std-aia/nas nas 1130-engl 2000 0318743 0507142 855 m see view 8 +e max^ sect. a-a r min tangent cqroition list of current sheets enlarged view b r no i rev _" custodi*n hatiowal aerospace standards cocbiittee third paojection angle prccurlment title i cllsslfsitbn insert, screw thread standard part l l copyright 2003; aerospace industries association of america, inc. (aia/nas) t document provided by ihs licensee=naval rsch lab/5929363100, user=, 07/09/2003 09:19:47 mdt questions or comments about this message: please call the document policy management group at 1-800-451-1584. --`````,,`,```,```,,``,`,,`,,-`-`,,`,,`,`,,`---
std*aia/nas nas 1110-engl 2000 w 03187q3 0507143 791 ael uapabt: industries national aerospace standard association ocopvrm3ht 2000 aerospace inwstrils assocuixhi of meiiici wc. all whr reserved table 1 - dimensions 1 dumeter nominal length nominal n m weight length thread thread *.25 *l lbll00 (ref) size size coil coil and length dash no (2)oo.) (1.) .086-56 5.000 2.500 .lo9 .250 -4f-10 .250-28 3.375 1.6875 .145 .250 -4-10 .250-20 4.125 2.0625 .o414 .190 -3-10 .190-32 2.875 1.4375 .o573 .190 -3c-10 .190-24 3.500 1.750 .o355 .164 -08-10 ,164-32 2.750 1.375 .o243 .138 -06-10 ' .138-32 2.750 1.375 .o121 .112 44-10 .i1240 3.000 1.500 .o05 1 .o86 -02- 1 o 1.5 diameter nominal length sue coil coil and .25 *l lblloo (ref) thread n m weight length length dash no (2.) (10) (1 .) -02-15 5.250 2.625 .o084 .i29 .o196 2.375 4.750 -06-15 -08-15 -3c- 1 5 -3-15 3.4375 6.875 -4-1 5 2.875 5.750 -4f-15 4.125 8.250 i 2 diameter nominal length ii 25 diameter nominal length ~ nominal n m weight length thread thread .25 kl lblloo (ref) size size dash no (2)(10.1 (1 .) length coil coil and .086-56 1 1.375 5.6875 .212 soo -4f-20 ,250-28 8.000 4.000 .308 ,500 4-20 ,250-20 9.500 4.750 .i12 ,380 -3-20 .190-32 7.125 3.5625 .i330 .380 -3c-20 .190-24 8.375 4.1875 ,0776 .328 -08-20 .164-32 6.875 3.4375 ,0525 .276 -06-20 .138-32 6.750 3.375 .o272 .u4 44-20 .i 12-40 7.375 3.6875 ,0117 .172 -02-20 2 diam nominal i thread .086-56 .i 1240 .i3 8-32 ,164-32 .190-24 .190-32 .250-20 .250-28 dash no -02-30 -04-30 -06-30 -08-30 -3c-30 -3-30 -4-30 -4f-30 dash no -02-25 -06-25 -08-25 -3c-25 -3-25 4f-25 (1.1 .215 .280 .345 ,410 .475 .475 .625 h25 ieter nominal length length n m weight (ref) (2h10.1 (1.1 coil coil h.25 *1 lblloo .258 17.625 11.9375 .338 .i50 12.750 8.750 ,490 .i50 14.875 10.125 .i70 ,570 11.375 7.8125 .219 si0 13.250 9.0625 .i25 .492 10.750 7.4375 .o807 ,414 10.875 7.500 .o423 .336 11.875 8.1875 .o183 table 2 - dimensions nominal a b thrwu) c 'ize 1 min gage ,11240 ,138-32 164-32 .190-32 ,190-24 .250-20 o weigh t lbll o0 m &i coil 5.4375 5.6875 7.500 6.375 d j f e min w'rn min max min max .o1584 .i07 .i19 .i10 .o156 .o126 .o116 ,0112 ,141 .159 ,144 .o219 .o189 .o1624 .o1985 .o2030 .o233 ,291 326 .306 .o313 ,0253 ,02320 .o2270 .307 .330 .310 .o438 .o378 .o3248 .o3198 .226 256 .236 .o273 .o233 .o2030 .o1985 ,237 .259 .244 .o365 ,0305 .o2706 .o2656 ,200 220 .205 .o273 .o233 .o2030 .o1985 .i74 .i93 .i78 ,0273 n *.25 coil (2.) (10) 9.625 8.875 8.875 10.750 9.250 12.000 10.375 14.500 4 5 1 .o056 ,0075 5 1 .o090 5 .o064 1 ,0098 .o 1 56 nas1 130 sheet 2 of 3 use of or rellance upon this document or any national aerospace standard is entirely voluntary. aia does not qualify suppliers or certify conformance of items procured under national aerospace standards. aia makes no representation or cwm respecting (1) the suitability of items for any particular application, or (2) the existence of or appllcabllrpl thereto of patent or trademark rights. copyright 2003; aerospace industries association of america, inc. (aia/nas) t document provided by ihs licensee=naval rsch lab/5929363100, user=, 07/09/2003 09:19:47 mdt questions or comments about this message: please call the document policy management group at 1-800-451-1584. --`````,,`,```,```,,``,`,,`,,-`-`,,`,,`,`,,`---
