The inpector is looking for "FAA approved data" or existing "guidance"
to allow a return to service with this fix.
Without this we will need a new canopy.
I am not looking for "we've always done it that way" types of
responses.
Anybody got any formal documentation that would satisfy the FAA that
this repair is allowed?
Thanks,
--Jim
Lane
XF
Jim,
Page 3-19 in AC 43-13B addreses repair to plastics:
http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/list/AC%2043.13-1B/$FILE/Chapter%2003.pdf
Your mechanic should have a copy of this laying around the shop.
Seems to me on a small crack out of the line of sight stop drilling is
acceptable to the FAA.
Tony
-Not and A&P
Section 4 Paras 3-40 c and d (pg3-23) would seem to apply to an area
as described by the OP. More on PS-30 and Weld-On 40.
http://www.altuglasint.com/expert/data/236
Give 10 minutes for bubbles to rise out after mixing the two parts
together and before application. A real expert can make the crack all
but vanish with proper application, sanding and polishing. IMVHO, a
glued repair is also much stronger than a drill stopped crack.
http://www.rplastics.com/weldon40.html
Frank Whiteley
Not an A&P, but have repaired canopy cracks using both Acrifix 192 and
methylene chloride two-part kit (in the UK).
Lane
XF
Except when 43.13 conflicts with manufacturer's information which
becomes the prevailing approved data.
UH