MS21042
Transcription
MS21042
NATIONAL AEROSPACE STAN DARD O COPYRIGH'I'2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC, ALL RIGHTS RESERVED DESJGN OF WRENCHING PAD FACES BETWEEN WRENCHING CORNERS IS OPTIONAL IF THE WRENCH]NG CORNERS ARE WITHIN THE L]MiTS OF E, W AND C BEFORE LUBRICATION AND THE UMIT OF THE AREA BETWEEN THE CORNERS IS WITFIIN THE MAXIMUM LIM]T OF W FOR THE E LENGTH OF WRENCHING CORI{ERS, BEFORE LUBRICATION U = d RADIUS, CHAMFER OR SQUARE p. u : I L z tr -G/// s q E:N 46< =z> ugz' TOOL MARK OR a=6 9.^4 it=3 <=< DISTORTION PERMISSiBLE IN LOCKING AREA TABLE I SIZE THREAD DASF NO, /3t QIA QD @B E MAX MIN MIN 02 04 06 F 08 u{ <U @F uFE 3 LO 6+ 4 Z= EY Sx 5 oo az d< <AF o Z* gtri UNJC-38 .LL20-40 UNJC-38 .1380-32 UNJC.3B .L640-32 UNJC-38 .1900-32 .t6i UNJF-38 .3750 24 UNJF.3B t6t t7t __l DIMENSIONS OD & G DIMENSIONS H J W X /VRENCHINC MIN tst t4t TORQUE IN-LBF MIN MAX MIN \4AX MIN \4A) MIN .LJ/ .138 .106 .086 .04s ,01s .02L ,004 .100 ,080 .Lzi .L22 ,002s .L4I 1i5 244 .2Lz .207 .16€ .138 .055 039 .29C ,26( .244 .L94 29C .277 ?RF .220 't ,19C .181 . or 065 .043 .22L .2r LZJ .003 .34i .280 .250 .090 .057 .03€ 00, .2t9 .204 .UI:' .316 .304 .575 .49L .405 .375 .L25 089 5 660 .020 10 1,1 1o ,0s0 20 L,670 .080 30 2Ael .150 OU 3,470 .180 f, 1s0 6,20Q .350 i:i 330 9,820 .600 530 15,200 .800 E .252 .24 .266 .251 .023 ,378 .367 .042 ,00€ .OZU t9l .01 .t54 ,520 .482 .4L9 .342 .3L2 .LaC 077 WT O N .t64 .060 .04L .031 .006 .188 ,33C AXIAL STRENGTH LBSi 10C LBF MIN MAX tB/ 20( .L76 .L7L .L42 .TL2 05c n)9 .027 .005 .L2s .103 .010 .15t .150 UNJF-3B .2500- 28 42C UNJF-38 .3125-24 - U MIN MIN MIN .0860-56 F COUNTERSINK, COUNTERBORE, OR MDIUS RELIEF TO THREAD WITHIN THE LIMITS OF .004 ,282 .267 .030 .440 .430 z. ko z 6 U d. 9< xz E9 ur FTI zn <[ lu <u o @E HH @fi YOF ga" e4A @ cover-rrElY d) 5 Permission of AIA/NAS Under Royalty Agreement REVTsED ii <ts2 q!20 ,^ O ilo> rdu o : d U Y Reproduced By IHS wlh The E o U YJ THE INITIAL REL.EASE OF THIS DOCUMENT SUPERSEDES MS2IO42, REVISION PROCUREMENT SPECIFICATION NASM25O27 M. PART NUMBERS REMAIN M527042. CUSTODIAN REVISION NATIONAL AEROSPACE STANDARDS COMMITTEE 1 TITLE CLASSIFICATION PART STANDARD NtuT, SELF-LOCKING,450o F, REDUCED HEXAGON, REDUCED HEIGHT, RING BASE, NON-CORROSTON RESISTANT STEEL NASM21042 SHEET 1 OF 4 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTiFY CoNFoRNIANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. ALA MAKES NO REPRESENTATION OR CLArM RESPECTING (1) THE SUITABILITY OF ]TEIVIS FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS. =) 6 tt NATIONAL AEROSPACE STANDAR.D @ COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED MATERIAL: STEEL: UNS G10350 (AISI C103s) PERAMS5080, AMS-QQ-S-700 z UNS UNS UNS UNS UNS UNS d : u z E rAN G10420 G10500 G40270 G40370 G86300 G87400 (ArSr C1042) (AISI 1050) (AISI (AISI (AISI (AISI 4027) 4037) 8630) 