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Reproduced By IHS
Vvith The Permission Of AIAJNAS
Under RoyaltyAgreement
NATIONAT AEROSPACE STANDARD
O COPYRIGHT 2014 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC, ALL RIGHTS RESERVED
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IDENTIFY PER
NAS1347, TYPE II
*---+-_
DRILL @K WHEN SPECIFIED.
BREAK SHARP EDGES
LENGTH + ,015
(GRIP, NOM + J, NOM) +.010
.020 + .005
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DRILL @M WHEN
SPECIFIED /6/
THREADS PER
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- @TABLE I DIMENSIONS AND STRENGTH VALUES
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MATERIAL:
1.801
CRES, 4286 (UNS 566286) pER AMS573t, AM55732, AMS5737 OR AMS5B53,
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HF FINISH:
CLEAN AND PASSIVATE IN ACCORDANCE WITH AMS27OO, METHOD 1, CLASS 4.
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CODE:
BASIC PART NUMBER DESIGNATES NOMINAL DIAMETER.
DASH NUMBER DESIGNATES GRIP AND LENGTH (SEE SHEET 3).
ADD "A"TO DASH NUMBER FOR UNDRILLED BOLT.
CUSTOD]AN
NATIONAL AEROSPACE STANDARDS COMMITTEE
PROCUREMENT
SPEC]FICATION
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NOTED
T]TLE
BOIT, MACHINE,
HEXAGON HEAD, A286 CRES
usE oF oR RELIANCE UPON THIS DOCUI4ENT OR ANY NATIONAL AEROSPACE STANDARD 1S ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SLtppLIERS
CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESP'ECN.NG (1) THE SU
'ITEN4S FOR ANY PARTICULAR APPLICATTON OR (2) THE EXISTENCE OF OR APPLICABIU'IY THERETO OF PATENT OR TMDEMARKS RIGHTS:
,
CERTIFY
]IL,ITY OF
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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.

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NATIONAT AEROSPACE STANDARD
@ COPYRIGHT 2014 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED
TABLE II _ LENGTHS AND DASH NUMBERS
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