Mid Fuselage skeleton assembly

Completed page 23-04.

All parts were prepared earlier

At step 8 (Insert the F-1234-L and -R Canopy Decks and F-1255-L and -R Longerons), the longerons are slightly misaligned with rollbar attach plate. Left longeron goes slightly inwards of the fuselage and the right one slightly outward.

I dont think hammering of the longeron more is good for it. I think I will use a bit of persuasion and force it to allign when I do match-drilling.

Completed page 23-05

Cutting the wing spar penetration hole with dremel tool turned out to be 20 minutes job

Completed step 1 on page 23-06


Spent 3 hours

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