VII.WING CONSTRUCTION
Be sureandprotect yourplans bycovering them
withbackingfrom a rollofMonoKote or a material
suchasclearfoodwrapping. Take a minuteto
studythe plans andunderstandthem. We suggest
buildinga rightandleftwingpanel, startingwith
the inboard sections, we'llstart withthe left
wing first.
1.From the 1/16"x 3"x 30"sheeting
provided, cut, fitandlocate over the
plans, the bottom leadingedge sheet (use
along straightedge to develop the correct
widthandto true-up the edges).From the
1/8"x 3/16"spruce sparstock provided,
measure andcut the required 15" length for
the bottom spar, setthisaside . Now cut
andlocate over the plans, the 1/4"x 1"
length ofshaped trailingedge stock.Next
cut andgluethe bottom center section
sheetinginplaceto thetrailingedge
stock andthe forward bottom wingsheet.
Cut, fitandglueinplacethesixbottom
1/16"x 3/16"cap stripsfrom thestock
provided. Usingoneof thedie-cutW-2
wingribsasa locationguide,the bottom
spruce spar (cutearlier)can now beglued
inplace. Lastly,note inthecross
sections thatthe leadingedge ofthe
bottom wingsheeting needsto beliftedup
andsupported inorder to match thebottom
contours ofthewingribs, forward ofthe
spar.Thisisbestdonewitha length of
trailingedgestock.
2.Note the "tick" marks justinfront ofand
just behind thewingpanel drawings.These
correspond to theriblocations. Use a
straightedge anda softlead pencilto
mark theriblocationsdirectlyonthe
leadingedge andcenter sectionsheeting.
Thefirstwingribto beinstalledisthe
firstW-2rib,inboard from the polyhedral
break (the inboard endofpolyhedralbrace
W-10willbutt againstthisribwhen itis
installed).Continuingto work inboard,
toward thecenter, installthe next three
U-2ribs.From theirdie-cutsheets,
remove plydihedralbraces W-8andW-9 and
polyhedralbraces w-10(balsa).The two
remaininginboard w-2ribsmust now becut
to compensate for the installationofthe
W-8 andW-9 dihedralbraces; usethese
braces asa thickness guideandtrimthe
ribsasshownonthe plans. Finally,root
ribW-1mustalso betrimmed intotwo
pieces to fitinfront ofandbehind the
dihedralbraces. Once thisisdone,
holdingW-8 inplaceagainasa guide,glue
alloftheremainingforward ribendsin
placeto thebottom leadingedge sheeting;
remove W-8from thestructure. UsingW-9
as a guide,glueallremainingrear rib
ends inplace andremove W-9 from the
structure.The remaining outboardW-2 rib
mustbetrimmed ina similarmanner. Using
the sameprocedure asdescribed, trimthis
ribinto a front andrear piece andgluein
place using W-10asa spacer;removeW-10
fromthe structure.
3.Cut.fitandglue the 1/4"sq.leading edge
in place.
4.Carefully removethisstructure fromyour
work surface. Use a sanding blockto
lightlysandthe outboard edges(the
polyhedral break) smooth. Placethe
structure back onthe plans andblockup
the center 2-1/2."Usingthesame
construction asdescribed earlier,the
outer wingpanel isnowbuiltdirectlyover
the plans anddirectlyto the inner panel.
Take pains to bevel the trailingedge butt
joint for a goodfit.Be sure to install
w-10firstbeforethe front andrear
segmentsofU-2,followed byW-3,W-4,etc.
5.Withallofthe ribs inplace, cut, fitand
gluethe top spruce spar inplace from W-7
tothe W-2 at the polyhedralbreak. From
yourparts bag, locate the bundle often
verticalgrainshear webs.Carefullytrim
oneofthese to fitbetween W-3andW-2and
againstthe spars andW-10withthe top
flushwiththe top ofthespar.Once
satisfied,gluethisweb inplace.
6.As shownonthe plans, the 1/4"sq.leading
edge must nowbesandeddown to matchthe
top contours oftheribs. The razor plane
then sanding blockwork greathere. Once
satisfied,cut, fitandglueinplacethe
top 1/16"leadingedge sheeting(notethat
thistop sheetingisplaced slightly
forward onthe top sparthus creatinga bit
ofa "shelf"). Lastly,cut, fitandglue
inplaceallofthetop 1/16"x 3/16"cap
stripswiththe exception oftheonewhich
willcover the W-2ribsat the polyhedral
break. Remove theleftwingpanel from
yourwork surface. Use your sanding block
to smooththe outboard face ofW-7in
preparationfor the wingtip.Inspect the
bottom polyhedral joint andlightlysandas
needed.
7.The rightwing structure is nowbuiltusing
the sameproceduresjustdescribed.
8.Next,therightandleftwinghalveswill
bejoined together. Preparationfor this
requires that the two inboard endsofthe
winghalvesbesandedsmooth andbeveled
to createa good,straightfit.Dothis
now.Pinorweightoneofthe winghalves
(let's usetheleft)flatto yourwork
surface. Next,make sure theribcurve in
the bottom leadingedge sheetingis
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