After match-drilling the canopy and canopy frame holes, countersinking or dimpling as appropriate, the canopy went back on the canopy frame for riveting and final torquing of zones 1 and 2 (zone 3 will be torqued later). I also figured out an easy way to thread safety wire in the left rail of the canopy frame (for the canopy switch) - details below, and involve using sewing thread!
The next task is a dreaded step for many builders: the canopy's fiberglass fairing, which provides a transition from the aluminum canopy frame to the plexiglass canopy. Fortunately, I attended an EAA Sportair workshop titled "Fiberglass Techniques for RV Aircraft" led by Scott Vanderveen, who had us do a complete process for a mockup canopy fairing over the 2 day class (along with 2 other RV-relevant projects). Scott's method differs from Van's quite a bit; I've provided many of the steps below, but unless you already know how to work with fiberglass, I
highly recommend taking Scott's workshop. The major differences are: 1) the Van's-supplied templates to outline the fairing or cut the fiberglass pieces are not needed; 2) instead of cutting umpteen fiberglass pieces, some on the bias but most not, simply cut enough fiberglass
all on the bias (important!) for 4 strips of BID fiberglass, 2.5" wide; 3) a strong structural adhesive is used to bond the fiberglass to aluminum (epoxy doesn't adhere well to bare aluminum), 4) all filler and fiberglass layers are tinted, so the result is a deeper black than the Van's method that has only the first layer or so of fiberglass tinted; and, 5) the finishing layer is Aeropoxy light - a wonderful epoxy paste that is strong yet can be easily sanded and shaped (unlike epoxy/flox/micro). So far, I've completed half the process - i.e., up to the point right before the second application of dual-layer BID fiberglass. I've delineated each step with pictures, following these details from the past week:
- match-drilled #27 (w/reamer) all holes common to canopy and canopy frame; deburred holes; dimpled #27 holes in side skins; started prepping for interior paint
- painted interior of canopy frame assembly; deburred and machine-countersunk holes in canopy; separated seal retainers; cut notches in rear seal
- painted top of glare shield matte black; painted seal retainers gray; primed contact surface of canopy handles; installed safety wire (to eventually pull canopy latch switch wires, when avionics are installed)
- placed canopy back on canopy frame assembly; clecoed left side skin, loosely attached hardware on left side, and tried to “fish” 0.041” safety wire though the channel
- loosely attached screws/hardware on right side of canopy; riveted side skins to canopy; fished 0.041” safety wire through wire channel using thread and needlenose pliers; attached screws/hardware and seal retainers on aft part of canopy (tightened inboard 14 screws); fabricated and installed canopy wear strips
- separated and fit hinge covers; tightened screws in “zone 2” of canopy with my wife’s help; fabricated canopy clips
- riveted canopy clips to canopy frame assembly; sanded canopy (80 grit) and aluminum (220 grit); followed Scott Vanderveen’s canopy fiberglass transition, Day 1 (structural adhesive; flox/micro/tint epoxy fillet; 2 layer tinted BID fiberglass cut on bias, pre-preg)
- Day 2: sanded fiberglass (80 grit); brushed on thin layer of epoxy; used tinted dry micro/epoxy paste and a bondo spreader to form center fillet and fill some of the low spots
Final #27 drilling of the canopy and canopy frame: