ros pa ce ndu st r ies national aerospace standard a ssoc i atio n . = :o _ ,. _ r,. = ,, = , _ , , _ , = o = , _ o f_ ,., _ fed sup class one (1 ) raised m a rk " 5320 -. \- - _.030 m ax -- w . e 2o / _ s : _ \ ,010 r a d t manufacturer's id raised a28 6 i " _ _ . or recessed .010 max . i i -, _ .i _ - see n ote 11. 0 o ) .' r . 01 m a x p ' z ' = = , ._ , _ / _ --- leng th ? uji- o = +. 010 or r ec ess e d . 0 3 0 ma x , . 010 hi g h ma x or .o20 d ee p max dia c a c a' b e o f p ow s t o a bsolu t e (r e f) max :b005 max min max min pad = - u_ min tuo = < . 094 + . 0 0 2 .14g 0 .1260 .021 .006 no .0123 . 0 0 8 9 .1192 .1190 .023 . 029 cu p ,, =_ - . 001 .139 8 recess ,9,,, " ' " ; . 125 + . 0 0 3 . 1970 i . 1739 .029 .0 0 6 . 0 7 0 . 0141 . 0106 .162 8 .1626 .03 1 .039 - .001 .187 _ - _ . 1 56 + . 0 0 4 . 2 487 .2251 ,037 . 006 .0 80 .0189 . 0153 . 2 0 28 . 2026 . 039 . 04 9 !_ - .001 .238z . 187 +.004 . 2987 .2749 .046 .006 .100 .0225 .0188 .2 4 41 . 2439 . 04 7 .059 < _ - .001 . 2 8 79 _ _ 250 +.004 .3953 .371 0 .060 .008 .125 .0263 .0223 .3315 .3313 .062 . 0 78 - .00 1 .3835 _ ust of curre n t shee t s _!ii ? 1 : , custodian national aerospace standards committee =_ z _ proj e ction - , < pro c urment title cl _ s s lfic a t _ n specification rivet, solid, 100 deg flu s h sh ear head , a286 standard part no ne corrosion resi st ant steel and NAS1200 monel sheet 1 of 2 us e of or reliance upo n this document or any nat i onal a erospace sta n dard i s e n t i rely volu nt ary. n a does not q ua lify s u ppl i er s or _,__=.,__. o ,_._.,__ o __ . _ ,,._ u ._ u . o e.. . t, o. _ .-- os. . oe st . .o . rds. , , , , , , _ . 0 re_res_ . _ o . o . 0 _.,. res p e_r , ._ (,) " r .e , . h t u _ " u i:m::; poh a ny partigui ar apptlcatio n . or (2) the _' xiste n ce of or applicability th ereto of patent or trademark rights. http://
_erospace nd us tr i e s national aerospace standard ass o c i at io n _ "_ ' _ ' _ ' _ "_ ' _ _ ' =_ ' _-_"_ i ' " i i bas i c le n g t hs an d d ash numb e rs part d i a number . 1 25 .188 .2 5 0 .3 1 2 .375 .438 . 5 00 .563 .625 .68 8 .7 5 0 __ _ n as1200 - 3 .094 - 2 . - 3 - 4 - 5 - 6 - 7 - 8 - 9 - 10 -11 -12 nas .. 1200-4 .125 - 3 - 4 -5 - 6 - 7 -8 -9 - 10 -1 1 -1 2 nas120g-5 .156 - 4 - 5 - 6 - 7 - 8 -9 -1 0 - 11 - 12 c_ NAS1200 - 6 . 18 7 -4 -5 -6 - 7 -6 -9 . - 10 - 11 - 1 2 NAS1200 - 8 . 250 - 5 - 6 -7 - 8 - 9 -10 -11 -12 < _ basic lengths and dash numbers - part dia - number .813 .875 .938 1.000 1.125 1.250 1.375 1.500 1.750 2 . 000 _ _ _ NAS1200 - 3 .094 -1 3 -1 4 -15 - 1 6 e d NAS1200 -4 .12 5 -13 - 14 - 15 - 16 - 18 - 20 = = _ :d NAS1200 - 5 . 