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NASM20426 PDF даташит

Спецификация NASM20426 изготовлена ​​​​«AIA» и имеет функцию, называемую «Nut».

Детали детали

Номер произв NASM20426
Описание Nut
Производители AIA
логотип AIA логотип 

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NASM20426 Даташит, Описание, Даташиты
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NATIONAL AEROSPACE STANDARD
©COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED
NATIONAi AfROWACf STANDARD$
FED. SUPPLY CLASS
5320
100°±1/2°
(B)
/6/
E ""I
LENGTH ±.010
R .010 MAX
C(APPROX
ATERIAL FOR
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MATERIAL IDENTIFICATION MARKS
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1100 (A)
PLAIN
5056 (B)
RAISED CROSS
2117 (AD)
DIMPLED .020 MAX
2024 (DD)
RAISED DOUBLE DASH
(INACTIVE)
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RAISED TEAT
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INDENTED RING
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INDENTED SQUARE
(INACTIVE)
2219-T62 (J)
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With The Permission Of AIA/NAS
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THIRD
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PROJECTION
PROCUREMENT
SPECIFICATION
NASM5674
CUSTODIAN
NATIONAL AEROSPACE STANDARDS COMMITTEE
TITLE
RIVET, SOLID, COUNTERSUNK 100°, PRECISION HEAD,
ALUMINUM AND TITANIUM COLUMBIUM ALLOY
REVISION
3
CLASSIFICATION
PART STANDARD
NASM20426
SHEET 1 OF 7
USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY
CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AIA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABiLITY OF
TTFMS FOR ANY PARTTn JI AR APPi TrATTON OR (7) THF FXTSTFNrF OF OR APPi ](":ARTI TTY THFRFTO OF PATFNT OR TRAnFMARKS Rll,HTS.









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NASM20426 Даташит, Описание, Даташиты
74/A
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NATIONAL AEROSPACE STANDARD
© COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED
NAJIONAt A!ROS?ACf STANDARDS
0A
±.004
.114
.179
.225
.286
.353
.415
.476
.564
.694
TABLE I - RIVET DIMENSIONS
(B) c
0D
E
+.003
-.001
.022 .094
.062 (1/16)
.004
.036 .141
.094 (3/32)
±.002
.042 .188
.125 (1/8)
.005
.055 .234
.156 (5/32)
±.002
.070 .281
.187 (3/16)
.006
.083 .328
.219 (7/32)
±.003
.095 .375
.250 (1/4)
.008
±.003
.106 .469
.312 (5/16)
.010
.134 .562
.375 (3/8)
±.004
sT
RAD
.016 .019
.023 .029
.031 .039
.039 .049
.047 .059
.054 .069
.062 .078
.078 .098
.094 .117
MATERIAL:
ALUMINUM 1100-F (UNS A91100) AND ALUMINUM ALLOYS 2017-T4 (UNS A92017), 2024-T4 (UNS A92024), 2117-
T4 (UNS A92117), 2219-T62 (UNS A92219), 2219-T81 (UNS A922119), 5056-H32 (UNS A95056), 7050-T73 (UNS
A97050) PER QQ-A-430 AND TITANIUM COLUMBIUM ALLOY 45Cb (UNS R58450) PER AMS4982.
EXAMPLE OF PART NUMBER:
MS20426 AD 4 - 12 A -5 = ALUMINUM ALLOY 2117-T4 RIVET, 1/8 DIA. (3/4 + 1/32) LONG, ANODIZE CLEAR.
-- -- L INDICATES ADDITIONAL 1/32 INCH INCREMENT IN LENGTH.
- NO CODE INDICATES CHEMICAL SURFACE TREATMENT PER MIL-DTL-5541,
CLASS lA, GOLD/YELLOW.
"A" INDICATES ANODIZE PER MIL-A-8625, TYPE II, CLASS 1, CLEAR.
~ "D" INDICATES ANODIZE PER MIL-A-8625, TYPE II, CLASS 1, DICHROMATE SEAL.
"F" INDICATES OPTION OF ANY FINISH EXCEPT AS NOTED BELOW.
"S" INDICATES CHEMICAL SURFACE TREATMENT PER MIL-DTL-5541, CLASS lA, CLEAR.
- "N" INDICATES ANODIZE PER MIL-A-8625, TYPE II, CLASS 2.
NOTE: FOR 1100 AL. CHEMICAL SURFACE TREATMENT PER MIL-DTL-5541, CLASS lA,
GOLD/YELLOW (NO CODE).
FOR 2024 AL. ANODIZE PER MIL-A-8625, TYPE II, CLASS 1, DICHROMATE SEAL OR CLEAR
OR CLASS 2 WITH SPECIFIED COLOR (A, D, ORN CODE).
FOR 2017, 2117, 2219, 5056 AND 7050 AL. CHEMICAL FINISH SURFACE TREATMENT PER
MIL-DTL-5541, CLASS lA, CLEAR OR GOLD/YELLOW (CLEAR FILM SHALL BE USED ONLY
WHEN AUTHORIZED) OR ANODIZE PER MIL-A-8625, TYPE II, CLASS 1 (CLEAR OR
DICHROMATE SEAL) OR CLASS 2.
FOR TITANIUM COLUMBIUM, NO FINISH REQUIRED.
~-INDICATES LENGTH IN 1/16 OF AN INCH.
' - - - - - - INDICATES DIAMETER IN 1/32 OF AN INCH.
- "A" INDICATES 1100-F ALUMINUM
"AD" INDICATES 2117-T4 AL. ALLOY
"B" INDICATES 5056-H32 AL. ALLOY
"D" INDICATES 2017-T4 AL. ALLOY - (INACTIVE FOR NEW DESIGN)
"DD" INDICATES 2024-T4 AL. ALLOY - (INACTIVE FOR NEW DESIGN)
"K" INDICATES 2219-T81 AL. ALLOY- (INACTIVE FOR NEW DESIGN)
"E" INDICATES 7050-T73 AL. ALLOY
"T" INDICATES TITANIUM COLUMBIUM ALLOY 45Cb
- "J" INDICATES 2219-T62 AL. ALLOY
' - - - - - - - - - BASIC MS NUMBER
G) COMPLETELY REVISED
REVISION
3
NASM20426
SHEET 2
USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLIERS OR CERTIFY
CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AJA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF
ITEMS FOR ANY PARTICULAR APPLICATION OR 121 THE EXISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARKS RIGHTS.









