Each fuselage section consists of the external skin, internal circumferential frames, and longitudinal stiffening members (longerons and intercostals).

Reeds for looms, healds and heald-frames

Reeds for looms, healds and heald-frames

Reeds for looms, healds and heald-frames

Reeds for looms, healds and heald-frames

Reeds for looms, healds and heald-frames

Reeds for looms, healds and heald-frames

A trailer body includes left and right bottom rails and left and right top rails all parallel to each other.

A container has a platform (1) and a roof (2) , each incorporating side rails, respectively lower side rails (3) and upper side rails (4) , these rails being outwards opening channels.

Corner posts (5) interconnect the platform to the roof and the lower side rails to the upper side rails (4) .

The sideframe column bearing surfaces are permanent, and may be formed as part of the sideframe castings.

The frame has bays and comprise a front spar, a rear spar, and a number of spars located between the front and rear spars.

Reeds for looms, healds and heald-frames

The unit support frame (44) is suspended from the pair of side frames (64, 64) and is fastened to the pair of side frames (64, 64).

The support structure comprises a plurality of parallel spaced beams and a plurality of parallel spaced rails that are mounted approximately perpendicular to the beams.