NAS1160
Transcription
NAS1160
#e* NATIONAL AEROSPACE STAN DARD O COPYRIGHT 2011 AEROSPACE OF AMERICA" INC. ALL RIGHTS RESERVED FED. SUPPLY CLASS 5306 U = O &. U trS *,oro E L GRIP z o tr .016 *.005 @K WHEN SPECIFIED U o q qo N CHAMFER 45O APPROX, h9ii u;z =z^>, ?:e *=te THREAD PROFILE v9r ^z tr5t OP WHEN SPECIFIED 15O MAX NAS1347. TYPE IV CHAMFER 150 TO OE OPTIONAL T - THREAD r PER ASBB79 TABLE h: u< I_ DIMENSIONS FIRST T A B @D AE DASH NO. THREAD SIZE ACROSS FLATS MIN SHOULDER MIN aF FO or >4 08 .L640-32 UNJC-3A 5x =; AO 3 .i900-32 UNJF-3A A .2500-28 UNl]F-3A .3L25-24 UN!F-3A .3750-24 UNJF-3A .4375-20 UNJF-3A .s000-20 UNJF-3A .s52s-18 UNJF-3A ,6250-18 UNJF-3A .7500-16 UNJF-3A oz <E OF a <tr 6 7 8 9 5 z* p< 4.o fiu O> !Jtr <[ =li iu <U 10 12 @z MAX .429 .492 .439 .502 .348 ,410 .480 .552 .554 .564 .623 .678 .690 .752 .877 .764 .836 .940 1.050 .74t .865 ,928 1.052 .376 1.065 MAX ,1890 ,1895 - .2490 .2495 .3740 .4365 .4990 .s615 .6240 .7490 .8740 .015 .000 AK DRILLED HEAD MAX MIN N .042 d f .272 ,335 ,398 ,460 .362 .362 .095 .110 .453 .L25 .498 .l-81 .523 .607 .156 .188 .4995 ,5620 ,648 .629 .2t9 .7L0 ,250 .6245 .835 .770 .8s5 .20L .216 .287 .23t .7495 .8745 .89B .94L .3L2 1.023 1.041 .375 .249 .249 .3r20 .978 1.191 MIN J BASIC H + tBl MIN .305 .367 .3t4 (F) .3745 .4370 N/A .0s2 N z rort .L78 . .070 |! ko .L97 z. .060 6 .080 U d o 6 o '+o 'jO ")6 frJ d -U dj F ==4 <ts2 =<o x99 o U f a a *o> Tdu THIRD ANGLE PROJECNON PROCUREMENT SPECIF]CATION = o NAS40O3 CUSTODiAN REVISiON NATIONAL AEROSPACE STANDARDS COMMITTEE 5 ,Hil, sHouLDE& HEX HEAD, CLOSE TOLERANCE, CRES-A286,95 KSI Fsu CLASSJFiCATION PART STANDARD NASl160 SHEET 1 OF 3 THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT OUALIFY SUPPLIERS OR CERTIFY copYriqht Aerosoace Industies affir*rqBftA&eF€fthteus pnooucED UNDER NATToNAL AERospAcr surrABrury oF Prov,ded by tHS under license wbYJAd]AS'j ir;;;.ij"il;;;;;tu;;ki;;S[F{HfiHBd$lltYf,$BTlfilbAR APPUcATIoN oR (2) rHE EXISIENcE oF oR APPL(I{H USE OF OR REUANCE UPON srnnoeno:f;:ffiffip6qpph&Bfffir6ffiEFff.#fb(AbilHE d$e$ NATIONAL AEROSPACE STAN DARD @ COPYRIGHT 2011 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. AtL RIGHTS RESERVED TABLE FIRST QM UNDERCUT DASH NO. = Id u MIN 115 MAX 1 .137 .L4I 4 .189 s 5 a 6 7 8 9 10 ,244 .306 ,356 .4L9 .474 .194 ,249 z tr g:R o6< zz> uiz ?J9 a=b tr38 ,010 tst 08 E * N t2 + - ,010 ,000 DRILLED SHANK .119 ,025 ,031 .031 ,047 .047 .047 .311 .362 .425 N/A .070 .076 ,076 .106 .106 .106 .106 .106 .Q47 ,480 .062 .534 .542 .650 .658 .062 .062 