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NASM20426 Даташит, Описание, Даташиты
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NATIONAL AEROSPACE STANDARD
©COPYRIGHT 2013 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED
NATIONAL AFROS?ACE STANDARDS
NOTES:
/1/ .001 INCH SHANK DIAMETER INCREASE PERMISSIBLE WITHIN .100 INCH OF BASE OF HEAD.
/2/ RIVETS MAY BE FURNISHED WITH PLAIN ENDS, OR CHAMFERED ENDS WITH A RADIUS TO THE "T" DIMENSION
OR A 20° CHAMFER TO THE "S" DIMENSION.
/3/ A PROFILE VIEW OF LAND AREA MAY VARY FROM A LINE PARALLEL WITH THE SHANK TO A CURVE THAT WILL
FALL WITHIN THE LIMITS ALLOWED.
/4/ THE CONICAL SURFACE OF THE HEAD SHALL BE CONCENTRIC WITH THE SHANK OF THE RIVET WITHIN .005
(.010 FIM).
/5/ HEAD-COCKING ANGLE RELATIVE TO AXIS OF RIVET 1/2° MAX.
/6/ MAXIM.UM HEAD DIAMETERS ARE TO THEORETICAL SHARP CORNERS AS MEASURED BY PROJECTION.
(7) FOR PART NUMBERS OF RIVET LENGTH NOT LISTED SHOW 1/16 INCREMENT REQUIRED.
(8) ADDITIONAL 1/32 LENGTH INCREMENTS MAY BE OBTAINED BY ADDING -5 AFTER THE LAST DIGIT OR LEDER
IN PART NUMBER.
/9/ OUTER DIAMETER OF INDENTED RING (7050 RIVETS) SHALL BE A MAXIMUM OF 75% OF RIVET SHANK
DIAMETER. THE MAXIMUM DEPTH OF THE RING SHALL BE .Ol!YINCH. INDENTED RING IS REQUIRED ON 7050
RIVETS MANUFACTURED AFTER 2 JULY 1990.
/10/ MANUFACTURER'S IDENTIFICATION IS REQUIRED TO BE DEPRESSED ON RIVET HEADS WITH A SHANK
DIAMETER .125 INCH AND LARGER MANUFACTURED AFTER 2 JULY 1990.
/11/ ALUMINUM ALLOY 2017-T4 RIVETS WITH 33 KSI MIN. UNDRIVEN SHEAR STRENGTHS ARE ACCEPTABLE UNTIL 2
JULY 1990.
(12) DIMENSIONS ARE IN INCHES AND APPLY AFTER FINISH UNLESS OTHERWISE SPECIFIED.
(13) UNLESS OTHERWISE SPECIFIED, TOLERANCES: DECIMALS ±.010.
(14) INTERCHANGEABILITY RELATION WITH AN426 RIVETS: MS20426 RIVETS OF LIKE DASH NUMBERS ARE
UNIVERSALLY, FUNCTIONALLY, AND DIMENSIONABLY INTERCHANGEABLE.
(15) IN THE EVENT OF A CONFLICT BETWEEN THE TEXT OF THIS STANDARD AND THE REFERENCES CITED HEREIN,
THE TEXT OF THIS STANDARD SHALL TAKE PRECEDENCE.
(16) 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.
(17) UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURED TO PREVIOUS REVISIONS OF THE
APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED.
/
(18) DIMENSIONING AND TOLERANCING PER ANSI Y14.5M-t982.
REVISION
3
G) COMPLETELY REVISED
NASM20426
SHEET 3
USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY. AJA DOES NOT QUALIFY SUPPLIERS OR CERTIFY
CONFORMANCE OF ITEMS PRODUCED UNDER NATIONAL AEROSPACE STANDARDS. AJA MAKES NO REPRESENTATION OR CLAIM RESPECTING (1) THE SUITABILITY OF
ITEMS FOR ANY PARTTCLJLAR APPLICATION OR 17) THE EXISTENCE OF OR APPLTCABfLTTY THERETO OF PATENT OR TRADEMARKS RIGHTS.










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