NAS1351
Transcription
NAS1351
NATT.NAL AERospAcE @ COPYRIGHT 'TANDARD ffiffif 2009 AEROSPACE INDUSTRIES ASSOCIATION OF AMERIC/\, INC. ALL RIGHTS RESERVED |rali0.i4At AsHostAcI sIdNla(o$ FED. SUPPLY CLASS 530s t WHEN SELF"LOCKING ELEMENT IS SPECIFIED: HEAD MARKING OF A MINIMUM OF SIX (6) DOTS, MISED OR DEPRESSED, IS REQUIRED. TOP OR SIDE LOCATION OPTIONAL. (scREW SrZES 04 AND LARGER) I a d U E o z 300 SHAPE OF SOCKET BOTTOM OPTIONAL AD To 450 (D tr o tsoil E=i..i o6< uiAz ==>- THREAD SIZE d=5 AZ v9n it=- IDENTIFICAT]ON SEE NOTE (e) FILLET (s) K AB FOR NUMBER OF HOLES, PLAIN OR KNURLED HEADS OPTIONAL sEE NOIE (d) TABLE NOMINAL SIZE DASH NO. THREAD SIZE BODY DIAMETER u< <u 6i uF IE z+ Sx oo az <T Z* 3tr FE zu> ;x SOCKET SIZE MIN. .0568 ,0695 IVIAX. MIN, MAX MTN 138 MIN, .UJ/ .070 ,083 ,09s ,108 L34 .096 118 .091 .050 7r2 .073 .086 .099 159 .148 01 02 03 .0730-72 .060 n7? .0860-64 .0990-56 ,086 .099 .0822 ,0949 .740 .tof 04 TLZO.4B rLz .1075 .183 134 154 176 06 1380-40 1640-36 1900'32 .2500-28 138 L64 7329 1585 .226 )tR .270 ,262 .t64 .19U .184U .2435 .190 .250 .3053 .3678 .312 .375 .469 .562 .303 .250 ,3125 .4375 ,4294 .656 .500 ,49L9 .6163 .750 .3L25-24 .3750-24 .4375-20 5 6 7 B 10 z.H <ii fu <U oE J HEAD SIDE .0600-80 4 !!tr S HEAD HEIGHT 00 OB g9 DIAMFIER T2 14 16 @ T K WALL :NGAGEMENI THICKNESS KEY CHAMFER OR RADIUS HEIGH-I" MAX. F HEAD I H U ,937 ./35 .927 LZJ T,LO7 ,5000-20 .6250-18 .7500-16 .750 .7406 L, .87s0-r4 .6/J .8647 .988b L.3L2 1.0000-12 1.000 .365 .457 .550 .642 1.500 1.293 1.479 tLz .054 .066 .o77 .089 .101 .I24 ,16) 17r .244 .306 .368 NOMINAL .050 MIN. .uoz .031 .078 .078 .094 ,109 .L4T "038 .029 .044 20 .034 .038 ,047 .056 .065 .095 .250 151 19 .5 tl .375 .raz .r43 .213 .245 .1bb .190 .307 ,370 .238 1s6 ,188 .437 .500 .4JU .225 .28L .55 / .394 .492 .4s0 .5IJ .625 .750 .875 .616 ,740 ,562 .675 .500 .864 .74', 1.000 .98B .900 .3L2 -5/J .625 .750 .750 .ula ,051 .064 .o77 ,090 MIN, .020 MAX. 003 .003 .00J .003 .00s .00s .005 .005 .008 .008 .008 .010 .010 .010 .010 .015 ,015 .285 .432 .495 .380 frH d-. = tri F o z 6 U d N @ o J fiF Reproduced By IHS E?= <ts2 Wth The Permission 4S20 :d0 #9i Of AIA/NAS Under Royalty Agreement FdE THIRD CUSTODIAN ANGLE PRO.]ECTION PROCUREMENT NOTED REVISION NATIONAL AEROSPACE STANDARDS COMMITTEE 10 TITLE CLASSIFICATION PART STANDARD SPECIRCATION E 4 I= e a L 6I l9 o N 5UKEI'V, L;AP, S'UCKEI fIEAL', UNDRILLED ANT' DRILLED, PLATN AND SELF-LOCKING, ALLOY STEEI- CORROSTON.RESISTANT STEEL AND H EAT-RESISTANT STEEL, UNRF.3A NAS1351 SHEET 1 OF 5 USE OF OR REUANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SqPPLIERS OR CERTIF/ CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS, AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1D THE SUITABIUfi OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPL]CABILITY