1. Does the seat frame of Exhibit B contain "a longitudinal
element engagable with the upper longitudinally extending
support of the chassis"? His Honour accepted Avion's
submission that the "longitudinal element" was supplied by a
hole at the front of the front transverse member of the seat
frame which was "engagable with" the chassis by a removable
threaded bolt or stud passed through the hole, as
illustrated by photographs f, g, h and i in Exhibit KHH6.
On the appeal, there was further debate as to whether by
this means the seat frame was truly "engagable with" the
chassis in the sense required by the claim. It will be
necessary to refer further to that aspect of the matter.
2. If the answer to issue 1 is "yes", is there engagement "to
prevent relative transverse displacement therebetween"? The
trial judge rejected the submission that in Exhibit B such
displacement was prevented, not as described in issue 1, but
by fins or wings forming part of the seat frame which
engaged the lugs, as described above when dealing with
integer "e". These fins or wings also appear in photograph
l in Exhibit KHH6.
3. If the submissions for the appellant are correct as to
matters 1 and 2, so that his Honour was in error,
nevertheless is there infringement by reason of the
application of the "pith and marrow" doctrine or the
reasoning of Menzies J. in the Commonwealth Industrial Gases
Case, supra?
4. Despite his findings on issues 2 and 3, the trial judge held
integer "f" was not present in Exhibit B. His Honour so
decided on the ground that the locking device relied on as
providing integer "f" also incorporated integer "g", and the
claim required not two but three separate mechanisms, as
integers "e", "f" and "g", for prevention of relative
movement between and disengagement of the chassis and seat
frame. Is this correct?