Date:	2-8-2016
Number of Hours:	6.00
Brief Description:	AFT ACK POINT
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. 9. INSTALL THE BOLTS, WSHERS AND LOCKNUTS.