fig. 001)


 3.
 Description


___________
 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,
 A. Trailing Edge Structure
 (1)
 The panel support frames are made of laminations of Carbon Fiber Reinforced Plastic (CFRP). They are attached to the rudder hinge arms.

 (2)
 The trailing-edge access panels are identified: 325BL, 325CL, 325DL, 325EL (left-hand side) and 325BR, 325CR, 325DR, 325ER (right-hand side). The access panels are made of Carbon Fiber Reinforced Plastic (CFRP) and Glass Fiber Reinforced Plastic (GFRP) laminations on a honeycomb core. The panels are attached to the flanges of the spar-box side shells as follows: access panels 325BL, 325BR, 325CL, 325CR and 325DL with piano hinges and screws; access panels 325DR, 325EL and 325ER with quick-release fasteners. Quick-release fasteners also attach the panels to the rudder hinge arms and to the panel support frames. Access panels 325CL and 325CR are only attached to the rudder hinge arms, panel support frames are not installed for these panels.

 (3)
 The hinged panels have a lever assembly so that you can safety the panels in the open position for maintenance practices.

 

R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 A. Trailing Edge Structure
 (1)
 The panel support frames are made of sheet metal. They are attached to the rudder hinge arms.

 (2)
 The trailing-edge access panels are identified: 325BL, 325CL, 325DL, 325EL (left-hand side) and 325BR, 325CR, 325DR, 325ER (right-hand side). The access panels are made of Carbon Fiber Reinforced Plastic (CFRP) and Glass Fiber Reinforced Plastic (GFRP) laminations on a honeycomb core. The panels are attached to the flanges of the spar-box side shells as follows: access panels 325BL, 325BR, 325CL, 325CR and 325DL with piano hinges and screws; access panels 325DR, 325EL and 325ER with quick-release fasteners. Quick-release fasteners also attach the panels to the rudder hinge arms and to the panel support frames. Access panels 325CL and 325CR are only attached to the rudder hinge arms, panel support frames are not installed for these panels.

 (3)
 The hinged panels have a lever assembly so that you can safety the panels in the open position for maintenance practices.

 


 Vertical - Stabilizer Trailing Edge
 Figure 001
 1EFF :  ALL  1  55-33-00 Page 2 
1  1  Feb 01/98
 1  1
 1CES  1

 

R 1EFF : 062-099, 106-149, 153-199, 205-299, 1 55-33-00Page 3 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 VERTICAL STABILIZER TRAILING EDGE - INSPECTION/CHECK


____________________________________________________
 TASK 55-33-00-200-001
 Inspection of the Vertical Stabilizer Trailing Edge Access-Panels for Missing Fasteners
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 
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 STABILIZERS 安定面(86)