THERETO OF' PATENT OR TMDEMARKS RIGHTS. o U a = o NATIONAL AEROSPACE STANDARD o CoPYRTGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA" INC, ALL RIGHTS RESERVED TABLE SAFET MINXMUM BASIC THREAD NOMINAL SIZE DASH NO. I FNGTH = 00 a u UI E 02 o 03 tr 04 06 d zo U o DRILLED HOLE DRILLED HOLE LOCATION MIN. MAX. (d) (d) (d) .026 4 1.000 5 I.IZJ 6 1.250 . rz5 .035 .040 .045 .065 .084 .103 7 r.375 ,L4L ,LZt d 1.500 1.750 2.000 2^2s0 2,500 .160 .198 .235 .273 .310 .140 .750 10 I2 14 IO (A) MAX. MIN. (d) (d) .039 n?? 324 500 7r0 ''M'' MIN, (5 THREAD PITCHES) .067 .L78 .2L5 .253 .290 = 1.190 1.820 2.650 .050 .097 .044 ,uol 6,20S +ssg +4*€0 2W0 E.$gs .091 RIEGION OF MINIMUM ENGAGEMENT ]VIEET MIL-DTL-I8240 HEAT RESISTANT STEEL 28B CORROSION RESISTANT STEEL ALLOY STEEL 940 .040 .050 .060 .065 .085 .104 q:N IVIINIMUM BREAKING STRENGTH (POUNDS) AB .625 At*''544*t *IAr{Ea{$, II WIRE HIOLE WHEN SPECIFiED .500 OB a6z =v,-, >=9 *=6 A_Z frx; fc) ?.1.4'l[0titAl 3,600 6.550(h) 10.400(h) 15,800(h) 21,400(h) 28,800(h) 43,500 63,400 86,500 1 13,000 L40 220 445 310 420 530 810 1,180 1,600 OJI 836 1,058 r.620 2.360 3.200 s.820 2,970 4,640 7,020 9.280 14.080 19.000 25.600 9,500 12,800 20,500 26,100 41.000 ca 7nn 3s.600 46.400 81.400 106,200 WITH FULL FEMALE THREAD REQUIRED REQUIREMENTS. T^O @ LOCKING ELEMENT WITHIN ''M" REGION MUST DEVELOP REQUIRED TORQUE WHEN TESTED IN ACCORDANCE WITH MIL-DTL-LB24O. LENGTH OR DIAMETER OF LOCKING ELEMENT MAY BE MORE OR LESS THAN ''M'' PROVIDING ALL REQUIREMENTS ARE MET. (b) U< (c) st UF FO or 6T zt 9< (d) (e) =o 89 2P, <[ <u oE UA (f) (g) (h) <tz "N', = oNE (1) COMPLETE THREAD pt-US UNTHREADED PORTION OF END. FOR EASE OF STARTING, LOCKING ELEMENT SHALL NOT BE EFFECTIVE WITHIN THIS AREA, SCREWS WHICH HAVE A LENGTH LEIJS THAN THE MINIMUM BASIC THREAD LENGTH, SHALI." BE THREADED AS CLOSE TO HEAD AS PMCTICABLE, FICR SCREWS WHICH HAVE A LENGTH GREATER THAN THE MINIMUM BASIC THREAD LENGTH, THE BODY AND GFI.IP LENGTH SHALL BE IN ACCORDANCE WITH ASME 818,3. 5x =E oo oz <I Z* gtr dD) OTHER V ^ \t9 DRILLED HOLE DATA IN ACCORDANCE WITH PROCUREMENT SPEC FF-S-86. PARTS SI-IALL HAVE DRILLED HEADS IF SPECIFIED BY CODE H. SCREW SIZES 04 AND 06 SHALL HAVE TWO (2) DRILLED HOLES SPACED 1800. SCREW SIZES 08 THRU 16 SHALL HAVE SIX (6) DRILLED HOLES SPACED 600. (DRILLED HOLES NOT APPLTCABLE TO SCREW SIZES BELOW 04). IDENTIFICATION LETTER "N" IMPREIiSED ON THE TOP OR SIDE OF THE HEAD, FOR SCREW SIZES 04 AND LARGER ONLY, TO DENOTE HEAT-RESISTANT STEEL, THE INTERSECTION OF THE TOP ANID SIDE OF THE HEAD MAY BE CHAMFERED OR MDIUSHD AT THE MANUFACTURER'S OPTION PER ASME 818.3. THE FILLET SHALL BE IN ACCORDANCE WITH ASME @ 818.3, @ MINIMUM BREAKING STRENGTH VALUES ARE BASED ON 180 KSI HEAT TREATMENT. LINED THROUGH