/’4
(a) u m“ 08
32
znPx2vxcTP3!2M
A+2m
x
FED. SUP
CLASS
5307
2s2n2RuLTm
smYPIosl mm
c2sAnma.04-7.45Q
m IIt-’
~;;y
lb
NAslPIIR.onx45~
TERKAD
PRoPISx
ArP210x
APPUOX
BOT’3TED9XZ&9
W-*
#l
-- II J
II II
.090
.-
*
.040
e-.
C D1
..
II
;&9:
L--’ -’--
-J”
.250-2oNs
21NDSRXIZEAHD 0TUR62XB
SER
TAB2a mR PD
IDLNWIFICATIONSTAMP
PM Ais22800 .010MAX mm
.250.28UW?-3A
1
RIM-7742
+.003
0
3
—
.245-.250
.2243-.2253
.2248-.2263
.2185-.2205
J’#y$#=
A.u.u;;~;
*
AN126223
Ns326229
AN126001
AS226235
M126007
AS32601>
AR326019
*
AW326043
ASJ126049
*
bJi126073
An$32J9
*
AUU261OY
AR226109
+%&
AX126133
A31126139
+%&
Am.2616>
Anr26169
W
AN126193
MU26199
AN126205
AN126211
AmR;mRcmlm
aTAmP POR
ANs 26430.010
UAx D3Pr6
NOTE:
PITCH OIAMETERS OF BOTH THREAOEO ENDS SHALL BE CONCENTRIC WITHIN .006 FIR.
(a)
CROSS THREAOING PERMISSIBLE AT THREAO RUNOUTS ON SHORT STUDS.
MATERIAL: STEEL AUS 6322.
(AK+ 6320 MATERIAL HAY ALSO BE USED FOR THESE PARTS UNTIL 1 JAN 1960.)
HARDNESS: ROCKWELL C26-32.
FINISH:,CAD!41Ut4PLATE AM’S 2400.
DIMENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN.
SURFACE ROUGHNESS :
AS291. MANUFACTURING SPECIFICATION AUS 7456.
1NSPECTION:
DO NOT USE UNASSIGNED PART NUMBERS.
ALL PARTS SI!ALL UNDERGO KAGNETIC INSPECTION IN ACCORDANCE WITH AMS2640.
BREAK SHARP EOGES
.003-.015 UNLESS OTHERWISE SPECIPIEO.
I
<
OINENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED:
TOLERANCES :
(b)
LINEAR DIMENSIONS f.010.
INACTIVE FOR NEW OESIGN AFTER 31 MAY 1958
TU7S STANDARD WAS DFVF1.OPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILI”TYPARkS COMNITTEE OF THE SAE.
PA 11
AIR FORCE-NAVY AERONAUTICAL STANDARD
AW:151
CUST: AV. AS
1--
11’
STUD - STRAIGHT, .250-20 , .z50-2F!
AM
126274
.!),-—, ,— o,m.am,.,,,.,,”,.,,
ProjectNo.5307-0342
T2SJ,S.GOVERNMENT PRINTING OFFICE: 1986 — 605-036/43942
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