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PDF NAS1352 Data sheet ( Hoja de datos )
| Número de pieza | NAS1352 | |
| Descripción | Screw / CAP / Socket Head | |
| Fabricantes | AIA | |
| Logotipo |  |
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 1. Head Cap Screws - Aerospace  Hay una vista previa y un enlace de descarga de NAS1352 (archivo pdf) en la parte inferior de esta página. Total 6 Páginas | ||
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*NAArTroIONNAALL AEERROoSsPpAACcEE STANDARD
'TANDARD ffijBIO COPYRIGHT 2009 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC, ALL RIGHTS RESERVED
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FED. SUPPLY CLASS
WHEN SELF-LOCKING ELEMENT IS SPECIFIED:
HEAD MARKING OF A MINIMUM OF SIX (6)
DOTS, MISED OR DEPRESSED,IS REQUIRED.
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TOP OR SIDE LOCATION OPTIONAL.
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a.
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IDENTIFICATION
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FOR NUMBER OF HOLES,
sEE NOTE (d)
MIN,
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THREAD SIZE
FILLET (9)
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M (a)
K
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TABLE I
NOMINAL
stzE
DASH
THREAD
SIZE
D
BODY
DIAMETER
HEAD
DIAMETER
H
HEAD
HEIGHT
S
HEAD
SIDE
HEIGHT
J
SOCKET
SIZE
T
KEY
:NGAGEMEN.l
MIN.
WALL
THICKNESS
MIN.
N
CHAMFER
OR MDIUS
MAX.
NO.
MAX,
MIN,
MAX. MiN, MAX. MIN.
MIN. NOMINAL
01
.0730-64 naa .0695 .1 1B
r72 .073 .070
.066
.062
.031
.025
.003
02
.0860-s6 .086 .0822 .140
1?4 .086 .083
.077
.078
.038
.029
.003
F
03 .0990'48 .099 .0949 .IOI
154 .099 .095
.089
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.1900-24 .190 .1840 .JIZ
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4
.2500-20 .250 .2435 .375 .365 .250 .244
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5
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.450
.375
.213
.245
166 .010
190 .010
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10 ,6250-1 1 .625 ,6163 .937 .92I
.616
.562
.500
.307
.238
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.370
.285
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1.0000-B 1.000 .9886 1.500 L.479 1.000 .988
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20 L.2500-7 1.250 1.2336 1,87s 1.852 1.250 L.236 1.125 .875
.495
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.475
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24 1.5000-6 1.500 1.4818 2.250 2.224 1.500 1,485 1.350 1.000
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Reproduced By IHS
With The Permission Of AIAJNAS
Under Royalty Agreement
THIRD
ANGLE
PROJECTION
CUSTODIAN
NATIONAL AEROSPACE STANDARDS COMMITTEE
REVISION
11
PROCUREMENT
SPECiFICATION
E
d NOTED
TITLE
SCREW, CAP, SOCKET HEAD, UNDRILLED AND DRILLED, PLAIN AND
SELF-LOCKTNG, ALLOY STEEL, CORROSION-RESISTANT STEEL AND
HEAT-RESISTANT STEEL, UNRC-3A AND UNRC-2A
CLASSIF]CATION
PART STANDARD
INAS1352
SHEET 1 OF 5
USE OF OR REUANCE UPON THIS DOCUN4ENT OR ANY NATIONAL AEROSPACE STANDARD I5 ENTIRELY VOLUNTARY. AIA DOES NOT QUAUFY SUPPUERS OR CERTIFY
CONFORT4ANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS, AIA [4AKE5 NO REPRESENTATION OR CLAI[4 RESPECNNG (1) THE SUITABIUTY OF
1TEMS FOR ANY PARTICULAR APPUCATTON OR (2) THE EXISTENCE OF OR APPUCABILITY THERETO OF PATENT OR TMDEMARKS RIGHTS.
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NATIONAL AEERROoSsPACcEE STANDARD
"ATT'NAL 'TANDARD RESERVED@ COPYRIGHT 2009 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS
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EMtt4PLE: NAS1352-02-8
NAS1352C04H12
NAS1352-O8LE16P
=
=
=
NAS1352C4LL24P
NAS1352N10LN32 =
NAS1352N12LB36S =
NAS1352N4LB16B =
.0860-56 UNRC-3A SCREW, CAP, SOCKET HEAD, ALLOY STEEL, UNDRILLED HEAD,
PLAIN, .5OO INCH LONG, BLACK OXIDE FINISH.
