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A# NATIONAL AEROSPACE STANDARD @ COPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC, ALL RIGHTS RESERVED H NO[4/2 +.010 i8l-\\ POINT SHALL BE FLAT AND CHA14FERFD. SEE PROCUREIqENT SPECIFICATION FOR DETAILS DR]LL OP /4/ WHEN ' LOCK]NG ELFIYE[17 SPECIFIED BY PART NO, WHEN SPECIFIID BY CSK OPTIONAL /13/ PART NUIT1BER, DRrLr ON (3 HOLES) /14/ ,,..,.-1-!,\\' - I AD 161 --t R cHA[4 15. +5. TO OC OPT1ONAL UNJF-3A THREADS PER ASB879 EXCFPT FOR REDUCTION Ot THREAD N1AJOR DIAIV]ETER PER OTD FIGURE 1 - BOLT CONFIGURATION TABLE i - DIN4ENSIONS (CONTINUED ON SHEET 2) d<Yo-' <-3L ;tt' v]: Hq J<r -o> Id! I aasrc i iHREAD-l A - | ruuvreen I ur,r:r-:n I I I ivnxF,u'rr - il-- - uJ i ,r7vv- 04 | .2500- ns 1 ?rla 606 |+607 o O o a z l F o zo d o d L F O t USE OF OR REL.IAr\\CE UPON THIS DoCJqENT OR ANY NATIONAL AFROSpACF STANDARD tS ENTIRELY VOLUNTARY. AIA DOES NCT QUAUFY SUppLtERS OR CERTTF\\ coNFoRFIANCEOFITENTSPRODUCFIIUNDERNATIONALAEROSPACESTANDARDS. AtAIYAKESNOREPRESENTATIONORCLAIMntSp'tC-illtC(1)THESUITABILITYOf ITEI4S FOR ANY PARTICULAR APPLICATION OR (2) THE EXISTENCE OF OR APPL]CA8IL]TY THERETO OF PATENT OR TMDEI,4ARKS RIGHTS. \\- HEAD N1ARKING /15/ a a ao oP BASIC NUMBER THREAD UNJF-3A jA iMAXI [4IN B N4IN MIN t3t OD tr t10t H +.015 -.000 l lfit 1.01 MAX MIN NAS66O3 .376 .367 4i0 .33s 1895 1885 156 110 .094 19 NAs6605 .3125 24 .50 .492 s52 460 3120 3110 .208 156 r25 J1 @ coverrrELY REVTsED Reproduced By IHS With The Permrssron Ot AIA/NAS Under Royalty Agreement CUSTODIAN NATIONAL AEROSPACE STANDARDS COMMITTEE REVISION I PROCUREMENT SPECIFIC}T1ON NOTED TITLE 4\\ BOLT, TENSTON, HEX HEAD, CLOSE TOLERANCE, \\y ALL_qY STEEL, LONG THREAD, REDUCED MAIOR DIA.,SELF-LOCKING AND NONLOCKING, 150 KSI FtU CLASSIFlCATION PART STANDARD NAS66O3 THRU 6620 SHEET 1 OF 7

o o o -- _ a=Y *ls OI oI az uu $rF 2P,<E aZ n ;-1 IY f<c IdU NATIONAL AEROSPACE STANDARD O COPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIAT1ON OF AMERICAI INC' I'LL RIGHTS RESERVED USE OF OR RELIANCE UPON THIS DOCUI4ENT OR ANY NATIONAL AEITOSPACE SIANDARD ]S ENT]RELY VOLUNTARY. A]A DOES NOI QUALIFY sUPPL]ERS OR ':RTIFY CO\\FORI'IANCEOFITEi'4SPRODUCEDUNDERNATIONALAEROSPACESTANDARDS. AIAMAKESNOREPRESENTATIONORCLATNIRESPECTING(1)THESUITABIUTYOF I TEMS FOR ANY PARTICULAR APPUCATION OR (2] THE EXISTENCE OF OR APPUCABJLITY IHERETO OF PAIENT OR TRADEVARKS RIGHTS c TABLE I - D]MENSIONS (CONTINUED) BASIC NUMBER