RUDDER MAIN STRUCTURE 55-41-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
ACCESS PANEL 55-42-13
REMOVAL/INSTALLATION 401 106-149, 159-199 211-299, 301-399 401-499,
Removal of the Access Panel 326CT 401 106-149, 159-199 at the Rudder Attach Fitting No. 7 211-299, 301-399 401-499,
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CHAPTER 55
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STABILIZERS
TABLE OF CONTENTS
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SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Installation of the Access Panel 405 106-149, 159-199 326CT at the Rudder Attach Fitting 211-299, 301-399 No. 7 401-499,
RUDDER FILLET FAIRING 55-43-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL RUDDER FILLET FAIRING - INSTL 55-43-19 REMOVAL/INSTALLATION 401 ALL Removal of the Rudder Fillet 401 ALL Fairing Preparation of the Rudder Fillet 405 ALL Fairing for Installation Installation of the Rudder Fillet 406 ALL Fairing
RUDDER TIP 55-44-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL RUDDER TIP 55-44-11 REMOVAL/INSTALLATION 401 ALL Removal of the Rudder Tip 401 ALL Installation of the Rudder Tip 404 ALL
RUDDER ATTACH FITTINGS 55-46-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Description 1 ALL Attach Fittings Location 1 ALL HINGE BEARING NO. 6 - RUDDER 55-46-11 REMOVAL/INSTALLATION 401 ALL Removal of Rudder Hinge Bearing 401 ALL No. 6 Installation of Rudder Hinge 405 ALL Bearing No.6
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STABILIZERS - GENERAL - DESCRIPTION AND OPERATION
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1.
General
_______ The tail assembly has a vertical stabilizer, a rudder assembly, a trimmable horizontal stabilizer and two elevator assemblies.
2.
Component Location
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(Ref. Fig. 001)
3.
Description
___________ The primary structural components of the stabilizers (spars, ribs and skin panels) are made of laminations of Carbon Fiber Reinforced Plastic (CFRP). All other components are made of the same material, or Glassfiber Reinforced Plastic (GFRP) or of light alloy. Three independant hydraulic systems control the rudder and the elevators. You can trim the horizontal stabilizer and the rudder. You can remove the stabilizers completely.
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Stabilizers
Figure 001
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HORIZONTAL STABILIZER - DESCRIPTION AND OPERATION
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1. General.
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A. Trimmable Horizontal Stabilizer (THS).
-The Trimmable Horizontal Stabilizer (THS) is installed to the fuselage tail section. It has the supporting structure for the left-hand (LH) and right-hand (RH) elevator.
2. Component Location
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-------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF. -------------------------------------------------------------------------------SPAR BOX 330/ 55-11-00 340 LEADING EDGE 330/ 55-12-00 340 TRAILING EDGE 330/ 55-13-00 340 TIPS 330/ 55-14-00 340 APRON 330/ 55-15-00 340 ATTACH FITTINGS 330/ 55-16-00 340
3. Description.
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(Ref. Fig. 001)
A. THS Description.
-The THS is installed in a large cut-out at the fuselage tail section. It is connected to the fuselage at three points. The connecting points are at the THS actuator and at the two hinge points on either side of the fuselage.
B. Primary Structural Components.
-The primary structural components of the THS are the LH and RH spar boxes and the center joint. All other components are attached to the LH and RH spar boxes.
C. Components.
-The other components are the leading edge, the trailing edge, the tips, the aprons and the attach fittings. Except for the attach fittings, you can remove all components for repair and/or maintenance.
Trimmable Horizontal Stabilizer
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