STRENGTH VALUES WERE BASED ON 170 KSI, =23 HO> EdU REVISION 10 E P NAS1351 tntrEt z USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY CONFORMANCE OF ITEN4S PRODUCED UNDER NATIONAL AEROSPACE STANDARDS, AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABIUTY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TMDEI4ARKS RIGHTS. *- NATIONAL AEROSPACE STA]\IDARD O COPYRIGHT 2009 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICIA. INC. ALL RIGHTS RESERVED TABLE scnlw o z e u 00 01 UZ -00-2 -00-3 -00-4 -00-6 -01-2 -01-3 -02-3 .375 -0L-4 -02-4 -01-6 -02-6 -02-B .s00 z .625 .750 .875 tr I o g=N 29s 03 1 .250 E SCREW SIZE .L25 .1BB I 1.000 1.250 1.500 T.75IJ P{tr, < 2.000 *EE A^z 2.250 E:A 2.750 III 04 06 08 J -03-4 -03-6 4 -04-4 -06-4 -08-4 -04-6 -06-6 -08-6 - <-6 -4-6 -03-B -04-8 -06-8 -08-B - l-x -4-B -03-10 -04-10 -06-10 -08-10 -3-10 -4-70 -04-12 -06-L2 -08-12 -4-L2 -06-14 -08-14 -3-14 -4-L4 -06-16 -08-16 -J--tb -4-L6 -08-20 -3-20 -a-zv -08-24 -3-24 -4-24 -3-28 -4-28 -3-32 -4-32 -4-36 I -7-r4 -B-14 -7-16 -8-16 -10-16 -8-20 -10-20 -B-24 r0-24 10 12 L4 16 -f,-o -5'8 -s-10 -5- rz -5-14 -s-16 -s-20 -5-24 -5-28 -5-32 -5--l b -5-40 2.500 7 6 5 3 000 3.250 3.500 4.000 -6-8 -6-10 -o- rl -b--t{ -6-16 -6-20 -6-24 -6-28 -6-32 -6-36 -6-40 -6-44 -6-48 -8-12 -7-20 -7-24 -7-28 -7-32 - /--16 -B-28 -8-32 -B-36 10-28 10-32 10-36 1 (l-4(l . LL-L1 rL2-28 i12-32 -14-32 rt2-36 L4-36 -8-40 r12-40 -14-+fJ -I6-40 -8-44 -10-44 ,12-44 -1 4-44 -8-48 10-48 -L2-48 -14-48 -f 0-46 t12-52 -L4-52 -ro-f,2 -4Il -7-44 -/ -7-48 -12-56 4.500 14-56 L4-64 -14-72 16-56 I o-n+ -16- / ) -16-80 5.000 NOTE: SEE CODE FOR ,ENGTH TOLERiqNCE SHALL BE AS JIZtr NOMINAL O THRU .375 LENGTH OVER.37I; THRU .750 ovER .750 THRU I.OOO TOLERIiNCES UP TO AND +.000 INCL. 1,000 -,030 u<L^ ovER 1.000 & SH INCL. 2,500 UF ovER 2.500 & +.000 - n40 +.000 FO INCL. 6.000 -.UOU or z< >X =v oo oz d< <E OF Z* gtr +.000 -,050 +.000 -.100 +.000 -.140 THREADS: UN[{F-3A IN ACCORDANCE WITH PROCUREMENT SPECIFICATION. MATERIAL: ALLOY STEEL IN ACCORDANCE WITH PROCUREMENT SPEC FF-S-86. CORROSION-RESISTANT STEEL IN ACCORDANCE WITH PROCUREMENT SPEC FF-S-86. HEAT-RESISTANT STEEL CONFORMTNG TO THE CHEMTSTRY OF AMS5731 (UNS 566286) OR AMS5737 (UNS s66286) COLD WORKED AND AGE HARDENED TO MEET THIE FASTENER REQUIREMENTS OF FF-S-86 AND THIS STANDARD. 9< zo g9 2!r <[ +.000 -.030 +.000 -.060 +,000 -.080 FINISH: ALL'Y srEE' clAss 2 <u -'ffiU'lK'#li,ltt8iBlRt!'',i#'i1i'H?,?P;il;1i?,ll'i1ll' 6H coRRosIoN RESISTANT STEEL - CADMIUM PLATE IN ACCORDANCE WITH AMS-QQ-P-4L6, TypE @z /i-d\ v E?: <ts2 65X ,^42 ;.to> IdU @ v /in) r, CLASS 2. - SILVER FLASH IN ACCORDANCE WITH AMS2411. - PASSIVATE IN ACCORDANCE WITI-I AMS27OO, METHOD 1, ryPE 6 OR TYPE 1ml 7, \]/ CLASS 1. REVISION 10 = e NASrSsl SHEET 3 