$
,
ares;
:
b ~~;v’-‘‘ 3
.120,.030
..—
.562
.500
D1A
MIN
EH
:-
--
-.
.31 1A
.3s
.3125-24UN%3A
~k
SPEC MIL-s-7742
2
mns SmACE mm BE SQUARE
w1mi w WITHIN .003 FIR.
CHMXER 30° TO .500 DIA
(OPPOSITE SIDE OPTIONAL)
SECTION l’WJJTHREAD PROFILE
L
+ .:00 PART NO. L
+.;OO PART NO. L
+.;OO
..060
PART NO. L
+ .:00
PART NO.
-.060
-,060
-.060
1.375
.688 AN101218
2.750 2.062 AN101232
4.5o0 3.812
1.438
,750
AN101219
2.875
NJ101246
2.18a
.625
(a)
AN1012o6
1,500
AN101233
.812 AN10122O
3.000 2.312 PN10123k
j::;: ~:~g mm:~J
.688
(.)
AJ1012O7
1.562
,875
AN101221
3.125
2,u38
AN101235
4.875
4.188
.750
(a)
AN1012O8
1.625
AN101249
.938 AN101222
3.250
2.562
AN101236
5.000
4.312
.812 .125 AN1012C9
1.682 1.000
AX101223
3.375
2.688
AN10125O
AN101237
5.125
4.438
AN101251
.875
.12a AN10121O
1.750 1.062.
AN101224
3.500 2.812 AN101238
5.250
4.562
.938 .250 AN101211
1.875
1.188 M4101225
AN101252
3.625
2.938 AN101239
1.000
5.375
4.688
.312
AN101253
AN101212 2.000 1.312 AN101226
3.750
3.062 AN10124O
5.500
11.812
AN101254
1.062
.375
.4N101213
2.125 1.438
1.125
.J138
AN101214
2.250
1.562
;:% ~:y; ::% W;]:
;:%
:%: W%
1.12a .500 AN101215 2.375
1.688
3.438
5.875
5.188
1,250 .562 AN101216
;:g 1.812 AN10123O
4.250 3.562 AN1012J44
6.00o
5.312
1.312 .625
AN101217
1.938 AN101231
4.375
3.688
AN101258
AN101245
(m) TmEAD TO HEm. mxmum mo IMpERFEcT mms.
‘m: {;1
stmti SHm BE STRAIGHT MITHIN .003 FIR.pm INCH OF 00LT LENGm.
m CONCENTRICITY OF m!m.m PD IN RELATION TO THE SHANK SHALL BE WITHIN .006 FIR.
W CONCENTRIC1l”l OF ~E SHANK IN RELATION TO l’liEWASHER FACE D1MC3TER AND HEXAGON
SHALL BE WITHIN .015 FIR.
MATZRIAL , STEEL. AK36322
HARDNESS , ROCKWELL c26-32
FINISH : CADMIUM PLATE .hMs2400
SUXi?ACERODGMME$S , AS107
rmlNG “’’:1’7: ‘7”52
INSPECTION MLPAR?95iALL
UNDERGOMAGNETIC Q4S2ECTIONIN ACCC=DANCE WITH AM=64Q.
)X SHARP EDGES 003 015 -S 03”iCiRW1SESPECIFIED.
D1uENS1ONS IN lNCi+?S UNL2L3SDTHERMISE SRECIPIED:
T0mA)+cZ3 ; LINEAR D1M?.NS1ONS i.010, ANGUIJR
D1WS1ONS *2..
DO NOT USE UNA?.S1ONT.DPUT NlJTL3&PS
INACTIVE FOR NEW DE SIGN AFTER 3 )w.m 1969 NO SUPERSEDING STANDARD.
THIS STANDARZ WAS DEVELOPED COOPERATIVELY BY TH3 ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE ME.
AIR FORCE-NAVY AERONAUTICAL STANDARD
Ph. AF-11
AN IO1201
l“RU
CUST, NAVY-AS
BOLT - HEX ift#zD.3125-24
ARW-AV
AN IO1300
53 G6-0997
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