KitLog pro

Powered By Kitlog Pro v2.0

GA Aerospace’s Web Site
' style=
Date:  2-13-2019
Number of Hours:  5.25
Manual Reference:  
Brief Description:  12-03

02/05/19: 1.5Hrs
Step 1. The VS-1213 was placed onto the V-Stab assembly.
step 2 was worked on.

02/06/19: 1.75Hrs
2. Match-drilled #30 the holes from the VS-1201 into the V-stab tip fairing and clecoed.
3. The V-stab tip fairing was removed and the surface sanded.
4. The Vs-1213 was trimmed.
5. The rudder assembly was temporally attached to the V-stab assembly.

02/08/19: 1Hr
Worked on 6.

02/13/19: 1Hr
step 6. The VS-1213 V-stab tip fairing was placed in its correct position. The aft edge of the V -stab was marked in order to indicate any material that was within 1/8 of the rudder assembly. The fairing was removed and triom to the marked areas. The process was repeated untill 1/8 inn of clearence was reached.
' style=





' style=










Copyright © 2001-2024 Matronics. All Rights Reserved.