/ Shear. NAS1118 Datasheet

NAS1118 Shear. Datasheet pdf. Equivalent


AIA NAS1118
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Reproduced BY IHS
With The Permission Of AWNAS
Undr:r RoYaltY Agreement
NATIONAL AEITOSPACE STANDARD
@ COPYRIGHT 2010 AEROSPACE INDUSTRIES
.1|l)
EI--L
DETAIL A
LENGTH r.01
GRIP +.010 /3/
.020 *.005
K
(r)
,ril
fr
r*"I#-,kJt
POINT SHALL BE FLAT AND
CHAMFERED. CHAMFER (U).
CNNUTTN PLUS INCOMPLETE
THREADS NOT TO EXCEED
TWO THREAD PITCHES.
}-"*
IDENTIFY PER
NAS1347, TYPE IV
.'\- sEE DETA'L A
CHAM 15" TO
OC OPTIONAL
DRILL OP WHEN
spictrleo, csK oPTIoNAL /4/
;il;oTHREADS PER AS8B79 EXCEPT MAX
BE .oot arlow MIN sHANK
MA]OR
DIA'
iinrno RUNour PER NAS4oo2'
BASIC
PART
THREAD
UNJF-3A
(B) (/tC
IVIIN
ftI@D
l-l
+.015
,.000
J
+.U IJ
-.000
OK
!nl
M
r.010
AP
+.010
-.000
R
RAD
NUMBER
NAS11O3
NAS1104
NAS1105
1900-32
.2500-28
.3L25-24
.376
.367
.439
.430
.502
.492
.564
,+5
.f,r
.58
t".65
398
,460
.1895
.1885
.2495
.2485
,3T20
.3110
.110
. LZ-)
.156
,1BB
.073
.083
104
.r25
.19 .
1L7
.25 .Lro
119
.38 .r20
.070
,u/o
.076
.106
.010
,uzv
.010
.020
.010
.025
nt E
NAS1106
NAs1107
NASllOB
.3750-24
.4375-20
.5000-20
.553
.690
.679
,t 3z
.79
.87
,b.td
.7LO
.4370
.4360
.4995
.4985
.219
.250
.146
.L67
.025
.44 .724 .106 _ .01s
,030
qn .r23 .106 .020
NAS1109
NAS1110
NAS1112
NAS1114
.5625-18
.6250-18
.7500-16
.8750-14
.877
.865
.940
.928
1.064
1.052
1.252
r.239
1.01
1.09
1.23
r.44
.835
.89B
. n12
1,210
.5615
.5bu)
.6240
.6230
.7490
.7480
.8740
.8730
.281
.312
.375
.438
1BB
.208
.250
.292
.56 .L24
.62 .L24
.75 .128
.BB .134
.IAI
.141
.L47
.02c,
.04tI
.vzal
.045
.030
.050
.0315
.0611
1' 1976-NAs1i16
NAS111B
NAS1120
1.0000-12
1.1 250- 12
1.2500-12
t.440
7.427
L.627
7.614
1,815
1.801
r.oo
1,BB
2.10
1.398
1.585
L.772
.9990
.9980
L.1240
7.L225
1.2490
L.2475
,s00
.562
.625
.375
,417
1.00
t.12
r.25
DEscRrprroNb] srnrus NorEs, NAs38o' @_F_ofR THRUTNACTTVE FOR DESTGN AFTEiR JULY
SEENASS2O3
sEE
.139
.170
.L70
.141
l Aa
.14I
n4q
.070
.055
NAS6zz-u-'
corurer-rrEt-Y REVISED
PROCUREMENT
SPECIFICATION
NATIONAL AEI1OSPACE STAND{lDSiglullt4Ifi-
TITLE
BOLT, SHEAR' HEXAGON HEAD
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NAS1118 Datasheet
Recommendation NAS1118 Datasheet
Part NAS1118
Description Bolt / Shear
Feature NAS1118; Iz O :ul 6z tr U 9eE 6 =oz :N -N 6z<> =tez U :a 1 )i Uz*+-<5 ;i: to4u aT =56oxx6zvi AF 3# 9< Hz .
Manufacture AIA
Datasheet
Download NAS1118 Datasheet




