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AIA

NASM35206 Datasheet Preview

NASM35206 Datasheet

SCREW

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Aerospace
Industries
Association
NATIONAL AEROSPACE STANDARD
@COWRIGHT 2004 AEROSPACE INDUSTRIES ASSOCUTION OF AMERICA. INC. ALL RIGHTS RESERVED
r n r ØD
/ It
FED SUP CLASS
5305
i
U
NOMINAL SIZE
TABLI 1. asst NUMBER!
.O86
.112
.190
.250
,3125 .375
THREADS PER INCH UNC-2A
OD BODY
0A HEAD
H HEAD HEIGHT
56 40
MAX
.O860
,1120
MIN .O717 .O925
MAX
.1670
.2190
MIN
.1550
.2050
MAX
.O620
.O800
MIN
.O530
.O700
24
.1900
,1586
.3730
.3570
.1330
.1220
20
.2500
,2127
.4920
.4730
.1750
.1620
18
.3125
,2712
,6150
5940
,2180
,2030
16
,3750
.3287
.7400
.7160
,2610
.2440
P HEAD RADIUS
MIN .o1O0 ,0100
,0200 ,0350
,0400 ,0400
R FILLET RADIUS
MAX
.O130
.O1 70
,0290 ,0380
,0470 .0560
TENSILE STRENGTH, LBS-MIN 2 /
~
L LENGTH
TOLERANCE
220 360
DASH
DASH
(UMBER NUMBER
1,050 1,900
DASH
DASH
NUMBER NUMBER
3,140 4,650
DASH
DASH
NUMBER rlUMBER
,125
,188
,250
.312
.375
.438
,500
.562
+.o00
-.O31
201 21 1
202 212
258
203 213
259
204 214 227 242 260 276
205 215 228
206 216 229
207 217
320 1/ 323 i/ 322370 1/
243 261
244 262
263
234351 1/ 337 1/
277 292
278 293
279 294
343 1/ 349 1/
307
355 i/
,625
,750
,875
1.O00
208 218 231
246
264 280
295
308
209 219 232
247
265 281
296
309
210 220 233
248
266 282
297
310
321 1/ 221
234
249
267 283
298
31 1
1.125
1.250
1.375
1.500
1.750
1.875
2.000
2.250
2.500
2.750
3.000
3.250
3.500
+.o00
-.O62
+.o00
-.O94
I/ INDICATES MANUFACTURER'S NON-STOCK
2/ SEE REQUIREMENT 7.
324 11 328
332
39:222
325 11
250
11 333 1/
322 I/ 223
236
251
326 1/
238
330
362
1 254
255
256
I 257
335 1/
336 1/
PRODUCTION ITEMS.
338 344
350
3: 1/ 3:; 1/ 3;: 1/
269 285
300
3: 1/ 3:s 1/ 35: 1/
27 1 287
302
272 288
273 289
274 290
303
304
305
275 29 1
306
341 347 11 353 i/
342 1/ 348 1/ 354 1/
URRENT
356
312
357 11
313
314
358
315
316
317
318
319
359 1/
360 1/
IEETS
1
mu
THE ORIGINAL RELEASE O F THIS DOCUMENT SUPERSEDES MS35206, REVISION H, AMENDMENT 1.
CUSTODIAN NATIONAL AEROSPACE STANDARDS COMMITTEE
PROCUREMENT
SPECIFICATION
FF-S-92
TITLE
SCREW, MACHINE-PAN HEAD, CROSS-RECESSED,
CARBON STEEL, CADMIUM PLATED, UNC-2A
I 4 I NEW
PART NUMBERS REMAIN MS35206.
THIRD
ANGLE
PRn.IFCTlnN
CLASSIFICATION
PART STANDARD
SHEET 1 OF 4
USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT OUALIM SUPPLIERS OR
CERTIM CONFORMANCE OF ITEMS PROCURED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE
SUITABILITY OF ITEMS FOR ANY PARTICULAR APPLICATION, OR (2) THE EXISTENCE OF OR APPLICABIUM THERETO OF PATENT OR TRADEMARK RIGHTS.
Copyright Aerospace Industries Association of America Inc.
Provided by IHS under license with AIA/NAS
No reproduction or networking permitted without license from IHS
Licensee=L3 Communications/5954372002
Not for Resale, 10/20/2005 14:23:17 MDT
Free Datasheet http://www.Datasheet4U.com




AIA

NASM35206 Datasheet Preview

NASM35206 Datasheet

SCREW

No Preview Available !