I\\4 r.010 ON +.010 -.000 AP +.010 -.000 t4t R RAD S +.015 -.000 (r) tst U MAX ATD INSP--X t6t qpN Y t6t !4r4 Z t7t MAX MIN MAX MIN N4566O3 .161 .178 .046 .07.1 .076 .02q .020 qlq .010 ro71 .083 .341 .425 .039 .045 .184 .244 11B 1 .24r 005 006 0q1 ,0045 .0040 .0030N456604 .046 N4566O6 t97 .070 106 .025 015 125 578 052 368 .364 009 0045 .0025 N4566OB zLo .070 106 .030 020 LO/ 735 .062 .493 4BB 011 006 0020 018 006 0020 NAS66 2 .252 .070 t4 .045 030 250 041 07B 743 737 009 0020 NAS66 o 264 .070 I4 060 045 333 309 r04 993 .986 022 .009 .0020 N4566 8 357 .070 I4 070 .05 5 tBt 458 t04 1.118 1 111 025 009 .0020 NAS662O 389 070 t4 075 .060 tBt 646 t04 I 743 r . 1-to 028 009 .0020 MATERIAL: ALLOY STEEL - 4I4O (UNS G41400) PER MI{-S-596 AMS6349 OR AMS63B2, 4340 (UNS G43406) PER M+{=€-5€e€ AMS6415 OR AMS6484 OR 8740 (UNS G87400) PER M{+-5-6€49 AM56322-. LOCKING ELEI.4ENT - NYLON OR EQUIVALENT PER MIL-DTL.1B24O AND QPL-18240. HEAT TREAT: DEVELOP BASIC MATERIAL PROPERTIES AS FOLLOWS, WITH CONTROLS PER AF45-f+€875-eR AM52759: 160 - 180 KSI Ftu FINISH: CADMIUM PLATED BOLTS _ CADMIUM PLATE PER AMS-QQ.P-416, TYPE II, CLASS 2. EN4BRITTLEMENT REQUIREMENT PER NAS4002. CHROMIUM PLATED BOLTS _ CHROMIUM PTATE PER AMS-QQ-C-320, CLASS 2 ON SHANK ONLY. ALL OTHER SURFACES CADMIUM PLATED. NO CHROMIUIVI WITHIN .O2O OF LINE OF TANGENCY OF HEAD TO SHANK FILLET. CHROMIUM IN THREAD RUNOUT PERMITTED. CHROMIUN4 PLATED BOLTS NOT AVAILABLE WITH GRIP DASH NUMBER 1 OR NUIVIBER 2. CODE: NO FINISH CODE AFTER BASIC NUI'1BER FOR CADIYIUIY PLATED BOLTS. ADD "C" AFTER BASIC NUMBER FOR CHRON4IUM PLATED BOLTS. ADD "D" AFTER BASIC NUN4BER FOR DRILLED SHANK BOLTS. DO NOT USE WITH ''1" OR ''P'' CODE. /13/ ADD ''H'' AFTER BASIC NUN4BER FOR BOLT WITH DRILLED HEAD. ADD ''L'' AFTER BASIC NUMBER FOR SELF-LOCKING BOLT WITH LOCKING ELEMENT TYPE OPTIONAL; SEE PROCUREMENT SPEC BELOW. DO NOT USE ''1" WITH ''D'' OR ''P'' CODE. ADD "P'' AFTER BASIC NUMBER FOR SELF-LOCKING BOLT WITH PATCH TYPE LOCKING ELEMENT ONLY; SEE PROCUREMENT SPEC BELOW. DO NOT USE ''P" WITH ''D'' OR "L'' CODE. cRIp DASH NUMBER INDICATES GRIP IN .0625 INCREMENTS (CONVERTED TO THREE DECIIVIAL PLACES PER ANSI Y14.5-1982). SEE TABLE rr FOR TABULATIONS OF GRIP AND LENGTH DITVTENSIONS. t17 I CODE LETTER "X" AND "Y" FOLLOWING THE GRIP DASH NUIYBER INDICATES REPLACEMENT OVERSIZE REPAIR BOLT. (SEE LAST SHEET) IF MORE THAN ONE CODE LETTER IS USED IN SEOUENCE, ARMNGE THE LETTERS ALPHABETICALLY. @ counr-rrElY REVTsED REVISION I

