NASM 14200-1999 nut, floating, self locking, attached, retention element (a.r.e.), 450 deg. f, steel, 125 ksi ftu, replaceable nut element.pdf

1、NASM 14200-1999 nut, floating, self locking, attached, retention element (a.r.e.), 450 deg. f, steel, 125 ksi ftu, replaceable nut element_NASMl4 2 O O ADOPTION NOTICE NASMl4200, NUT, FLOATING, SELF-LOCKING, ATTACHED, RETENTION, ELEMENT (A.R.E.) 450F STEEL, 125 KSI FTU, REPLACEABLE NUT ELEMENT, was

2、adopted on 14 DECEMBER 1999 for use by the Department of Defense (DoD). Proposed changes by DoD Activities must be submitted to the DoD Adopting Activity: Defense Supply Center Philadelphia, ATTN: DSCP-ILEA, 700 Robbins Avenue, Philadelphia, PA 19111-5096. DoD Activities may obtain copies of this st

3、andard from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094. The private sector and other Government agencies may purchase copies from the AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC., 1250 EYE STREET, N. W., WASHINGTON, DC 20005- 3924. Cust

4、odians : Army - AR Navy - AS Air Force - 11 DU- IS Adopting activity : DLA-IS (Project 5310-0716) AMSC N/A FSC 5310 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling

5、ServicesAerospace Industries Association NATIONAL AEROSPACE STANDARD coFwGnl19o9 KROSPACE ltwJsmEs ASMQATHII W MleRlch Hc al. mfs EsEREo FED SUP CUSS 5310 I. APPUCATION ANO OESIGN SELECTION: THESE A.R.E. (AllACHEO RETENTION ELEMENT) NUT ASSEMBLIES SHALL BE SELECTED AND USED IN ACCORDANCE WITH MS3358

6、8. 3. -NUTS: MSI 4201 OVERSIZE NUTS MAY BE USED A5 REPLACEMENT FOR M51 4200 NUTS. 5. GNFRAl RFPUIRFUFm 5.1 PERFORMANCE PER MIL-N-25027: INSTALLATION HOLES SHALL BE PER TABLE 11, PANEL GRIP THICKNESS PER TABLE 111. 5.2 MATERIAL: 5.2.1 NUT ELEMENT: STEEL AISI 1050 PER AMs 5085 OR AISI 4130 PER AMs 635

7、1. 5.2.2 SLEEYE: CRES AISI 304 PER AhlS 5639 OR AlSI 305 PER AMS 5514. 5.2.3 CAGE STEEL NSl 1050 PER AMs 5085. 5.3 HEAT TREAT: 5.3.1 NUT ELEMENT: ROCKWELL C49 MAX. 5.3.2 CAGE: ROCKWELL C40-47. 5.4 COATING: 5.4.1 SLEEVE ANO CAGE SHALL BE CADMIUM PLATED PER QQ-P-416. lYPE II CUSS 2. 5.4.2 NUT ELEMENT

8、SHALL BE CADMIUM PLATED PER QQ-P-416. lYPE AND CLASS OPTIONAL PROWDEO THE ELEMENT MEETS THE SALT SPRAY REQUIREMENTS OF MIL-N-25027. 5.5 LUBRICANT 5.5.1 NUT ELEMENT ONLY SHALL BE DRY FILM LUBRICATED PER MIL-L-46010, TYPE I. 5.6 SURFACE TEXTURE: 5.6.1 SURFACE TEXTURE IN ACCORDANCE WlTn ANSI/ASHE 946.1

9、 UNLESS OTHERWISE SPECIflECl, WE SURFACE ROUGHNESS SHALL NOT EXCEED 125 MICRO NCHES. 5.7 NUT FLOAT. 5.7.1 MINIMUM RAOIAL FLOAT 0.020 INCH. THE NUT ELEMENT SHALL eE CAPABLE OF ENGAGEMENT WITH THE BOLT IN MAXIMUM MISWGNED POSITION. 5.8 NUT REPLACEABIUPI: 5.8.1 ME NUT ELEMENT SHALL BE REMOVABLE FROM M