NATIONAL AEROSPACE STANDARD
@COPYRIGHT 2004 AEROSPACE INDUSTRIES ASSWTION OF AMERICA. INC. ML RIGHTS RESERVE0
0 -REQUIREMENTS:
1. MATERIAL. CARBON STEEL IN ACCORDANCE WITH PROCUREMENT SPECIFICATION.
2. ' CADMIUM PLATED IN ACCORDANCE WITH AMs-QQ-P-416,
TYPE 11, CUSS 3.
ZINC COATING IN ACCORDANCE WITH ASTM 8633-78, Fe/Zq 5 (5prn), TYPE 11,
3. THREADS: THREADS SHALL BE IN ACCORDANCE WITH FED-STD-H28/2.
ACCORDANCE WITH FED-STD-H28/20. SYSTEM 21
ACCEPTABILITY OF SCREW THREADS SHALL BE IN
4. JHRF4D L F N G M. SCREWS 2.000 INCHES LONG AND SHORTER SHALL HAVE COMPL€Ei THREADS EXTENDING TO WITHIN TWO
THREADS OF THE BEARING SURFACE OF THE HEAD OR CLOSER IF PRACTICABLE. LONGER SCREWS SHALL HAVE A
MINIMUM THREAD LENGTH OF 1.750 INCHES.
5.
un 6.
. 4tB.E€ES% THE RECESS SHALL BE IN ACCORDANCE WITH MS9006.
PART NUMBER. THE PART NUMBER SHALL CONSIST OF THE BASIC MS NUMBER FOLLOWED BY A DASH NUMBER FROM TABLE I.
EXAMPLE:
-
PROTECTIVE COATING CODE
Z INDICATES ZINC COATING
NO CODE INDICATES CADMIUM PLATING
LDASH NUMBER
BASIC MS NUMBER
-MS35206-201 INDICATES SCREW, MACHINE-PAN HEAD, CROSS RECESSED, CARBON STEEL, CADMIUM PLATED.
,086-56 UNC-2A. .125 LENGTH
-MS352D6-2012 INDICATES SCREW, MACHINE-PAN HEAD, CROSS RECESSED, CARBON STEEL, ZINC COATED,
.086-56 UNC-2A. ,125 LENGTH
7. m F STRF- ' BASED ON 60,000 PSI MINIMUM ULTIMATE TENSILE STRENGTH. LOAD POUNDS ARE CALCULATED BY THE
STRESS AREAS AS SPECIFIED IN FED-STD-H28/2.
NOTES:
1. ALL DIMENSIONS ARE IN INCHES
2. IN THE WENT OF A CONFLICT BETWEEN THE TEXT OF THIS STANDARD AND THE REFERENCES CITED HEREIN, THE
TEXT OF THIS STANDARD SHALL TAKE PRECEDENCE.
3. REFERENCED GOVERNMENT (OR NON-GOVERNMENT) DOCUMENTS OF THE ISSUE LISTED IN THAT ISSUE OF THE DEPARTMENT
OF DEFENSE INDEX OF SPECIFICATIONS AND STANDARDS (DODISS) SPECIFIED IN THE SOLICITATION FORM A PART OF THIS
STANDARD TO THE EXTENT SPECIFIED HEREIN.
4. SUPERSEDES: MS35204, MS35208. MS3521O, MS35221, MS35223. MS35225, MS35227; AND IN PART, MS24584(USAF).
MS35357, MS35359 THRU MS35362, MS35364 THRU MS35366, AN515 AND AN526, MS35366. AN515 AND AN526.
SEE TABLE 11, INTERCHANGEABILITY.
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SE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS C
ERTIFY CONFORMANCE OF ITEMS PROCURED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATIONOR CLAIM RESPECTING (1) T
UITABILIM OF ITEMS FOR ANY PARTICUCAR APPLICATION, OR (2) THE EXISTENCE OF OR APPUCABILIM THERETO OF PATENT DR TRADEMARK RIGHTS.
Copyright Aerospace Industries Association of America Inc.
Provided by IHS under license with AIA/NAS
No reproduction or networking permitted without license from IHS
Licensee=L3 Communications/5954372002
Not for Resale, 10/20/2005 14:23:17 MDT
Free Datasheet http://www.Datasheet4U.com


Part Number NASM35206
Description SCREW
Maker AIA
Total Page 4 Pages
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