Mark Byrne - Experimental Aircraft Builder's Log

DAVID'S WEB SITE


Date: 4-1-2016
Number of Hours: 6.00
Manual Reference: 14.2.F.3
Brief Description: PASSENGER SHOULDER HRNESS

1 DETERMIN THE LOCATION OF THE PASSENGER AND PILOTS SHOULDER HARNESS ATTACHMENT POINTS ON THE FUSALAGE. REF TO FIG 14.2.F.6 2 CUT A 3" HOLE AT THE CENTRE OF THIS LOCATION. CUT ONLY THE INNER SKIN OF THE FUSALAGE. 3 REMOVE AND CORE OUT THE AREA. 4 SURFACE PREP THE FUSALAGE IN THAT AREA USING 80 GRIT SANDPAPER. THOUGHLY CLEAN HE AREA. 5 RADIUS THE PERIMETER OF THE HOLE USING A NIX OF RESIN AND FLOX MIX. 6 AFTER CURING COVER THE INTERIOR OF THE HOLE WITH 2 BID (45.45) OF CARBON LAYUP EXTENDING 1" BEYOND THE HOLE. 7 ENSURE ALL AIR BUBBLES ARE WORKED OUT OF THE AREA. 8 ALLOW TO FULLY CURE. 9 USING A FLOX MIX BOND A FENOLIC BLOCK OF G10, 3/8 TO THE RESESEND AREA. 10 ALLOW TO FULLY CURE. 11 COCER THE DISC WITH A 2 BID (45.45) CARBON LAYUP. 12 APPLY PEEL PLY. AFTER CURING REMOVE THE PEL PLY. INSTALL THE REAL HARNESS INERTAIL REEL USING AN960-516) WASHERS AND AN365-524A) NUTS. 13 ALL LAP BELTS SECURE TO THE SEAT BELT BRACT ON THE SEAT FRAME.

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