DIMENSIONS (CONNNUED W TOL TOL UNDERCUT U FILLET as RAD RAD .t4l MIN ,015 ,01s ,015 ,015 MAX .UZU .030 .020 .UJU .020 .025 .025 ,025 .030 .035 ,035 GRIP + ,010 - .000 ILII I .072 2 .135 .r97 .260 .322 4 5 .385 .447 .510 .572 .635 6 7 F U< oF lnl I 9 10 L2 L4 16 20 24 >= 5x =: oo az d< 57iNFAcl5 MIN TENSILE AT UNDERCUT TOL LBS1421 ABLE SECOND DASH NO. X THREAD RELIEF R @P ll/il ii*0.lFAde tiAtifr .025 .025 ,025 ,025 II - .0030 .0030 .0030 ,002s ,002s ,0020 .0020 .0020 .0020 .0020 ,00s .006 .008 .009 ,010 ,011 .0t2 .015 .018 ,020 MIN MAX MIN .01s ,020 .020 .030 ,030 ,030 ,035 ,0s0 .050 .050 ,0s0 .042 .056 ,vz) .025 .030 ,030 ,030 .050 .050 .047 ,054 ,063 .063 .075 .075 MAX 1,660 2.350 4.500 .062 .07r 7,490 ,083 .083 .100 .100 ,ILz .070 .083 ,083 .070 .094 .L25 .010 11.800 15,900 22,000 28,200 .t12 .015 35.800 53.100 GRIP AND LENGTH LENGTH +.030, -,010 FIRST DASH NO. t2 10 8 s lLjl 6 08 3 4 5 .L640-32 .1900-32 ,2500-28 .3t25-24 .3750-24 .4375-20 .5000-20 .5625-18 .6250-18 .7500-16 .424 .424 .515 .487 .578 .623 .487 .549 ,549 .640 ,68s .879 ,857 .6L2 .6t2 .703 .748 .919 .94L .674 .765 .810 .674 1.316 L,4L6 1,230 .982 i.004 t.t45 .737 .873 .737 .828 r.478 r.207 r.292 1.378 1.066 1.044 .799 ,890 ,935 .799 .862 .862 ,953 1.015 1,078 1.203 1,328 1.453 L. /U5 1,953 .924 .987 .760 T.IT2 ,885 L.237 i.010 I.JOZ 1,260 1.510 .998 1.060 L.LO7 1.t29 1.169 1.191 t.L23 r.232 ]-254 L.248 1.357 L.379 L.373 1,498 t.482 I.748 1.857 2.L07 1.504 1.609 T.879 2.020 2.r29 2.270 1 004 r.607 t.270 r.332 1.395 1.520 1.355 L.4L7 1.480 1,605 1.645 L.730 t.770 1,855 2.355 t.44L 1.541 1,503 1.566 1.603 1,665 I.OYI t.79r 1.816 1.94L 2.04L 2.tgr 2.29t 2.44L 2.54L 1.916 <E OF Zd <U 9< zd MATERIAL: H= 9> Ptr <[ =!t =u <U @z d-. <ts2 CRES - A286 (tr,NS 566286) CONFORMING TO THE CHEMISTRY OF AMS5731, AMS5732, AMS5737 or AMS5853. HEAT TREATMENT: 160-190 KSI UTS rN ACCORDANCE WrrH PROCUREMENT SPECIFICAION /+2/ (t) THREADS: SHALL BE ROLLED AND BE IN ACCORDANCE WITH AS8879. (SEE PROCUREMENT SPECIFICATION). FINISH: *q9 =?z ;6!? fio> UNCOATED AND COATED BOLTS - PASSIVATE IN ACCORDANCE WITH AMS2TOO METHOD 1, TYPE 2 ORTYPE 8, CLASS 4. ALUMINUM COAT ALL SURFACES, EXCEPT ''OD' AND WASHER FACE, IN ACCORDANCE WITH NAS4OO6 WHEN SPECIFIED, REVISION 5 NASl160 SHEET 2 THIS DOCUMENT OR ANY NATIONAL AEROSPACE €ftrttEMs pRoDUcED UNDER NATToNAL AERospAcE sTANDA USE OF OR RELIANCE UPON Copyright Aerospace Industries ffifft$f,IdrteE #e$. jlttia NATIONAL AEROSPACE STAN DARD o coPYRIGHT 2011 AEROSPACE INDUSTRIES ASSOCIATION OF AMERIC& INC. ALL