456603 THRU 66

g o g _- !' ZZ> g-i: L-.r NATIONAL AEROSPACE STANDARD @ COPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED USE OF OR {ELIANaE UPO\\ Tl-1lS DOCUf'1ENT OR ANy NATIONA- AEROSPACE STANDARD IS ENT]RELY VOLUNTARY. AtA DOES NOT eUALIFY SUppLIbn5 OR CERIIFYCONFoR^4ANCEOFITEI4SPRODUCEDUNDER\\ATIONALAEROSPACESTANDARDS. AIAMAKESNOREPRESENTATIONORCLA.TNIRESPECnNG(1)THESUtTABtUTyOF 1IFr45 FOR ANY PAi\\TICUIAR APPdCATIO\\ OR (2) THE EX]STENCF OF OR APPLICABILTIY IHERETO OF PATENI OR IRADEMARKS RTGHTS G -tI a:, u)! Au) az 7ta ff, UY ;.' 6 - =a a o NOTES: EXAMPLE OF PART NUMBER: (SEE LAST SHEET FoR OVERSIZE BOLTS.) NAS66O4-10 = BOLT, ,2500-28 THREAD, .625 GRIP, UNDRILLED, NONLOCKING, CADMIUN4 PLATED. NAS6604D10 = BOLT, .2500-28 THREAD, .625 cRIP, DRILLED SHANK, UNDRILLED HEAD, NONLOCKING, CADIVlIUN4 PLATED. NAS6604H10 = BOLT, .2500-28 THREAD, .625 GRIP, DRILLED HEAD, UNDRILLED SHANK, NONLOCKING, CADMIUM PLATED, NAS6604DH10 = BoLT, .2500-28 THREAD, .625 GRIp, DRILLED SHANK, DRILLED HEAD, NONLOCKING, CADN4IUM PLATED. NAS66O4L1O = BOLT, .2500-28 THREAD, .625 GRIP, UNDRILLED, SELF-LOCKING (LOCKING TYPE OPTIONAL; SEE PROCUREN4ENT SPEC BELOW), CADN4IUM PLATED. NAS6604P10 - BOLT, .2500-28 THREAD, .625 GRIp, UNDRILLED, SELF-LOCKING (pATCH TypE; SEE PROCUREN4ENT SPEC BELOW), CADMIUM PLATFD. NAS6604C10 = BOLT, .2500-28 THREAD, .625 GRIP, UNDRILLED, NONLOCKING, CHRCwTUp'I PLATED. IU GRIP LENGTH: FROM UNDER SIDE OF HEAD TO END OF FULL CYLINDRICAL PORTION OF SHANK. l2l BEARING SURFACE SQUARENESS: WITHIN .003 FII\\4 OF"gD',. I3I ..OC" MAX NOT TO EXCEED ACTUAL WIDTH ACROSS FLATS; MlN AS TABULATED IN TABLE I. I4I "OP" HOLE CENTERLINE WITHIN ,O10 AND NORMAL WITHIN 20 OF BOLT CENTERLINE. I5I REFERENCE DIN4ENSIONS ARE FOR DESIGN PURPOSES ONLY AND ARE NOT AN INSPECTION REQUIREMENT. VALUES FIM. 17l SHANK STRAIGHTNESS: WITHIN "Z" VALUES FIt'4 PER INCH OF LENGTH. lgl ToP oF HEAD SHALL BE FLAT ON THE 1.1250-12 AND 1.2500_12 SrZE BOLTS. I9I PROTRUSION OF LOCKING ELEMENT SHATL BE CONTROLLED SO THAT IT WILL PASS FREELY, OR WITH FINGER PRESSURE, THROUGH A RING GAGE WITH DIAMETER OF .010 (+.001, -.000) GREATER THAN NIAXIMUM MAJOR DIAMETER OF BOLT THREAD. ITOI ''F'' MIN (5 THREAD PITCHES) = REGION OF MINIMUM ENGAGEMENT WITH FEMALE THREAD REQUIRED TC 14EET MIL DTL.1B24O REQUIREMENTS. LOCKING ELEI\\4ENT WITHIN ''F" REGION N4UST DEVELOp REQUTRED TORQUE WHEN TESTED pER tyrL_DTL_18240. IIII FOR EASE IN