1 REMOVE RUDER CONTROLACCESS PANEL AT THE VERTICAL STABILIZER
2 FROM THE INSIDE OF THE ACCESS , DRILL A 5/8 HOLE VERTICALLY THROUGH THE BOTTOM OF THE TIL ALONG THE CENTRLINE OF THE AIRCRAFT AND AS NEAR TH TAIL SPAR AS POSSIBLE
3 INSERT THE JACK POINT IN THE TAIL ( PART NUMBERR 218-0003)
4 VERIFY THE JACK POINT IS CERTICAL RELATIVE TO THE WATERLINE OF THE AIRCRAFT AND INSERT AS FAR AS POSSIBLE WITHOUT PROTRUDING PAST THE FUSELAGE EXTERIOR. ADJUST THE POSITION AS REQUIRED.
5 SET THE JACK POINT SO THE THREAD END IS FLUSH WITH OR SLIGHTLY INSIDE THE OUTER SURFACE OF THE FUSALAGE.
6 CUT A PHENOLIC OR G10 SPACER TO FILL THE GAP BETWEEN THE JACK POINT AND THE SPARE.
7 FLOX OR HYSOL THE JACK POINT AND THE SPACER INTO PLACE AGAINT THE VERTICAL SPAR.
8 AFTER FLOX OR HYSOL CURES, MATCH DRILL THE FOUR JACK POINT MOUNTING HOLES THROUGH THE TAIL SPAR.
