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PDF NAS6707 Data sheet ( Hoja de datos )
| Número de pieza | NAS6707 | |
| Descripción | BOLT | |
| Fabricantes | NATIONAL AEROSPACE STANDARD | |
| Logotipo |  |
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Hay una vista previa y un enlace de descarga de NAS6707 (archivo pdf) en la parte inferior de esta página. Total 8 Páginas | ||
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NATIONAL AEROSPACE STAN DARD
@ coPYRIGHT 2013 AEROSPACE TNDUSTRIES ASSOCIAT!0N 0F AMERICA/ INC, ALL RIGHTS RESERVED
FED, SUPPLY CLASS
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MAX TWO
INCOMPIETE
THREADS
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POINT SHALT
BE FIAT AND
CHAI'4FERED. SEE
PROCUREIvIENT
SPECIFICATION FOR
DETAILS
arD lt3l
ao 16l
R
CHAM 15q *50
TO OC OPTIONAL
DRILL @P /4/ WHEN
No.SPECIFIED BY PART
csK oPTIONAL /18/
WHEN SPECIFIED BY
PART NUNIBER
UNJF'3A THREAOS PER ASB879 EXCEPT FOR
REDUCI]ON OF THREAD MAJOR DIAMETER PER OTD
-FIGURE 1 BOLT CONF]GUMTION
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BAS]C
NUMBER
NAS67O3
NAS67O4
NAS67O5
NAS67O6
NAS67O7
NAS6TOB
NAS67O9
NAS671O
NAS671 2
NAS67 1 4
NAS6716
N456718
NAS672O
THREAD
UNJ F.3A
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,2540-28
,3t25-24
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5000-20
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1,0000- 12
1 I ?qn-1 ?
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-TABLE I DIMENS
A B ava
M]N MIN
t3t
MAX
,376
,q5v
,502
. JO.+
,690
,752
,877
,940
t ,uoJ
L,252
1
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IVl]N
.JO/
,429
,492
,)5.i
.o,/d
,/a1r 1
,865
,9 28
1,052
r,239
1 A-1
1 801
,410
,480
,J'Z
,oz5
,764
,836
,978
1,050
l,fvt
l..f uJ
1,619
2,046
,398
,460
.t zJ
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,7 L0
,835
,898
L,UZJ
1,210
1.398
1,585
t,772
III\UtrU UI\ 5Ntrtr I
AD
UNPLATED
MAX
1895
2495
,3120
,37 45
,4370
,4995
,6240
,7490
,8740
,9990
1,1240
1,2490
MIN
1890
,2490
,JII5
,37 40
,4365
,4990
,5610
,6235
, /q65
,8735
,9985
t,1230
1,2480
PLATED OR COATE|D
MAX
,1895
,2495
,3120
,4370
4995
,6240
,7490
,8740
,9990
t,t24Q
t,2490
MIN
1B8l;
,2485
,3110
,373!;
,4360
,.tyu)
,560!'
,6230
,7480
,8730
,9980
1,t225
1,247 5
F H J 6K
trct +,015 IILI +nl
-,000
156
L/d
,208
.208
,250
250
,278
,278
?1)
,357
,416
.1i0
125
IJO
,188
,219
250
,26r
.312
,375
,438
,500
,562
,625
,094
,107
125
,125
. 150
t50
,t67
,167
,188
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250
250
250
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PROCURE14ENT
SPECIFICATION
NOTED
TITLE
BOLT, TENSION, HEX HEAD, CLOSE TOLERANCE, A28€i
CRES, LONG THREAD, REDUCED MAJOR THREAD DIA,,
SELF-LOCKING AND NONLOCKING, 160 KSI FtU
CLASSIFICATION
_ -PART STANDJRD
I,IAS67O3 THRU NAS672O
SHEET 1 OF 8
USEOFORRELIANCEUPONTHISDOCUMENTORANYNATiONATAEROSPACESTANDARDISENTIRELYVOLUNIARY.
AIADOESNOIQUAUFYSUPPLIERSORCERTIF/
CONFORMANCEOFITEI'lSPRODUCEDUNDERNAT]ONALAEROSPACESIANDARDS, AIAMAKESNOREPRESENTA.I.IONORCLqIT4RESPE TING(t)THESUITAEILIIYOF
ITEt.ls FOR ANY PART'ICUIAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABITITY THEREIO OF PATENT OR TMDEI4ARKS R1GHTS,
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NATITO'NNAL AEERROoSspPAAcCEE STANDARD
'TANDARD ffittQO COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA/ INC, ALL RIGHTS RESERVEO
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ITSI HEAD MARKING: BASiC NUMBER PLUS GRIP DASH NUMBER PLUS ''D,,, ''1,., OR UP,, WHEN APPLICABLE,
-PDLU' SIDMEANNTUIFFIEACSTUBROELTR'SWISTYHMDBORILL,LEMDISSEHDANOKR. DEPRESSED ,O10 MAX, ARMNGEN1ENT OPTIONAL,
"1"
-P"
JDENTIFIES
iDENTIFIES
BOLT
BOLT
WITH
WITH
LOCKING ELEMENT (OPTIONAL TYPE),
PATCH TYPE LOCK]NG ELEMENT ONLY.
