KitLog pro

Powered By Kitlog Pro v2.0

GA Aerospace’s Web Site
' style=
Date:  3-19-2020
Number of Hours:  3.83
Manual Reference:  
Brief Description:  38iS/U-17

1: The stabilator cables (D & F) were routed aft using the previously set strings, then they were secured to the stabilator horns.
2: The routed cables were connected to the cables already in the fuselage by using the turnbuckles called out.
3: A weight was placed on the stabilator.
4: The cables were tightened enough to remove slack.
5: The weight from the stabilator was removed.
6: Our tow bar was used to hold the control sticks at a 10" distance from the panel base, then the turnbuckles were tightened until we ended up with around 40lbs of tension on each of the cables.
7: The tow bar was removed and the control sticks were moved to confirm the stabilator could move all the way through its travel and that the stops were reached.
' style=





' style=




' style=




' style=










Copyright © 2001-2024 Matronics. All Rights Reserved.