1 56 - 1 3 - 14 -1 5 - 16 - 18 - 20 - 22 - 2 4 -28 - 32 /_ l . u ? z tu _ na91200 -8 .187 - 1 3 - 14 - 15 - 16 - 18 i -20 1 - 22 - 2z _ -28 - 32 _=_ nas12 0 0-8 .250 - 1 3 -14 -15 -1 6 -18 1 " 20 - 22 -2 4 -28 -3 2 ?,,,__z note: monel rivets with le ngths t o the r i ght of the heavy une are not available with rad i used ends ? ma te r i al: a286 (u n s $662861 - corrosion and he a t resistant w i re per am _ 5734. monel (uns n04400) - ni c kle-copper- ai loy wire per qq - n - 281, cla ss a (annealed). s hear s trength at room temperature: a2 56 - 8 5 ks l to 95 ksi as heat tre a te d. 90 ksi min after driving. monel - 49 k s! to 5 9 ks i , as re c eived. see note 12. >; :::) heat trea t: a286 - solu _ on _ ' e at and pa r _ ally pred _ h e at tr e at a l ter aft e r h ea ding as fo l lows: heat at 16 5 0 f + /- 2 5 for 25 minu te s - oil qu e n c h. age at 1 250 f io 1350 f fo r 30 to 90 m _ as as neces s a r y to m e et sh e a r requiremen = . air cool. b finish: a295 - p es sivat e p e r qq-p-3 5 . _. monel - on l y when sp e dfied, cadmium plate p e r qq-p -4 16, typ e ii, class 2. c _ code: " m " in p l a c e of _ , st dash in_ monel " p " aft e r las t dash number indicates c adrnlum plate for monel only. i" examp les of part numbers: i_ , f_ n a _ 1 200mi' _ p == "125 d |a, "5 00 le ng th e mo n e l riv e t* c * _0 j _ m | u a pla ted n_ 1200 -4- 8 - 5 = .1 25 dia, .531 le ngth, a 2 8 6 rivet (see no te 10) _ ) notes: 1. tol e rances: u n le ss otherwise s _ . .010. 2. .001 shank d i a met e r incr e as e p e m _ ls __ _n e _ .10 in c hes of bas e of h e ad. 3. sha n k a n d head diam e t e rs sha l l b e c or _ eflldc within .010 for riv e t s i t u'u .125, withi n .01 5 for .1 5 6 a n d .187 riv e ts, and w i th i n . o2o fo r .25o _ ets, rm . 4 . riv e ts sh a l l driv e o old sa'dsfac te dly with full heads free from _ a cks. 5. riv e ts must b e of uniform qua rw a n d free lror n sca le , r,' z s, seams, c i n ch or die marks, cold shuls, or oil e r 6. head oidng angl e relativ e to ds of riv e t . 500 d e g max. 7. m m dmum head diamet e m ate to _ eoret _ ! sham comers as measured by projecti _ . >. 8. see n / l3527 for the reconune c c le d _ for irspe _ ng head ch a ra c te rblics. 8. the be a _ m_ y may be _ _ a _ " _ " c _ on, l o . _ d _ or _ .o _13 v _ reme _ may be oua v _ by add _ g - 5 a _ ter _ = st _ t o f part numb e r, i_ ( _ )11. ma n ufacturer _ identification is required on riv e t heads with sha n k diamet e r . 125 inch a n d la r ger ma n ufa c lured a l ter < june 19o -. .3. ? 12. do _ jb le shear strengthtests sha l l be i n a cc ort an _ w it h mi l -s td-1312, test 13 o r astm b565. si n gle shear i stm c tgth tasti ng per mi l -s td - 1312, test 20. i :c r n, . sheet 2 u se of or reliance upo n this d ocument or a n y national aerospace s t a ndard is entirely volu nt ary'. aia does n ot oua l if' f s upplier s or certify co n fori 4 ance of it e i / ,s pr oc ured u n der na tio n al aerospace st&noaros. n a ike, ke 8 n o represe nt a ti on or claim r es pegting (1) the su[ta e |l[ty of items f or any particular applicatio n . or t _ th e existen c e of or appuoab i uty ther eto of patent or trademark rights,
|