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NANONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUAUFI SI]'PPLIERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO*EPRESENTATION OR CLAIM RESPECTING (1) THE SUITABIL1TY OF ITEI'1S FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO.OF PATENT OR TMDEMARKS RIGHTS. NATIO,NAL AEROSPACE STANDARD O COPYRIGHT 2OO9 AEROSPACIi INDUSTRIES ASSOCIATION OF AMERICA/ INC, ALL RIGHTS RESERVED HEAT-RESISTANT STEEL @ @ ; = a - SILVER FLqSH IN ACCORDANCE WITH AMS2411. - PASSIVATE IN ACCORDANCE WITH AMS2700, METHOD 1, TYPE 2 NUMBEIR, "-" = ALLOY 4rsfi BA{ss OR TYPE 8, CLASS 1. :3$i[3,il'15+tfiT*tstBi'-l'JT^?,+liiR[:a'3:ih:1??ii,,.*,,, CODE; MATERIAL CODE AFTER BASIC = h.A?r0}}&1 Af 1e1i8a{E @ STEEL' "C" = CORROSION-RESISTANT STEEL, "N" = HEAT-RESISTANT STEEL, z tr o FIRST DASH NUMEER DESIGNATES SCREW THREAD SIZE AS TABULATED. q:N ulnZ ==>- a=6 d^z TYPE CODE AFTER FIRST DASH NUMBER: "H" = DR]ILLED HEAD. "LE" = SELF-LOCKING MALE THREADED FASTENER, (OPTIONAL TYPE LOCKING ELEMENT IN ACCORDANCE WITH NAS1283). "LL" = SELF-LOCKING MALE THREADED FASTENER. (LONGITUDINAL STRIP LOCKING ELEMENT IN ACCORDANCE WITH NAS12B3, TYPE L), ''LN" = SELF-LOCKING MALE THREAEIED FASTENER. (PELLET LOCKING ELEMENT IN ACCORDANCE WITH NAS12B3, TYPE N). "LB" = SELF-LOCKING MALE THREADED FASTENER, (PATCH TypE LOCKING ELE|\4ENT IN ACCORDANCE WITH NAS1283, TYPE P). SECOND DASH NUMBER DESIGNATES NOMIN,qL LENGTH IN SIXTEENTHS OF AN INCH AS TABULATED. TABULATED CODING IN DICATES PREFERRED LENGTHS. ADDITIONAL LENGTHS AVAILABLE ON SPECII\L ORDER, MINIMUM RUN BASIS, FoR SUCH LENGTHS ADDITIONAL CODING Mi\Y BE ASSIGNED TO LENGTHS IN .0625 INCH INCREMENTS UP TO 3.500 INCHES, AND IN ,125 INCH INCREMENTS FROM 3.500 INCHES UP TO AND INCLUDING 6.000 INCHES, u<6 FINISH CODE AFTER SECOND DASH ,'P'' NUMBER; ALLOY STEEL, = CADMIUM PLATE, NO SUFFIX FOR BLACK OXIDE. SH u- CORROSION-RESISTANT FO oL oE "S" = SILVER FLASH. NO SUFFIX FOR PASSIVATE. z= E= 1x oo HEAT-RESISTANT oz <E Ze gu =o 2P, <E <u qz U^ BH iT 9oE <FZ =86 xxH #9h STEEL, "S" = SILVER FLASH, uB" = BLACK OXIDE. "P" = CADMIUM PLATE, NO SUFFIX FOR PASSIVATE. 9< 8s STEEL. "P" = CADMIUM PLATE. EMMPLE: NAS1351-02-8 = NAS1351C04H12 = NAS1351-081E16P = NAS1351C4LL24P = NAS1351N10LN32 = .0i360-64 UNRF-3A SCREW, CAP, SOCKET HEAD, ALLOY STEEL, UNDRILLED HEAD, PLAIN, .5OO INCH LONG. BLACK OXIDE FINISH. .LL20-48 UNRF-3A SCREW, CAP, SOCKET HEAD, CORROSION-RESISTANT STEEL, DRILLED HEAD, PLAIN, ,750 INCH LONG, PASSIVATED, ,1t540-36 UNRF-3A SCREW, CAP, SOCKET HEAD, ALLOY STEEL, SELF-LOCKING, OPTIONAL TYPE LOCKING ELEMENT. l,OOO INCH LONG, CADMIUM PLATE, UNDRILLED HEAD. ,21500-28 UNRF-3A SCREW, CAP, SOCKET HEAD, CORROSION-RESISTANT STEEL, SELF-LOCKING, LONGITUDINAL STRIP LOCKING ELEMENT, 1,500INCHES LONG, CADMIUM