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NAS1008 डेटा पत्रक PDF( Datasheet डाउनलोड )


डेटा पत्रक - Bolt / Head - AIA

भाग संख्या NAS1008
समारोह Bolt / Head
मैन्युफैक्चरर्स AIA 
लोगो AIA लोगो 
पूर्व दर्शन
1 Page
		
<?=NAS1008?> डेटा पत्रक पीडीएफ

NAS1008 pdf
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NATIONAL AEROSPACE STANDARD
@ COPYRIGHT 2014 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED
ADD"H"TO DASH NUMBER FOR DRILLED HEAD ONLY,
NO CODE LETTER DESIGNATES DRILLED SHANK ONLY.
OF PART NUMBER:
NAS1003-8 = .1900 DIAMETER BOLT, .500 GRIP, DRILLED SHANK ONLY.
NAS1003-8A = .1900 DIAMETER BOLT, .500 GRIP, UNDRILLED.
NAS1003-8H = .1900 DIAMETER BOLT, .500 GRIP, DRILLED HEAD ONLY.
/1\ REFERENCE DIMENSIONS ARE FOR DESIGN PURPOSES ONLY AND NOT AN INSPECTION REQUIREMENT.
(2) MAGNETIC PERMEABILITY SHALL BE LESS THAN 2.0 (AIR= 1,0) FOR A FIELD STRENGTH H = 200 OERSTEDS
USING A MAGNETIC PERMEABILITY INDICATOR PER ASTM 43421A342M, TEST METHOD 3,
(3) REMOVE ALL BURRS AND SHARP EDGES.
(4) THESE BOLTS ARE INTENDED FOR USE AT TEMPEMTURES UP TO 12OO"F.
tst GRIP LENGTH: FROM UNDERSIDE OF HEAD TO END OF FULL CYLINDRICAL PORTION OF SHANK.
t6l COTTER PIN HOLE CENTERLINE: WITHIN .010 AND NORMAL WITHIN 2' OF BOLT CENTERLINE.
t7t "Of'|" MAXIMUM NOT TO EXCEED "B"; MINIMUM DIA AT TOP OF HEAD NOT LESS THAN "0H."
t8t CONCENTRICITY: ..@H,,AND "OA,,WITHIN "X" VALUES FIM, "OA" AND THREAD PITCH DIAMETER WITHIN
"Y" VALUES FIM.
I9I SHANK STMIGHTNESS: WITHIN "2" VALUES FIM PER INCH OF LENGTH.
i 10/ BEARING SURFACE SQUARENESS: WITHIN .OO3 FIM WITH SHANK.
(11) DIMENSIONS IN INCHES AND APPLY AFTER FINISH UNLESS OTHERWISE SPECIFIED. TOLERANCES UNLESS
OTHERWISE SPECIFIED: ANGLES + 5".
1S*
/13/ ULTIMATE TENSILE STRENGTH IS BASED ON A NON-DRILLED FED-STD-H2812 THREAD AREA AND 14O,OOO
PSI. FOR BOLTS WITH CROSS-DRILLED THREAD, A REDUCED SECTION SPECIMEN MAY BE MACHINED FROM
THE PART AND TESTED TO VERIFY THAT BASIC MATERIAL PROPERTIES MEET OR EXCEED 14O,OOO PSI
MINIMUM.
i14l DISCALOY INACTIVE FOR DESIGN AFTERJULY 1, 1979.
/15/ NAS1O16A INACTIVE FOR DESIGN AFTER JULY L, L979.
/16/I DASH NUMBER INDICATES GRIP LENGTH IN .0625 INCREMENTS. INTERMEDIATE OR LONGER LENGTHS MAY
BE ORDERED BY USE OF PROPER DASH NUMBER.
(17) FOR DESCRIPTION OF STATUS NOTES, SEE NAS380.
(18) THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS REFERENCED HEREIN.
(19) 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.
(20) UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE
APPLICABLE DMWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED.
(2i) DIMENSTONING AND TOLERANCTNG PER ANSI Y1.4.5M-1982.
A57477 EXCEPT AS NOTED. ULTIMATE TENSTLE STRENGTH ( LBF MIN ) LOAD VALUES AS TABULATED
HEREIN.
@
OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY
IRN4AI\CE OF ITEN'lS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA N'IAKES NO REPRESENTATION OR CLAIM RESPECNNG (1) THE SUITABILITY OF
FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TMDEN4ARKS RIGHTS.

विन्यास 3 पेज
डाउनलोड[ NAS1008 Datasheet.PDF ]


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