1 ‘
,,
3ECTION 17iRUTHREAD PROFIL.3
K
+.ko PAST NO. L
.4 + .000
PART NO. L A
K
L A
+.cao
PAST NO.
-.c60
-,60
0
1.750 1,640
1.125 AN102O26
b .375
U.265
3.750
JJJ102O4
:% :2% [:1 %%%
;:% ;:i;:” ;:;% %%$
::2:; ::% 2;% %:%!
.625
.515
(.)
AN102OIY3
2.125
2,015 1,500 .4N102O29
4.750
k.640
4:123
.&a .578
(a)
AN1020C9
AM102O5O
2.250
2.140 1.625
.750
.640
.125
JN102O1O
AN102O3O
2.375 2.265
1.750
AN102O31
;:% i :$2 ::%
ti::%2
.812
.702 lee AN102O11
2,500
2.390 1.875
.875
AN102O32
5,125
5.015 &.5oo IJI102O5
.765
.250
AN102O12
2.625 2,515 2,000 AN1U2033
5.250
5.140
4.625
M102C5
i
.938 .828
.312
A3J102O13
2.750 2.640
2.125
AN102O34
5.375
5.265
b.750
AII102$?35
1.030
.890
.375
.4N102O14
2.875
2.765
1.0s2
.952
L!38
AN102O15
2.250 AN102O35
5.5CQ 5.3W
4.875 Awlo’2@36
3.000 2.890
2.375
AN102o36 ,;@~
5.515
1.125 1.015
.500 AN102o16
3,125
3.015 2.500 AN102O37
5.6m
::m& :X=
1.18a 1.078
.562
1.250
AN102O17
3.250
3.lko 2.625
1,1*O
.625
AN102O38
AN102o18
1.312
3.775
3.265
2.’/50
1.20-2
6&?
AN102O39
AN102O19
3.500
gu?g
;:%
;:%
~~
3.390
2,875 AN102O4O
;:?:: ;:;:2 X2 :%% ::8 ;::i: :{% iutu~:
1.500 1.390
.875 AN102O22
3.765
1.562
1.452 .938 AN102O23
4.000 3.890
3.375
1.625
.4N102O24
AN102OU4
1.515 1.000
u.125
b.m~
3.500
1,6&3 1.578
1.C62 AN.102O25
4.250
AN102O45
ll,luo
3.625 AN1020&6
(*) ‘17CiEADTO HEAD. MAXIMUM ‘TWO IMPERFEcT ‘THREADS.
‘m: /;/
SHANX SHALL BE STRAIGHT WImIN c03 PIR.PER INCH OF BOLT I.ENOm.
m CONCENTRICITY OF mRE.43 PD IN RELATION m THE SHANK SHAU BE W13311N .006 FIR.
THE CONCENTRIC1l”i OF THE SHANK IN RELATION TO THE WASHER PACE D1- AND IIEXAOCN
SHALL BE WITHIN ,013 FIR.
MMTRIAL, STEEL Am6322
HARDNESS : R’XKUELL c26-32
FINISH: CADMIUM PLATE AMS2400
SU8XACE ROUOHNESS : AS107
MANUFACTURINO SPECIF1 CATION : M37452
~>+ ,ti:,::f
~ IIEPECTIOW ALL PARTS SJIAI.LUNDER(2J2MAGNETIC INSPECTION IN ~OUMNCE WTTH AMS2640
BIIEAXSHARP EEGES G03- .015 UNLESS 0T8ERW1SE SPECIFIED.
DIILEILSICm IN INCHE3. utrm.ssC71YERWISE SPECIFIED: TOLmANcm; L183m DImSIONS *.010, mauur.
DImNslONS *2..
~ NOT uSF,lJNP.SSIGNZCPART NUMBERS
INACTIVE FOR NEW DESIGN AFTER 3 MARCH 1969 NO SUPERSEDINGSTANOARO.
3w1S STANDW.D WAS DEVELOPEE COOFERATIVTLY BY THE ENGINE AND PROPELLER UTILITY PARTS CCNll?TEX W lT+KSW.
AIR FORCE-NAVY AERONAUTICAL STANDARD
P. A. A~-11
ANI02001
THaU
CUST: NAVY-AS
, ARw-.Av
BOLT HEX HEAD, DRILLED SHANK, .250-28
ANI02100
Project No. 6306-1005 .
. .
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