10、E CAGE WITH THE PROPER REMOVAL TOOL, ANO A NEW NUT PER MSI 421 4 SHALL BE CAPABLE OF BEING SNAPPED IN PLACE IN THE CAGE. FOR THE REPUCEMENT OF THE NUT ELEMENT IN ACCORDANCE WITH MS14214 ANO THEN THE NUT SHAU MEET THE TORQUE OUT ANO PUSH OUT VALUES OF MIL-N-25027. 5.8.2 CAGE REUSABILITY: CAGE SHALL B

11、E CAPABLE OF BEING REUSEO A MINIMUM OF 5 nMEs 5.9. WORKMANSHIP: 5.9.1 BREAK ALL SHARP EDGES ANO REMOVE ALL BURRS ANO SLIVERS. 5.9.2 DIMENSIONS ARE IN INCHES. 5.9.3 TOLERANCES: DECIMALS f.010. ANGLES 55 UNLESS OTHERWISE SPECIFIED. 5.1 O INSTALLATION: WHEN INSTALLED INTO PROPERLY PREPARED HOLES, USING

12、 PROPER TOOUNG, THE SLEM SHALL 8E CAPABLE OF FLARING SMOOTHLY WITH NO VISUAL EVIDENCE OF CRACKING OR SPLITTING. UST OF CURRENT SHEET THE INITIAL RELE4SE OF THIS DOCUMENT SUPERSEDES MS14200. REVlSlON B. PART NUMBERS REMAIN MS14200. CUSTODIAN NATIONAL AEROSPACE STANDARDS COMMITTEE ANGLE THIRD PROJECTI

13、ON PROCUREMENT TITLE CLASSIFICATION SPECIFICATION NUT, FLOATING, SELF LOCKING, ATTACHED PART STANDARD MIL-OTL-25027 RETENTION ELEMENT (A.R.E.), 450F, STEEL, 125 KSI Ftu, REPLACEABLE NUT ELEMENT NASM 14200 SHE3 1 OF 3 COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by In

14、formation Handling ServicesH 0318743 0507128 bTO E NATIONAL AEROSPACE STANDARD cam, 1990 KROSPACE INOUZTRIES =MN OF AVWU INC. ML RIGHTS RO 6. JLI USTRATIW MANUFACTURERS IDENTIFICATION MARK ON CAGE ANO NUT ELEMENT LOCATION OPTIONAL SHAPE OF LOCKING 1 A I PORTION OPTIONAL NUT ELEMENT (MS14214) 1 ANTI-

15、ROTATION DASH SIZE NO. SIZE MAX *.O10 MIN MAX . THREAD A 0 OC OD E 0F G H J K M V SENC LBS MIN AXIAL (a) MIL-S- MIN MAX MIN *.O10 MAX f.OlC REF MAX. +.o10 -.Ooc (b) -.ao0 04 .1120-40 UNJC-38 .310 .318 .182 .217 ,228 .234 ,116 .155 ,214 ,064 .O62 .435 ,020 750 I 06 1.1380-32 UNJC-381 .310 I .318 I .1

16、82 I .217 1.228 I .234 I .142 I .155 1.214 I .O64 I ,062 I .435 I .O20 I 1130 I o8 .1640-32 UNJC- ,405 ,425 ,235 ,270 .ma .304 ,168 ,187 ,270 ,075 ,068 sa7 .o25 1720 3 ,1900-32 UNJF-38 .405 .425 .235 -270 .296 .304 .194 .I87 .270 .O75 .O68 ,587 .O25 2460 4 ,2500-28 UNJF-38 .465 .496 J00 .335 .363 .3

17、69 .254 .198 325 .O83 .O89 .665 .O35 4580 (a) ASSEMBLY DASH NO. IS THE SAME AS MS14214 NUT ELEMENT SIZE DASH NO. (b) K = (THREAD RELIEF. SLEEVE FLANGE AND CAGE THICKNESS) I NASM 14200 PRESENTAnON OR CLAIM RESPECTING (1) THE RIGHTS. COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS

18、)Licensed by Information Handling Servicesrn 0338743 0507329 537 m NATIONAL AEROSPACE STANDARD .ornM 1999 AEROSPACE INWsmES ASSOMllON Of AIlERlCh INC. U RlCHlS REplFJED -I T, L 9. TAB1 E 111 04 .222 .217 ,307 .275 .312 06 .222 .217 ,307 .275 .312 I 08 I .285 I .280 I ,370 I .343 I .375 I 3 (e) I .28

