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rospace
ndustries
Association
NATIONAL AEROSPACE STANDARD
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MANUFACTURER'SID RAISED A286
OSERERNEOCTEESS1E1D. .010 MAX.
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.010 HIGH MAX OR
.O20 DEEP MAX
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DIA
.094 +.002
-.001
.125 +.003
-.001
.156 +.004
.187 -+..000014
-.001
_250 +.004
-.001
CA CA'
B
ABSOLUTE (REF)
MIN
.14g0
.1398
.1970i
.187_
.2487
.1260
.1739
.2251
.021
.029
,037
..2293887z
.2879
.3953
.3835
.2749
.3710
.046
.060
E
MAX
.006
.006
.006
.006
.008
OF
:b005
P
MAX MIN
OW
MAX MIN
ST
PAD
NO
RECESS
.070
.080
.0123 .0089 .1192 .1190 .023 .029
.0141 .0106 .1628
.0189 .0153 .2028
.1626 .031 .039
.2026 .039 .049
.100 .0225 .0188 .2441 .2439 .047 .059
.125 .0263 .0223 .3315 .3313 .062 .078
UST OF CURRENT SHEETS
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CUSTODIANNATIONALAEROSPACESTANDARDSCOMMITTEE
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PROCURMENT
SPECIFICATION
NONE
TITLE
RIVET,SOLID,100 DEG FLUSHSHEARHEAD,A286
CORROSIONRESISTANTSTEELAND
PROJECTION
CL_SSlFICAT_N
STANDARD PART
NAS1200
MONEL
SHEET 1 OF 2
_,__=.,__.o,o_.___.,._,,_._u._U.OE...T.,-O-O._S.S.OTE..O.R,,D, ,S,,_. .0RE_RESO_.0__O.,R.. ESPE(,_)"r,..E_USE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VOLUNTARY.
NA DOES NOT QUALIFY SUPPLIERS
OR
http://www.Datasheet4U.com
,.HT U_" UI:M::; POH ANY PARTIGUI AR APPtlCATION. OR (2) THE _'XISTENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADEMARK RIGHTS.

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_erospace
ndustries
Association
NATIONAL AEROSPACE STANDARD
_ "_ '_'_'_ "_'_
_'=_'_-_"_
I
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BASIC
PART
DIA
LENGTHS AND DASH NUMBERS
NUMBER
.125 .188 .250 .312 .375 .438 .500 .563 .625 .688 .750
II
___ NAS1200-3 .094 -2 .-3 -4 -5 -6 -7 -8 -9 -10 -11 -12
NAS..1200-4 .125
-3 -4 -5 -6 -7 -8 -9 -10 -11 -12
C_
NAS120G-5 .156
-4 -5 -6 -7 -8 -9 -10 -11 -12
NAS1200-68 ..215807
-4 -5 --66 --77 -86 -9 . -10 -11 --1122
<- _
BPAARSITC
DIA
-
LENGTHS AND DASH NUMBERS
NUMBER
.813 .875 .938 1.000 1.125 1.250 1.375 1.500 1.750 2.000
_Ed_ _
=/_=l_.u:d
z tu_
_=_
NNAASS11220000--43
NAS1200-5
NA91200-8
NAS1200-8
..019254
.156
.187
.250
--1133 --1144 --1155 --1166
-13 -14 -15 -16
-13 -14 -15 -16
-13 -14 -15 -16
-18 -20
-18 -20 -22
-18 I -20 1-22
-18 1"20 -22
-24
-2z_
-24
-28
-28
-28
-32
-32
-32
?,,,__z NOTE: MONEL RIVETS WITH LENGTHS TO THE RIGHT OF THE HEAVY UNE ARE NOT AVAILABLEWITH RADIUSED ENDS
MATERIAL:
A286 (UNS $662861 - Corrosionand heat resistantwire per AM_5734.
MONEL (UNS N04400) - Nickle-Copper-Ailoywire per QQ-N-281, Class A (Annealed).
SHEAR STRENGTH AT ROOM TEMPERATURE:
A256 - 85 KSl TO 95 KSI as heat treated.
90 KSI MIN after driving.
MONEL - 49 KS! TO 59 KSI, as received.
See Note 12.
HEAT TREAT:
A286 - Solu_on_'eat and par_allypred_
heat treat alter afterheadingas follows:
Heat at 1650 F +/- 25 for 25 minutes- Oil quench.
Age at 1250 F Io 1350 F for 30 to 90 m_as as necessaryto meet shear requiremen=.
Air Cool.
FINISH:
A295 - Pessivateper QQ-P-35.
MONEL - Only when spedfied, CADMIUM plate per QQ-P-416, TYPE II, CLASS 2.
CODE:
"M" in place of _,st dash in_
MONEL
>;
:::)
¢b
_.
c_
"P" after last dash numberindicatesCadrnlumplate for MONEL only.
EXAMPLES OF PART NUMBERS:
i"
i_
,
NA_1200Mi'_P
== "125 D|A,
"500 LENGTHe
MONEL
RIVET*
C*_0J_M| u a PLATED
N_1200-4-8-5 = .125 DIA, .531 LENGTH, A286 RIVET (SEE NOTE 10)
NOTES:
1. Tolerances: Unless otherwises_
.¢ .010.
2. .001 shank diameter increasepem_Ls____Ne .10 inches of base of head.
3. Shank and head diametersshall be cor_eflldc within.010 for rivets Itu'u .125, within .015 for .156 and .187 rivets,
andwithin .O2Ofor .25O_ets, RM.
4. Rivetsshall drive oold sa'dsfactedlywith full heads free from _acks.
5. Rivets must be of uniformquarWand free lrornscale, r,'zs,seams, cinch or die marks, cold shuls, or oiler
F_
_)
6. Head ¢o¢idngangle relativeto ¢ds of rivet .500 deg MAX.
7. Mmdmumhead diametemate to _eoret_! sham comersas measuredby projecti_.
8. See N/L3527 for the reconuneccled_
for irspe_ng head characterblics.
8.Thebea_m_y mabye_ _ a_"_"c_on,
lO._d_or_.o_1V3_remem_ aybeoUaV_byadd_-g5a_te_r =st_t ofparnt umber,
(_)11. JMuanneu1fa9cot-u..r3e.r_identificationis requiredon rivet heads with shank diameter.125 inchand larger manufacluredalter
12. Do_Jbleshearstrengthtests shall be in accoRtan_ with MIL-STD-1312, Test 13 or ASTM B565. Single shear
stmctgthtastingper MIL-STD-1312, Test 20.
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SHEET 2
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