"A" ALUMINUM COATED, *C'CHROME PLATED AND ''U', UBU AND NM' PASSiVATED PER. AMS2TOO
CODES NEED NOT APPEAR ON BOLT HEAD.
(16) SURFACE TEKIURE: -0D,,, HEAD.TO.SHANK FILLET, BEAR]NG SURFACE OF HEAD, THREAD FI-ANKS
AND THREAD ROOT: 32 MICRO]NCHES Ra; ALL OTHER SURFACES; 125 MICROINCHES Ra PER
ASME 846.1.
ITTI INTERMEDIATE OR LONGER LENGTHS MAY BE SPECIFIED BY THE USE OF WHOLE GRIP DASH
NUI'4BERS ONLY, NOMINAL LENGTH EQUALS NOMINAL GRIP PLUS "T",
ITsI IF REQUIRED, TENSILE TESTING OF BOLTS REQUIRING CROSS.DRILLED THREADS SHALL BE
PERFORMED PRIOR TO DRILL]NG AND THE APPLICATION OF PLATING AND/OR COATINGS, WHEN
BOLTS HAVE BEEN DRILLED/ STRENGTH MAY BE VERIFIED BY SHEAR TESTING, IN LIEU OF TENSILE
TESTING, IN ACCORDANCE WITH NASM1312. USERS SHOULD BE AWARE THAT FASTENERS WITH
CROSS-DR]LLED THREADS MAY EXHIB]T A REDUCTION ]N TENS]LE STRENGTH,
II9I TI.IE EFFECT OF COLD WORK AND AGING INDUCED DUR]NG THE MANUFACIURiNG CYCLE MAY
iilINCREASE THE ULTIMATE TENSITE STRENGTH OF THE FINISHED PART/ BUT ANY PART (TYPE ], ]] OR
AS IISTED IN NAS4003) SHALL NOT EXCEED 1,3 TIMES THE SPECIFIED TYPE I MINIMUIvI TENSILE
VALUES AS LISTED JN NAS4OO3 TABLE iII.
(20) DTMENSIONS TO BE MET AFTER pr-ATrNG,
(21) DTMENSIONS IN INCHES,
(22) REMOVE ALL BURRS AND SHARP EDGES,
(23) THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS REFERENCED HEREIN.
(24) REFERENCED DOCUMENTS SHALL BE THE ]SSUE ]N EFFECT ON DATE OF iNVITATIONS FOR B]D.
(25) UNLESS OTHERWISE SPECIFiED/ PART INVENTORY MANUFACIURED TO PREVIOUS REViS]ONS OF THE
APPLICABTE DMWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIT STOCK ]S DEPLETED,
PROCUREMENT SPECIFICATIONI NAS4OO3, EXCEPT AS NOTED. COLD WORK OF HEAD TO SHANK FILLET MDiUS AND
FATIGUE TESTING ARE N0T REQUIRED FOR NAS6703 BOLTS, LOCKING ELEMENT FOR SELF-LOCKTNG
BOLTSi PER NASM15981 AND MIL-DTL-18240, LOCKING
OPTIONAL WHEN UL" CODE IS SPECIFIED, PATCH TYPE
ELEMENT TypE, INCLUDING PATCH TypE,
LOCKING ELEMENT (WITH NO METAL
rS
REMOVED) IS REQUIRED WHEN "P" CODE I5 SPECIFIED, LOCKING ELEMENT MUST BE SUPPLIED BY A
QUALiFIED SOURCE LISTED IN QpL-1S240 OR APPROVED FOR LTSTTNG IN Qp1"18240, SHIpptNG
NOTICE SHOULD IDENTIry SUPPLIER OF BOLT AND LOCKING ELEMENT SEPAMTELY,
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REVISION
10
NA567O3 THRU NAS672O
ucosENFooFR0l4RARNEcLEIAoNFCITEEUMPsoPNRToHDIuScEDoOuTNUMDEENRTNA0RrtoANNAYLANEATRIOosNpAAL cAEEsRrAONSDPAACREDSsT,ANDAAtRADMIA5 KENETsIRNEoLRY EVpORLUENsTEANRYT,AAilIeAtoDnOcErS.qNrOuTneQsUiAeL-IoFYr'ljScUirPliPnLeIEsRuStrOARBClLErRfTioIFFY
NEMS FOR ANY PARTICULAR APPLICAT1ON OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS,
5 Page | ||
| Páginas | Total 8 Páginas | |
| PDF Descargar | [ Datasheet NAS6707.PDF ] | |
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