19、S I .280 1 370 I .343 I 375 I 4 (e) I .352 I .347 I .437 I N/A I St5 10. PART WFR FxqMeLE; h614200 - O8 - 6 I TT II LGRIP DASH NUMBER (SEE TABLE Ill) LSIZE DASH NUMBER (SEE TABLE I) I MILITARY STANDARD NUMBER 1- WEIGHT GRIP GRIP THICKNESS T1 LBS/lOO OAsH NUMBER (f) (COUNTERSINK) -1 . 8 ,134-,165 6 ,

20、107-,133 10 ,166-.tg6 12 .197-.227 14 .228-.258 16 .259-,289 18 .290-.320 20 ,321 -351 22 .352-382 24 .383-.413 26 .414-.444 28 .445-.475 30 ,476-.SO6 GRIP T2 ILI N/A I .O73 I I I .O31 -.O62 (e)/ .O99 I .063-.O94 1 1 .095-.125 .126-.156 I .192 I .157-.187 1 2: I .188-.218 +%I .344-.374 .409 ,375-.40

21、5 1 :z 1 ,406-.436 .437-,467 ,502 (c) INSTALLATION MAXIMUM AND MINIMUM HOLE LIMITS CAN BE REDUCED BY .O09 INCH FOR SIZE DASH NO. 08, 3 AND 4 WHEN INSTALLING IN SOFT MATERIALS, INCLUDING ALUMINUM ALLOYS WITH HARDNESS NOT EXCEEOING BHN 110 OR ROCKWELL 870. (d) COUNTERBORE IS OPTIONAL TO BE USED IN APP

22、LICA- TIONS REOUIRING SURFACE FLUSHNESS. FOR THE MIN- MUM GRIP THICKNESS OF EACH GRIP DASH NO. COUNTERBORE CAN BE INCREASED TO .O30 TO INSURE ROUOMR FLUSHNESS. (e) NUT OF SIZE DASH NO. 4 SHALL NOT BE INSTALLED IN GRIP THICKNESS LESS MAN .O60 INCH. ON THICKNESSES LESS THAN .060, THE HOLE DIAMETER FOR

23、 SIZE -3 SHALL BE ,276-.281 (f) TO OBTAJN WEIGHTS FOR DIFFERENT GRIP DASH NOS. ADD INCREMENTS OF .O10 LE. FOR SIZES 04 AND 06 ADD ,020 LB. FOR SIZES 08. 3 AND 4. 11.1 IN THE MN1 OF A CONFLICT BETWEEN THE TEXT OF THIS DOCUMENT ANO THE THE REFERENCES CITED HEREIN, THE TEXT OF THIS DOCUMENT SHALL TAKE

24、PRECEDENCE. 1 1.2 UNLESS OTHERWISE SPECIFIED, ISSUES OF REFERENCED DOCUMENTS ARE THOSE IN EFFECT AT THE nME OF SOLICITATION. 11.3 THE AR. NUTS WITHOUT MANUFACTURERS lOENTlflCAnON MAY BE FURNISHED FROM MANUFACTURERS STOCK UNTIL DECEMBER 31, 1985. 11.4 THE A.R.E. NUT ASSEMBLIES IDENTIRED HERUN ARE PRO

25、PRIETARY PRODUCTS OF DEUTSCH FASTENER CORPORAnON AND ARE COVERED BY THE FOLOWING PATENTS: U.S. 3,695.324 (EXPIRING OCTOBER 3. 1989); 22 17 490 (EXPIRING MARCH 31, 19921 ME COMRNMENT DOES NOT HAM ROYALR FREE LICENSE. 3,765.078 (EXPIRING OCTOBER 6, 1990 FRANCE 72.1 1463 (EXPIRING APRIL 13. 1990). GERMANY NASM 14200 01 QI m c COPYRIGHT Aerospace Industries Association of America, Inc. (AIA NAS)Licensed by Information Handling Services主营业务范围：ASTM、NAS、NASM、MIL、ISOOOO、EN、DIN等技术标准翻译；技术资料翻译。业务QQQQQQQQ：2298175560专业诚信质量不满意，可不付款专注于技术翻译