AN104601至AN104700(版本3)空军-海军航空标准 螺栓CRES六角头 190 32(1986年6月30日)

ID:43775

大小:0.07 MB

页数:1页

时间:2023-03-16

金币:20

上传者:战必胜
FEo.SDP.CLASS.
~3~
5906
r
MATERIAL IDENTIFICATIONPER
AmM300 .
RAISED OR DEPRESSED
.010 MAX
\ -.~
+20 MIN
SECTION T~U T~EAD
PROFIIJZ
.190 (NO.1O) -32 NF-3J4
SPEC MIL-S-7742
L
;?:2
.500
.562
.625
.688
:l?;
.875
.938
1.000
.150J
.090
K
+.
000
-.060
[:]
H
a
a
e
.125
.188
.250
.312
:?;3
PART NO.
kNI04606
AN1046o7
kN104608
4N1046o9
kN104610
IN104611
lN104612
iN104613
iN104614
LN104615
LN104616
~TNIS SURFACE NOST 8S SQUARE WITH
SHANK WITHIN .003 FuLL INDICATWl
READING
~ ~w~ 30*To .375D~
(OPPOSITESIDEOPTIONAL)
L
1.062
1.125
1.188
1.?50
1.312
1.375
1.4>8
1.500
1.625
1.750
1.875
2.000
2.125
2.250
2.375
K
+.
000
-.060
-
.500
.562
.625
.688
.750
.812
.875
.938
1.062
1.188
1.312
1.438
1.562
1.688
1.812
PARTNO.
AN104617
AN1046I8
AN104619
A?J10462O
AN104621
AN104622
AN10462>
AN104624
AN104625
AN104626
AN104627
AN104628
AN104629
AN1046>o
AN1046>1
L K
+.000
-.060
2.500
1.938
2.625
2.062
2.750
2.188
2.875 2.312
3.000 2.4>8
3.125
2.562
3.250
2.688
3.375
2.8K?
3.500
2.938
3.625
3.062
3. 50
i
3.188
3. 75 3.312
1
PART NO.
AN104632
AN104633
AN104634
AN104635
AN1046>6
AN104637
AN104638
AN104639
AN10464O
AN104641
AN104642
AN104643
L
K
+. 000
-.060
PART NO{
(a)
THREAD TO HEAD. MAXIMUM TWO IMPERFECT THREADS.
NOTE :
(1)
SHANKSHALLBESTRAIGHT WITHIH
.004
FIR. PERINCHOFSOLT LENGTn.
(2) “THE CONCENTRICITY OF THREAD PO IN RELATION TO THE
SHANK SHALL BE WITHIN .006 FIR.
(3) THE CONCENTRICITY OF THE SNANK IN RELATION TO TIIEWASHER
FACE DIAMETER AND HEXAGON
SHALL BE UITHIN
.011FIR.
HA~IAL t CfXIROSIONRESISTAIPTSTEEL - SES MANUFAC1’URIN(ISPECIFICATION!
.WUSFACEROUUHN33SS: AS107
~ACT~ING SPECIFICATION: AM 7472
~ INSPECTION: ALL PARTS SHALL UNDERCX) FLUORESCENT PENETRANT 1NSPECTION INACCORDANCE WITH AMS2645,
BREAK
SHARP EDGES .003-.015 UNLESS OTHERUISE SPECIFIED.
DIMENSIONS IN INCHES.
uNLESS OTHERWISE SPECIFIED:
TOLERANCES ;
LINEAR OIISENSIONS !.010, ANGULAR
DIMENSIONS t2”.
DO NOT uSE UNASSIGNED PART NUMSERS.
INACTIVE FOR NEW DESIGN AFTER 27DEC 1966
ND SUPERSEDINGSTANDARD.
THIS STANDARD UAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PABTS COMMITTEE OF THE SAE.
-L
P,A.
USAF - 11
Other
C“nt
Mtvy-AS
Arpy-AV
AIR FORCE-NAVY AERONAUTICAL STANDARD
ANl
4601
BOLT - CRES NEX HEAD .190-32
8
AN1’
‘4700
* U. S. GOVER””EW ?F,N,,NG WFKX: _ 34,. s17/A. 4931
ProjectNo.5306-1030
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