My ex neighbor and very good long time friend spent his whole life as an passenger aircraft engineer
So got to fly, lucky him !
I don't...
But he now lives a few km's away but we see each other probably weekly for a chat and coffee. He's retired now
Lots of stuff/stories to tell then, lucky you
I don't think any of it's titanium but I'd need to look harder. Is titanium magnetic ?
Never had the opportunity/need to take a magnet to it, but as far as I am aware, not it isn't...
Hardly a metallurgist expert, just old school boy memories... but I though only ferrous materials could be magnetic ?...
I see that Wikipedia states that iron can be used in Titanium alloys... so maybe an iron doped Titanium could have some magnetic properties....
Still on Wikipedia, it does not say whetever Titanimum is "magnetic" or not. ather it states a "degree" of magnetic "susceptibility", whatever this means exactly.
So maybe it's not an all or nothing things, maybe metals are all magnetic, just to a varying degree...
Boy there is so much knowledge in this Wikipedia thing, one could spend his entire life reading about science and technical stuff.....
Some without a head have a hex inside the shaft so they can be held and tightened for the same side/position.
All "screw type" (Hi-lock, Hi-lite...) fasteners (those used for the airframe I mean) have this hex at the tip of the screw, it's simply to keep it from turning round and round and round, as you try to tighten the nut ! Otherwise it would drive you crazy real quick ! I mean, depending what degree of interference is specified for the particular hole where the fastener goes (depends on loads applied, type and magnitude, and what material the various parts being held together, are made of), I mean "clearance fit", "transition fit", or slight interference, or strong interference... If it's a clearance fit then the fasteners is kinda lose in the hole, so it would just spin round and round as you try to tighten it. So in this case, you need that hex at the end of the fastener to keep it still, otherwise you are screwed, so to speak !
Are Airbus fasteners metric ? I'd have thought they would be. As we know M5x1 is quite close to #10 UNF.
Nope. 100% of the fasteners used on Airbus aircraft, be it LGP/Hi-lite used for the airframe, or fasteners for "mechanical" stuff (ie : anything that is not either the airframe, or electrical related stuff), or even the "blind" type fasteners used to mount light-weight trim panels here and there (mostly lining in the cargo bays)... any and all type of fasteners are all originated from the USA, historically. So they all use imperial dimensions ! The diameter and length are coded using fractions of inches. Most of the time, the diameter would be expressed in multiples of 1/32" , up to a diameter of a 1/4", then above that it will use larger steps (1/16"). repair/oversize is defined as a 1/64" above nominal diameter (for first oversize/"R1", and 1/32" for 2nd oversize/"R2"). Lenght is coded typically in multiples of 1/16" .
So for example in my pictures, you can see the label on the plastic box : " ASNA2042-4-07"
ASNA = Name of the norm (you could have "DAN" for the German norms, or "NAS", or "ABS" in the case of the most recent norm in use at Airbus).
2042 = "part number" : defines the type/model of fasteners... though strictly speaking, it could also link to not just parts, but also technical documentation/papers... You can get "ASNA" or "ABS" XYZ for pretty much anything. Only the 4 trailing digits will tell you what type of thing is being referred to... a fastener, a washer, a nut, a collar (for an LGP fasteners), or some technical paper about this or that...
4 = diameter code : 4 x 1/16" = 1/4" = 6,35mm.
7 = length code (of the shank/useful part of the fastener) : 7 x 1/16" = 11,2mm.
Same principle goes for any type of fastener.
Late here again, good night....