AIA NAS1118
NATIONAL AEROSPACE STANDARD
o coPYRrcHT 20to AERospAcE rNDUsrRrEs AssocIATr.N oF AMERrca, rNc. aLL RTGHTs REsERvED
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BASIC (r) (u)
PART
NUMBER
X
/tl
NAS1103 .276 .016 .005
NAS1104 ?1A .018 .006
NAS1105 .375 .02r .008
NAS1106 ?ot .021 ,009
NAS1107 .453 ,vzJ .010
NAS1108 .453 .025 .011
NAS1109 .511 .028 .012
NAS111O .543 .028 ,UI5
NAS1112 .572 .031 .018
NASl114 .652 .036 .020
NAS1116 .770 .042 ,uzz
NAS11i8 .864 .042 .025
NAS1120 .958 .042 .028
INSPECTION DATA
/r/
,0045
z
/2/
.0040
ULT TNSL
LBS MIN i8l
2,490
.0045 ,0030
4,520
.004s .0030
7,240
.006 .0025
10,950
.006 .0025
14,900
.0r05 .0020
19.950
,006 .0020
25,300
.006 .0020
31,950
.009 .0020
46,550
,009 ,0020
63,600
.0r09 .0020
82,900
.0119 .0020
106,900
.0"12 .0020
134,000
ii[ffi ffiALLOY
STEEL
- 4140 rUNS G414OO) PER
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IREATMENTT
FINISH:
i,;X!ig, titi:13fl..$ti*opERrrEs AS FoLLows, wrrH coNrRoLS pER AMs_rr_68r5€R
NO
'W"
CODE
CODE
- CADMTUM
- CADMIUM
p_!A.T_E_p-B
PLATE PER
AMS_QQ_P_416,
N[,IS-!b-P.A,6,
TypE rr,
ryPE I,
CLASS
CLASS
2.
3,
CODE:
DASH NUMBER DESTGNATES GRrp AND LENGTH lSrr fnerr +1.
rvi,iilA?pDl_sDD_r-'ulcwD._',"pAAAFFLrrTEENRRUDDMAABSSHEHRNN=UUUMyNqBDEERRRrLFrLooERnDDsHRniriGrrrripij['vifjri6vnrNrse.. lai
ARMNGE CODE LETTERS Ar-PHNAETTCATIV,'rilCNr APPLICABLE.
EXAMPLES:
,;;NAS'104-10
NAs1104-10D
NAS'1O4-1OW
NAS1104-10DW
=
=
=
=
.2500-28
.2500_28
.2500-28
.2500_28
BP9o.LLIi,
AOIi
Boai;
,'q62i5l
.62i
GRIP,
eirib,
Criib]
Gi#;
iUirNU-DrRDIILEsDHASNHKA,NrKy,prEyPrEr
II PLATING.
pLArrNG.
j[irr'rr_O,_rueioLED SHANK TYPE I PLATING.
sHANK rypE r pLArrNG.
{1/IrlorES:
&qyT,t$Firy: "gs,, AND "@D" WrrHrN "x,,'ALUI:S FrM. ,,aD,AND THREAD prrcH DTAMETER WrrHrN
,i,, SHANK STMIGHTNESS: WITHIN ',2' VALUE' FIM PEII IN.H oF LENGTH.
/?/ GRIP LENGTH: FROM UNDERSIDE OF HEAD To END I3F FULL .YLINDRICAL P'RTI.N oF SHANK.
/f/ COTTER PIN HOLE CENTERLINE: WITHIN ,O1O AND I\IORMAL WITHIN 20 OF BOLT CENTERLINE,
TNACTTVE FOR DESTGN AFTER
FoR pEscRrprroN oF srArui
JULY L,
rvores,
srgr7r6r.$uEiisEieNoA. S6203
THRU
NAS6220.
d @) covrnirrElY' REVTsED
I
ffifitil$,,Hsj#rgl[{ry



AIA NAS1118
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NATIONAL AE:ROSPACE STAN DARD
@ CoPYRIGHT 2010 AERosPAcE INDUsTRIEjs AssocIATIoN oF AMERICA, INc' ALL RIGHTS RESERvED
/tr\ REMOVE ALL BURRS AND SHARP EDGES,
(6)
t7t
t8t ACCORDANCE WITH NASM1312-8. TENSILE TEST IS NOT REQUIRED FOR PARTS WITH A GRIP LEqS THAN
2 x rHE NOMINAL DIAMETER. IF REQ|UIRED, TENSILE TESTING oF Bolrs.RE.Qllry,Ng9lo:::Plttto
THREADS SHALL BE PERFORMED PRIIfR TO DRILLING AND
COATINGS. WHEN BOLTS HAVE BEEN DRILLED, STRENGTH
THE APPLICATION
MAY BE VERIFIED
OF
BY
PLATING'AND/OR
SHEAR TESTING,I IN
LIELI
OF TENSILE TESTING, IN ACCORDAN,CE WITH NASM1312. USERS SHOULD BE AWARE THAT FASTENERS
- .*"."W\ ITH CROSS DRILLED THREADS MA\'EXHIBIT A REDUCTION IN TENSILE STRENGTH.
(9) btverusrotls IN INcHES AND Apply AFTER FINISH UNLESS oTHERWISE SPECIFIED.
(10)
*TOLEMNCES UNLESS OTHERWISE SPECIFIED: ANGLES 5"
(1 1)
(12)
(13)
51RI\DARD TAKES PRECEDENCI: OVER DOCUMENTS REFERENCED HEREIN.
''15
REFERENCED DOCUMENTS SHALL BE THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BID.
UNLESS OTHERWISE SPECIFIED, PAFIT INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OT THE
APPLICABLE DMWING OR SPECIFICI\T]ON MAY BE PROCURED AND USED UNTIL STC}CK IS DEPLF.TED.
(r4) DulIlvMltErl\NJlS(JIlO\rlN\uING AHNl\vD TI OvLLLEIuMlruNrlCruING IliPLErR\ AnrNrrSr I YI 1r 4.5M-1982'
t]5l DASH NUMBER INDICATES GRIP IN ,0625 INCREMENTS, INTERMEDIATE OR LONGER LENGTHS MAY BE
SPECIFIED BY USE OF WHOLE DASH NUMBERS ONLY'
PROCUREMENT SPECIFICATION: NAS49L .TENSION LOAD INSPECTION VALUES AS TABULATED ABOVE.
INACTM FOR DESIGN AFTERJULY t, L976. SEE NAS62O3 THRU NAS6220.
FOR DESCRTPTTON OF STATUS NICTES, SEE NAS38O'
=<x;il6ot9zs>929^<
=du
@ couer-erELY REVISED
USE OF OR RELIANCE UPON THIS DOCUN4ENT OR ANY NAT]ONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY' AIA DOES NOT QUAUFY
CONFORN4ANCE OF ITEN'IS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AlA MAKES NO REPRESENTATION OR CLAIM RESPECTINCi
S(iU) PTPHLEIESI9UI9TA1B-9IU5TIYiryO-F
rrtMs ron nNy pnnnlcuLAR ApplrcATioN oR (2) THE EXISTENcE crF oR APPLICABILITY THERETO oF PATENT oR TMDEMARKS RIGHTS.







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