RIGHTS RESERVED CODING: Lf 6DH llt- TTT (J z d BASIC NUMBER a u ALUMINUM COATED INDICATED BY "A" UNCOATED INDICATED EY A DASH "-" z L z tr DRILLED HEAD INDICATED BY DRILLED SHANK INDICATED BY lrJ 6 d.x "D" SECOND DASH NO, FROM TABLE FIRST DASH NO. FROM TABLE o "H" I II (GRIP LENGTH) (BOLT SIZE) EMMPLE OF PART NUMBER: E9i{ Zz> uxz CLOSE TOLEMNCE, CRES 4286; ALUMINUM COATED; DRILLED SHANK AND DRILLED HEAD GRIP; .385 UNJF-3A; ,1900-32 NAS116043-6DH = BOLT, SHOULDER, HEX HEAD, ?:e A=1, -lz HA= Eli< NAS1160-3-6DH = BOLT, SHOULDER, HEX HEAD, CLOSE TOLEMNCE, CRES 4286; UNCOATED; ,1900-32 UNJF-3A; ,385 GRIP; DRILLED SHANK AND DRILLED HEAD NAS1n60A3-6 = BOLI SHOULDER, HEX HEAD, CLOSE TOLEMNCE, CRES A286; ALUMINUM COATED; ,1900-32 UNJF-3A; .385 GRiP NOTES: (1) DIMENSIONS ARE IN INCHES. (2) DIMENSIONS APPLY AFTER FINISH UNLESS OTHERWISE SPECIFIED' (3) BOLTS SHALL BE FREE FROM BURRS AND SHARP EDGES' (4) TENSION AND FATIGUE NAS4OO3 SHEAR VALUES ARE APPLICABLE TO SHOULDER (SHANK) SIZES. NAS4OO3 I' TABLE SEE AREA, VALUES DO NOT APPLY. FOR MINIMUM TENSILE VALUES AT UNDERCUT <U oF EE FO (s) DIMENSIONiNG AND TOLEMNCING PER ANSI Y14'5M-1982' oL oF (6) TO BE 125 SURFACE ROUGHNESS PER ASME 846.1. UNLESS OTHERWISE SPECiFIED, SURFACES Y14.36M. ASME WITH ACCORDANCE BE IN MICROINCHES Ra, SURFACE TEXTURE SYMBOLS SHALL (7) OF THE UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS IS DEPLETED' STOCK UNTIL USED AND PROCURED BE MAY APPLICABLE DMWING OR SPECiFICANON t8l WASI-IER FACE DIAMETER: MAXIMUM NOT TO EXCEED @A (MAX); MINIMUM AS SPECIFIED' tel HEAT OM AREA SHALL BE AS FORGED OR MACHINED AND SHALL NOT BE FINISH ROLLED AFTER TREATMENT, Itjl NON.PREFERRED. U< >4 E; 5x oo oz <! OF Zd <tr 9< =o xz EU o> Frtr <[ =t? o= FE 5S I1'l I oR SECoND DASH NUMBER INDIcATES GRrp LENGTH IN ,0625 INCREMENTS +.010. INTERMEDIATE ONLY' NUMBERS DASH WHOLE OF BY USE BE SPECIFIED MAY LENGTHS GRIP LONGER t+f THE EFFEET EF EEtD WERK AND AGING INDUEED DURING THE MANUFAETURING EYELE TNY IN€REASE rHf Uttll4*te ffNSlUe STRENGTH eF THE FINISHEE tARTi BUT SHALT NeT EX€EED 1:3 TIMES THE F o =2 <k =< z Td d O REVISION 5 o : NAS1160 d o SHEET 3 USE OF OR RELIANCE UPON SUPPLIERS OR CERTIF/ THIS DOCUMENT OR ANY NATIONAL AEROSPACE STAN-DANO IS TNTSqIY^VOI-UNTARY. AIA DOES NOT QUALIFY copyrightAorospace|nd,.r,i""[ffig14i$e+#EFrl,ripnoijucrourlornrlniIorle|ninospncisrnruona?!8:Fb(3ttflEsUITABILrryoF l'"t*:*.U:;f:*::ffi$#StTdi[u6affignneriIcfitoru on 1z1rnr ercsmncr or onnecLl(:[$
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