Page 5 - January 2019
P. 5

The fuel tank mounting brackets were installed on some
        of the spars late in the quarter.  This was required prior
        to similar brackets being attached to the tanks.  Once in
        place, the precise location of the fuel tank brackets will
        be determined relative to the spar bracket locations and
        the top wing skin. This process and the final fuel tank
        fitting into the wing structure, complete with location
        bolts and cushioning, will be completed before the wing
        is attached to the fuselage. (See “Fuel Tanks” below.)
        Undercarriage progress: Two boxes were constructed to
        precisely fit the main undercarriage openings in the wing.
        These will be used to confirm the mounting points for the
        undercarriage systems prior to ordering the metal work           The second engine mount strengthener
        and undercarriage components late in the coming                   installed on the inside of the fuselage
        quarter.

        Fuselage:
        The fuselage underside continued to receive finishing        Fuel Tanks:
        sanding, aided by the unit being rotated on its stand
        exposing the ‘other’ side. There was some surface            Inspection hatch openings were cut into the four
        sanding just ahead of the hatch openings during the          fuel tank lids and carbon fibre hatch covers were
        quarter preparing for the underside access hatch to be       also cut to fit.  In the future, the hatch covers will
        fitted in place in the coming quarter; other areas under     be cut to accept fuel and temperature gauges for
        the fuselage will receive final surface finishing – both     each tank.  The foam board was removed around
        these tasks to be completed before the fuselage is           each of these openings on the inside surface,
        ‘righted’ to allow joining the wing to the fuselage, most    smoothly shaped before two double layers of
        likely before our January 2019 year-end.                     fibreglass are applied for strength.  The hatches
                                                                     were pre-drilled for bolts every 1 ½” around the
        The second engine mount support was installed –
                                                                     perimeter and the nuts were riveted in place on
        another task required to be completed before the wing
                                                                     the inside of the hatch openings.
        can be mounted permanently on the fuselage.























             The “boss’ working up a sweat sanding the area in
                             front of the hatch                          Fuel tank inspection hatch complete and
                                                                              installed on the fuel tank tops
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