td.aia/nas nas 3330-engl 2000 d 0338743 05oyl44 d ne1 uspabe industries national aerospace standard association ccoww(wt 2000 aerdspace -l're8 associaikwi of amuiici. wc. all resew material: type 304 (uns s3o400) corrosion resistant steel per as7245. @ finish: - none. - dry film lubricant in accordance with mil-l-46010, type i. - cadmium plated in accordance with qq-p-416, type ii, thickness shall be a maximum of.0001. as a minimum all surfaces shall show visual evidence of cadmium platmg. code: - first dash number designates insert thread size as tabulated. -no lelter after the first dash number designates free running. - add l after the first dash number to designate self-locking. - second dash number designates length as tabulated. - no leiter after the second dash number designates no finish. - add d after the second dash number to designate dry film lubricant. - add p after the second dash number to designate cadmium plate. example of part numbers: NAS1130 -2 l 2 1l i" finish code length code as tabulated type code thread size code as tabulated document number nas 113044-15 = a tangless, free running, corrosion resistant steel insert, thread sue. 112-40, 1 .s diameter nominal length. 2.0 diameter nominal length. nas i 13046l20=a tangless, self-locking, corrosion resistant steel insert, thread size .138-32, nas i 130-3l2sd =z a tangless, self-locking, corrosion resistant steel insert with dry film lubricant, thread size ,190-32,2.5 diameter nominal length. nas i 130-3cllop= a tangless. self-locking. corrosion resistant steel insert with cadmium plate, thread se ,190-24,l .o diameter nominal length. nominal length equals minimum through hole length without countersink and with insert located 114 to ln thread pitch below top surface. the number of free coils of the insert are counted from notch to notch. the insert, when assembled in a tapped hole as specified m ms33537, shall produce a finished thread meeting the requirements of fed-std-h28/2 and shall accept external threaded parts which conform to mil-s-7742 or mil-s-8879. the exceptions to ms33537 include: installation is performed with the notch at either end of the insert instead of a tang, and consequently, a tang does not have to be removed after installation. on ms33537 a tangless insert is the equivalent to the tanged insert with the tang removed after installation. surface roughness is 32 microinches arithmetic average "um per ansi i asme b46.1. dimensions are in inches and apply before plating. tolerance unless otherwise specified is *.o10 for decimals and ji s degrees for angles. insert color identification: - no finish, free running: none -no finish, locking: red (dye) - dry film lubricated, free running: dark gray - dry film lubricated, locking: dark gray - cadmium plated, free running: iridescent bronze or yellow (chromate) - cadmium plated, locking: olive drab (chromate) sizes. 190-24 and.250-20 are not mil-$7742 and mil-s-8879 preferred sizes. this standard takes precedence over documents referenced herein. referenced documents shall be the issue in effect on the date of invitations for bid. the assembled length of the insert is specified on ms33537. i nas1 130 sheet 3 of 3 use of or reliance upon this document or any national aerospace standard is entirely voluntary. aia does not qualify suppliers or certify conformance of items procured under national aerospace standards. aia makes no representation or cwm respecting (1) ?"e suitability of ems for any particular application, or (2) the existence of or applicability thereto of patent or trademark rights. copyright 2003; aerospace industries association of america, inc. (aia/nas) t document provided by ihs licensee=naval rsch lab/5929363100, user=, 07/09/2003 09:19:47 mdt questions or comments about this message: please call the document policy management group at 1-800-451-1584. --`````,,`,```,```,,``,`,,`,,-`-`,,`,,`,`,,`---
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