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Aircraft Type: 

CTSW 2006 

LSA; LTF (BFU)

 

FLIGHT DESIGN

 

Trim Tab Spring Modification 

 

Page: 5

 

 

 

 
Rev. No.: 

Original Issue Date: 13.10.2006 
Revision  Date:         

Install telescopic guide with new spring 

 
The telescopic guide consists of two tubes with washer welded to one end of each, that 
slide one in the other. The telescope supports the new spring from inside and is itself 
guided by the 5mm diameter rod (pos. 5 in drawing 1). The parts are shown in picture 3. 
The new spring has 37 windings and a length of approx. 260mm (the old spring had 35 
windings). 
 

 

Picture 3 

 
To install the spring with telescopic guide, compress the spring and hold it in 
compressed state using safety wire or ty-raps. Carefully grease the outside of both 
telescopic tubes and the flanges, where the spring will have contact. This is to ensure 
smooth operation of the telescopic guide itself and of the spring guided by it, when 
installed. Insert the telescopic tubes to the pre-tensioned spring. Insert the 5mm 
diameter rod (pos. 5 in drawing 1) to the telescopic guide. 
 
Insert the telescopic system with spring and rod to the lower hole in the shear wall of the 
fin (same position than the old spring. Caution, do not use the upper hole / attachment 
area!) 
 
Snap the Angle Ball Joint to the Ball Head attached to the Rocker Arm. And secure the 
ball head with the safety pin. 
 
Release the spring by removing the safety wires or ty raps, whatever was used. Be 
careful to fully remove the complete safety wire or ty raps used as tool. 
 
Depending from the overall adjustment of the elevator the free length between the 
spring attachment points might vary for the indicidual plane. The telescope is designed 
as to deliver maximum possible guidance in the design operation point. If at your 
airplane the unlikely case happens and the telescope comes to a block when trimmed to 
max. fast speed, the inner tube of the telescope can be shortened carefully. In this case 
take care, that the cutting edges are properly deburred as to allow smooth operation of 
the telescope. 
 
Drawing 2 shows the new installation. 

 

Summary of Contents for CTSW-2006

Page 1: ...ication CTSW2006 THIS DOCUMENT AND THE TECHNICAL DATA HEREON DISCLOSED ARE PROPRIETARY TO FLIGHT DESIGN AND SHALL NOT BE USED RELEASED OR DISCLOSED IN WHOLE OR IN PART WITHOUT EXPRESS WRITTEN PERMISSI...

Page 2: ...No Original Issue Date 13 10 2006 Revision Date 1 Table of Contents 1 Table of Contents 2 2 Type of Maintenance 3 3 Minimum Level of Certification Required 3 4 General 3 5 Used drawings 3 6 New parts...

Page 3: ...responsible individual which has received Flight Design Airplane Operation Training 4 General Set the plane on parking brake and ensure good access to the tail of the aircraft Ensure only new self loc...

Page 4: ...int M5 pos 15 from the ball head screwed to the Rocker Arm pos 3 by moving it to the left side Attention the spring is under high force approx 250 N and releases to a length of approx 250 mm Drawing 1...

Page 5: ...to the pre tensioned spring Insert the 5mm diameter rod pos 5 in drawing 1 to the telescopic guide Insert the telescopic system with spring and rod to the lower hole in the shear wall of the fin same...

Page 6: ...HT DESIGN Trim Tab Spring Modification Page 6 Rev No Original Issue Date 13 10 2006 Revision Date Drawing 2 Check deflection angels of trim tab stabilator following the maintenance manual of the aircr...

Page 7: ...Date 13 10 2006 Revision Date 9 Revisions The Revisions pages are updated by Flight Design each time revision is issued They contain a list of all revisions made to the document since its original iss...

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