pdf Gfa ad 029 Popular
By Tim Shirley Tagged in T61A, T61B, T61C, T61D 1001 downloads
gfa ad 029.pdf
![Gfa ad 029](http://doc.glidingaustralia.org/joomlatools-files/docman-images/generated/48aedb8880cab8c45637abc7493ecddd.jpg)
WELD CRACK INSPECTION ON LEFT WING ROOT FITTINGS
Applicable to the Slingsby T61 Falke. This directive derives from Slingsby Technical Instruction No. 61 as a result of the discovery of cracks in the welds of the left wing root fitting of a small number of T61 powered sailplanes. Additional inspection required at the 25 hourly inspections and subsequent remedy of any damage found.