Treatment of the M-18 Tail section
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The tail section vertical spar bottom end is attached to the V-frame with
an AN-3 bolt. During ground operations with the engine idling, there are
considerable vibrations. These can eventually lead to this problem. A
hairline crack can develop between the bolt hole and the bottom of the
vertical spar. See AD 59-22-03.
At the next annual inspection, or whenever you get a chance, take a close
look at this area. Being aware of this problem, several Mite owners in the Los
Angeles area have developed a fix. Besides the normal procedure of
re-gluing the crack and maybe installing mahogany reinforcing plates on
both sides of the lower section of the spar, we manufacture a U-shaped
(actually more like a tapered U-bracket, since the bottom of the vertical
spar is tapered), wrap-around bracket of 4130 steel (see below).. Installing a vertical spar reinforcing bracket: Drawing of bracket assembly (oriented sideways for printing) Instructions: after the bracket is fabricated, remove the tail stinger or at least detach it enough to have working room for fitting the bracket to the fin lower spar. Otherwise it is a tight squeeze for one's hands to do the job properly. Good common sense should apply. Another word of advice: if the spar is found to be cracked, it should be repaired first, before installation of the bracket. Submitted by Tony Terrigno, N120C |
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