PLATE:, UNDRILLED HEAD. .6250-18 UNRF-3A SCREW, CAP, SOCKET HEAD, HEAT-RE:SISTANT STEEL, SELFLOCKING, PELLET LOCKING ELEMENT, 2.000 INCHES LONG, PASSIVATED, UNDRILLED HEAD, REV]SION N 10 E NAS1351 P SHEET 4 THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIF/ SUPPLIERS OR CERTIFY CoNFoRMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS, AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABTUTY OF ITEMS FOR ANY PARTTCULAR APPLICATION OR (2) THE EXISTENCE OF OR APPL]CABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS. USE OF OR RELIANCE UPON ; NATIONAL AEROSPACE STANIDARD O COPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERIC/\, INC. ALL RIGHTS RESERVED NAS1351N12LB365 = F,rAl|f,n t*,t,q*ft{}5t$if; $lAi4Brns5 ,7500-16 UNRF-3A SCREW, CAP, SOCKET HEAD, HEAT-RESISTANT STEEL, SELFLOCKING, PA]-CH TypE LOCKING ELEMENT, 2,250 INCHES LONG, S]LVER. FLASH, UNDRILLED HEAD. a NAS1351N4LB16B = = a: e U E L o z o .2500-28 UNRF-3A SCREW, CAP, SOCKET HEAD, HEAT-RESISTANT STEEL, SELFLOCKING, PA']-CH TYPE LOCKING ELEMEN:r, 1.000 INCH LONG, BLACK OXIDE COATING, UNDRILLED HEAD. NOTES: (i) F o LOCKING ELEMENT: EXCEPTAS NOTED HEREIN, THE LOCKING ELEMENT WHEN SPECIFIED SHALL BE IN ACCORDANCE WITH MIL-DTL.L8Z4O AND SHALL BE FULLY ENGAGED WHEN USED. (2) EgN unz d>t; A-Z (3) IDENTIFICATION: MANUFACTURERTO IDENTIFYALL MINIMUM PACKAGES BY PACKAGE MARKING OFAPPLICABLE COMPLETE NAS STANDARD PART NO. IN ACCORDANCE WITH MIL-STD-13o. DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED DIMENSIICNS AND TOLEMNCES SHALL BE IN ACCORDANCE WITH FF-S-86, ryPE VI AND ASME 818,3. (4) REFERENCED DOCUMENTS SHALL BE OF THE ISSUE (5) THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS SPECIFIED HEREIN. (6) (7) r'^\ \t!2 (8) EFFECT ON HE DATE OF INVITATION FOR BID. UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE DMWING OR SPECIFICATION MAY BE PROCURED AND USED UNTII- STOCK IS DEPLETED, REMOVE ALL BURRS AND SHARP u< UF I: IN @ ADDTTTONAL PART MARKING SHALL BE IN ACCORDANCE WITH FF-S;-86. PROCUREMENT SPECIFICATION SH @ @ : EDGES. @ FF-S-86: UNLESS OTHERWISE SPECIFIED, CAP SCREWS FURNISHED UNDER THIS STANDARD SHALL BE SUB]ECT TO IN.PROCESS CONTR.OL AND/OR END PRODUCT INSPECTION WHICH WILL INSURE MECHANICAL, METALLURGICAL, CHEMICAL AND COATING OR TREATMENT CHAMCTERISTICS WHEN SAMPLED IN ACCORDANCE WITH ASQ 21.4, INSPECTION LEVEL S-1, 1% AQL. or >2 5x =: oo AZ d< <E Zn <tr 9q xz =o ts9 2H <[ @Z HH s n7, =22 to> -da REVISION 10 z NAS1351 SHEET 5 THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUAUFY SI'PPUERS OR CERTIFY CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1} THE SUITABIL]TY OF ITEMS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS. USE OF OR RELIANCE UPON
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