.1L20-40 UNRC-3A SCREW, CAP, SOCKET HEAD, CORROSION-RESISTANT STEEL,
DRILLED HEAD, PLAIN, .750 INCH LONG, PASSIVATED.
.1640-32 UNRC-3A SCREW, CAP, SOCKET HEAD, ALLOY STEEL, SELF-LOCKING,
OPTIONALTYPE LOCKING ELEMENT, 1.OOO INCH LONG,
CADMIUM PLATE, UNDRILLED HEAD.
.2500-20 UNRC-3A SCREW, CAP, SOCKET HEAD, CORROSION-RESISTANT STEEL,
SELF-LOCKING, LONGITUDINAL STRIP LOCKING ELEMENT,
1.500 INCHES LONG, CADMIUM PLATE, UNDRILLED HEAD,
.6250-11 UNRC-3A SCREW, CAP, SOCKET HEAD, HEAT-RESISTANT STEEL, SELF-
LOCKING, PELLET LOCKING ELEMENT, 2.000 INCHES LONG,
PASSIVATED, UNDRILLED HEAD.
.7500-10 UNRC-3A SCREW, CAP, SOCKET HEAD, HEAT-RESISTANT STEEL, SELF-
LOCKING, PATCH ryPE LOCKING ELEMENT, 2.250 INCHES
LONG, SILVER FLASH, UNDRILLED HEAD.
.2500-20 UNRC-3A SCREW, CAp, SOCKET HEAD, HEAT-RESISTANT STEEL, SELF-
LOCKING, PATCH TYPE LOCKING ELEMENT, ]..OOO INCH LONG,
BLACK OXIDE COATING, UNDRILLED HEAD.
NOTES:
(1) LOCKING ELEMENTT
EXCEPT AS NOTED HEREIN. THE LOCKING ELEMENT WHEN SPECIFIED SHALL BE IN
ACCORDANCE WITH MIL-DT1.18240 AND SHALL BE FULLY ENGAGED WHEN USED.
(2) IDENTIFICATION:
MANUFACTURERTO IDENTIFYALL MINIMUM PACKAGES BY PACKAGE MARKING OF
APPLICABLE COMPLETE NAS STANDARD PART NO. IN ACCORDANCE WITH MIL-STD-13o.
(3) DIMENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED DIMENSIONSAND TOLERANCES SHALL BE IN
ACCORDANCE WITH FF-S-86, TYPE VI AND ASME 818.3.
(4) REFERENCED DOCUMENT5 SHALL BE OF THE ISSUE IN EFFECT ON THE DATE OF INVITATION FOR BID.
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(s) THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS SPECIFIED HEREIN.
(6) ADDITIONAL PART N4ARKING SHALL BE IN ACCORDANCE WITH FF-S-86,
(7) UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE APPLICABLE
DMWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED.
(8) REMOVE ALL BURRS AND SHARP EDGES.
@/q'\ DELTTED
PROCUREMENT SPECIFICAT]ON: FF-S-86: UNLESS OTHERWISE SPECIFIED, CAP SCREWS FURNISHED UNDER
THIS STANDARD SHALL BE SUBJECT TO IN-PROCESS CONTROL AND/OR END
PRODUCT INSPECTION WHICH WILL INSURE MECHANICAL/ METALLURGICAL,
CHEMICAL AND COATING OR TREATMENT CHAMCTERISTICS WHEN SAMPLED
IN ACCORDANCE WITH ASQ 21.4, INSPECTION LEVEL S-1, 10lo AQL.
REVISiON
11
nlAS1352
SHEET 5
USE OF OR REUANCE 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 REPRESENTAT]ON OR CLAIM RESPECTING (1) THE SUITABIUTY OF
ITEMS FOR ANY PARTICULAR APPLICAT]ON OR (2) THE EXISTENCE OF OR APPLICABILIW THERETO OF PATENT OR TRADEMARKS RIGHTS.
5 Page | ||
| Páginas | Total 6 Páginas | |
| PDF Descargar | [ Datasheet NAS1352.PDF ] | |
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