36g
There was a fair amount of discussion centred around arm '36g'. Can't say I followed it or why a piece should be rated according to a maximum inertial load as opposed to x N/mm^2. Sadly, the pathology may well provide the most clear evidence of forces. Can anyone tell me the rated strength of a fastened seat belt and how that relates to the strength of the seat fixing, and remind me of which recovered articles allowed the 'line of flight' BEA conclusion (ie is it in any doubt with respect to the whole airframe ?). Thanks.