8740) PER pER pER pER pER AMS5085 ASTM A322 ASTM 4322, 4108 A33+, 4519, A547, AMS6300 AMS62B0, AMS6350 6355, AMS6360 653g, A|N4S6550 AMS6322, AMS6323, AMS6325, AM56327, AI\456358 HEAT TREATMENT: gER Qo< =1> HH< DEVELOP BASIC MATERIAL PROPERTIES WITH CONTROLS PER AMS2759, HARDNEISS TO 49 HRC MAX. >J9 a=6 6oZ t3ft FINISH: PLATING, CADMIUM PLATE IN ACCORDANCE WITH AMS-QQ-P-416, TYPE II, CLASS 2, FOR DRY FILM LUBRICATED NUTS, TYPE AND CLASS ARE OPTIONAL IF THE NUTS I\4EET THE SALT SPMY REQUIREMENTS OF AMS-QQ-P-416, TYPE II. LUBRICATION: DRY FILM OR NON-DRY FILM IN ACCORDANCE WITH NASM25O27. OTHER LUBRICA,NTS SHALL BE SOLUBLE IN THE CLEANER SPECIFIED IN PROCUREMENT SPE:CIFICATION. F U< <u @F CODE: TE THE PART NUMBER SHALL CONSIST OF THE BASIC MS NUMBER FOLLOWED BY A DIASH NUMBER Eo >2 LETTER"L" BEFORE FIRST DASH NUMBER DESIGNATES DRY FILM LUBRICATED NUTS, FROM TABLE I. 3= $x oo az d< <I Z* EXAMPLES OF PART NUMBER: <in M52I042L4.2500-28 NUT, CADMIUM PLATED, DRy FILM LUBRICATED. MS2IO42-4.2500-28 NUT, CADMIUM PLATED, NOT DRY FILM LUBRICATED. o< FJ zo 8E Ftr <tr =H NOTES: <u o: Aii !tir y,) 6 fiJ (1) DIMENSIONS IN INCHES AND APPLY AFTER FINISH UNLESS OTHERW]:SE SPECIFIED. (2) DTMENSTONS AND TOLERANCTNG pER ASME y14.5M-1982. /3/ THREADS BEFORE LUBRTCATION pER ASBB79. I4I BEARING SURFACE SHALL BE SQUARE WITH PITCH DIAMETER WITHII\ "X" WHEN ]VIEASURED IN ACCORDANCE WITH NASM25O27. YOF F=x <t-z xq9 EO> IdU REViSION I o E d @ cover-rrElY NASl"l21042 REVTsED usE oF oR RELIANCE UPON THIS DOCUMENT OR ANY NATTONAL AEROSPACE STANDARD IS ENTTRELY VOLUNTARY. CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION AIA DOES NOT QUALIF/ S;UPPLIERS OR CERTTFY OR CLAIM RESPECTING ITEMS FOR ANY PARTICUI.AR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABIL]TY THERETO OF PATENT OR TMDEMARKS RIGHTS. ( 1) THE SUITABILITY OF NATIONAL AEROSPACE STAN DARD O COPYRIGHT 20I3 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA" INC, ALL RIGHTS RESERVED U = d /51 DIMENSIONIS APPLY PRIOR TO DEFORMATION OF LOCKING FEATURE. /61 MINIMUM LENGTH OF EACH WRENCHING CORNER. 17I MINIMUM D]ISTANCE FROM THE WASHER FACE OF THE NUT TO THE BEGINNING OF THE MINIMUM O LENGTH &. u : L z tr s NUT SHALL I]E TESTED FOR WRENCHING TORQUE BY THE USE OF A BOX OR SOCKET WRENCH. /91 TEST BOLTS SHALL BE 180,000 pSI MrN. trciri a>ii o6< E=E -o ^= UOE EACH WRENCHING CORNER. IBI (10) ==>. 116'= *E'OF SURFACE TEXTURE: SURFACE TEXTURE IN ACCORDANCE WITH ASME 846.1 UNLESS oTHERWISE SPECIFIED THE SURFACE TEXTURE SHALL NOT EXCEED 125 MICROINCHES, (11) REMOVE ALt. SHARP EDGES AND BURRS. (12) THESE NUTS SHALL BE USED IN ACCORDANCE WITH THE LIMITATIONS OF NASM3358B, (13) (14) (15) (16) NASM21042 SUPERSEDES: AN363, AN364, AN365, MS20364, MS20365, MS21040, NAS679 IN pART, NAS1O21 IN PART, NAS1O22 IN PART, NAS1291 IN PART. THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS REFERENCED