LIFT STRUT ATTACH BRACKET TO FUSELAGE
Kitfox™ AIRCRAFT MANUFACTURED BETWEEN Sept. 1.1992 AND Oct.
SKYSTAR AIRCRAFT CORPORATION.
has come to our attention that some lift struts, shipped between Sept. 1
and Oct. 16, 1992, have fuselage mounting brackets that may have an
improper gap between tabs, thus allowing the lift strut to fit too loose
on the fuselage tab. This excess play between the fuselage mounting tab
and the lift strut attach bracket, does not allow the castle nut to be
secured on the AN6-11 bolt with a full safety pin hole showing on the
bolt. There should be virtually no play between the fuselage mounting
tab and the lift strut bracket. The temptation would be to over torque
the AN6-11 bolt, to lessen the gap, but this would result in permanent
damage to the bolt.
appropriate lift strut bracket gap, prior to paint or powder coating,
should be 0.286”. Measure the thickness of the lift strut mounting tab
on the fuselage and compare it to the distance between the flanges of
the lift strut bracket. Typically, the lift strut bracket gap should be
no more than 0.01” wider than the thickness of the fuselage tab. There
should be little, if any, play between the lift strut and fuselage when
the typical, hardware store variety 3/8” fine thread cap bolt,
matching washer and nut, as a torquing lever, tighten the bolt and nut
down until the gap on the lift strut bracket is approximately 0.02”
less than the required distance, allowing for some “spring back”.
This should close the gap to the required distance and allow adequate
securement of the castle nut on the bolt. You may wish to repeat this
procedure in small increments until a good fit is established.
a safety factor, please discard these over torque bolts and nuts. These
bolts are not A/C quality. If you use AN, MS or NAS bolts for this
adjustment, please discard them also because the adjustment will require
a higher torque value than allowed for this hardware.
you any have questions about this bulletin or procedure, please call our
Technical Department, at (208) 466-1711 or by Fax; (208) 466-7194.