HEREIN. UNLESS OTHERWISE SPECIFIED, ISSUES OF R.EFERENCED DOCUMENTS ARE THOSE IN EFFECT AT THE TIME OF SOLICITATION. UNLESS OTHERWISE SPECIFIED HEREIN, REFERENCED DOCUMENTS SHALL BE THE ISSUE IN EFFECT ON DATE OF MANUFACTURE. HOWEVER, EXISTING MATERIAL INVENTORY CERTIFIED TO A PREVIOUS REVISION OF THE APPLICABLE MATERIAL SPECIFICATION(S) IS ACCEPTABLE FOR USE UNTIL DEPLETION. u{6 ILTI #+ MARKING: MANUFACTURER'S IDENTIFICATION REQUIRED FOR SIZES .T640-32 AND LARGER. SIZES .1380-32 AND SMALLER AT MANUFACTURER'S OPTION (POSITION OPTIONAL). I: EY Sx oo az d< <AF Zd gtr FJ za Hz gs !!tr <[ =H lu <U oE ap g?x <t-z xg9 #9a E d 'I @ corvrer-rrElY REVTsED NASM21042 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUAUFY SUPPUERS OR CERTIFY CoNFoRMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUTTABILmY OF ITEMS FOR ANY PARTICULAR APPLICA IION OR (2) THE EXiSTENCE OF OR APPLiCABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS. *ee &55*{:t4rtQE NATIONAL AEROSPACE STANDARD @ COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC, ALL RIGHTIS RESERVED TABLE II - INTERCHANGEABILITY TABLE CANCELLED AND INACTIVATED PART NUMBERS AN363 AN364 AN365 MS20364 MS20365 MS21040 NAS679 NAS 021 NAS1022 a z o -440C e u -440C -04 104 E z -632 tr o -632C -448C -632C -640C -640C -832C -6321 -06 =Aa A6'=, *=6 -832C -836C <=< -428 -428C -518 -524 -616 -624 XO6W, XO6 AXO6 AXO6 -832C -832C -08 A06 A06 XOBW. XOB AXOB A06 AXOS A08 AOB A08 -524C -428C -518C -524C -06 MS21042106 XOB M521042-08 -08 MS21042108 -1032C -3 X3W, X3 L3 A3 AX3 AX3 X3 MS21042-3 -3 MS2104213 NONE -428C -428C A3 -4 X4W. X4 L4 A4 -5 AX5 L5 X5 A5 -6 X6 AX6 L6 A6 AX4 A3 AX4 A4 A4 x4 MS2t042-4 -4 MS2L042L4 X5 M521042-5 -5 MS2104215 X6 MS2L042-6 M52104216 NONE -524C -624C -624C -524C AX5 A5 A5 NONE -624C -624( AX6 A6 A6 -720C -820C AX7 A7 -B20C AXB AB -918C -918C AX9 A9 -101BC -1018C -L2L6C -t2t6c uEE .L4I4C -t4L4C -1614C o! -1614C -1812C -20r2c -2072C >= EY 5x M521042-06 -616C -720C *H x06 ttts2t042-04 NONE -1032C L7 u<o tv1s2r042L04 NONE -7 ts x04 -04 -420C -420 n:t=4 MSZLO42LO2 -836C -7024 -t024c -7032 -1032C -1032C 9. A04 MS2r042-02 -02 NONE 108 hein 5lN oo< -832C A04 SUBSTITUTIVE PART NUMBERS NONE -632C 106 Ua x04w. x04 AX04 NAS129i x02 -1B12C AXlO 410 AX12 ALz AX14 A14 AX18 A1B AX2O A20 -6 NAS679X7 NAS679A7 SEE NASM21245 SEE NASM21245 SEE NASM21245 SEE NASM21245 SEE NASM21245 SEE NASM21245 NAS1O22A17 SEE NASM21245 SEE NASM21245 a@ az d< <I 6F Ze <in 9< 4o Hz tsH PJtr <tr =!r fU'L (u oE NH 96 frJ ;;oui YOF <ts2 xq9 ==6 ;69 HO> Tdu REVISION 1 E d r @ couer-rrElY REVTsED |NASfrl21042 SHEET 4 USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SiUPPUERS OR CERTIFY CoNFoRMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. ALA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICAT]ON OR (2) THE EXISTENCE OF OR APPLIOqBTLITY THERE-TO OF PATENT OR TMDEIYARKS RIGHTS.