STARTING, LOCKING ELEMENT SHALL NOT BE EFFECTIVE IN '']'' AREA (3 THREAD PTTCHES). tt+I I13I IF REQUIRED, TENSILE TESTING OF BOLTS REQUIRING CROSS-DRILLED THREADS SHALL BE PERFORI'4ED PRIOR TO DRiLLING AND THE APPLICATION OF PLATING AND/OR COATINGS. WHEN BOLTS HAVE BEEN DRILLED, STRENGTH MAY BE VERIFIED BY SHEAR TESTING, IN LIEU OF TENSILE TESTING, IN ACCORDANCE WITH NASM1312. USERS SHOULD BE AWARE THAT FASTENERS WITH CROSS'DRILLED THREADS MAY EXHIBIT A REDUCTION IN TENSILE STRENGTH. @ couer-r-rELY REVTsED RE'/ISION I THRU 662 SHEET 3

z oo o;)-' I r'- U;Z ;=: *ts Sx OF Zn gU FIzi UY =zg =<U q!o TdL NATIONAL AEROSPACE STANDARD @ coPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVEI) USE OF OR RELIANCE UPON ]HIS DOCUIqENT OR ANY NATIONAL AEROSPACE STANDARD IS ENTIRELY VCLUNTARY AiA DOES NOI Q{TALIFY SUPPLIERS OR CTRTIFV CONFORMANCE OF ITEMS PRODUCED UNDER i\\IATIONALAEROSPACE STANDARDS. AtA MAKES NO REPRESENTAT]ON OR CLAI! RESPECTING (1) IHE SUIIABILJTY OF IIEMS FOR ANY PART]CULAR APPUCAT1ON OR {2) THE EX]STENCE OF OR APPTICAB].]IY THERETO OF PATENT OR TRADEN1ARKS R]GIJTs o II4I LOCKWIRE HOLES SHALL BE DRILLED WITHIN .O1O OF CENTER OF HEX FLAT \\^/HEN SPECIFIED BY PART NUMBER. IfiI HEAD MARKING: BASIC NUMBER PLUS GRIP DASH NUMBER PLUS "D", "1", OR "P", WHEN APPTICABLE, PLUS MANUFACTURER'S SYMBOL, RAISED OR DEPRESSED .O10 MAX. ARRANGEMENT OPTIONAL. *D" IDENTIFIES BOLT WITH DRILLED SHANK. .1" IDENTIFIES BOIT WITH LOCKING ELEMENT (OPTIONAL TYPE). .P" IDENTIFIES BOLT WITH PATCH TYPE LOCKING ELEMENT ONLY' CHROMIUM PLATED CODE "C" NEED NOT APPEAR ON BOLT HEAD. (16) SURFACE TEXTURE: "OD", HEAD-TO-SHANK FILLET, BEARING SURFACE OF HEAD, THREAD FLANKS AND THREAD ROOT: 32 MICROINCHES Ra; ALL OTHER SURFACES: 125 IvIICROINCHES Ra PER ASME 846.1, IITI INTERMEDIATE OR LONGER LENGTHS N4AY BE SPECIFIED BY THE USE OF WHOLE GRIP DASH NUIYBERS ONLY. NON4INAL LENGTH EQUALS NOI\\4INAL GRIP PLUS "T". (18) DIMENSIONS TO BE MEI AFTER PLATING. (19) DIMENSIONS IN INCHES. (20) REMOVE ALL BURRS AND SHARP EDGES. (21) THIS STANDARD TAKES PRECEDENCE OVER DOCUMENTS REFERENCED HEREIN, (22) REFERENCED DOCUMENTS SHALL BE THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BID. (23) UNLESS OTHERWISE SPECIFIED, PART INVENTORY MANUFACTURFD TO PREVIOUS REVISIONS OF THE APPLICABLE DRAWING OR SPECIFICATION MAY BE PROCURED AND USED UNTIL STOCK IS DEPLETED. PROCUREMENT SPECIFICATION: NAS4OO2, EXCEPT AS NOTED. COLD WORK OF HEAD TO SHANK FILLET RADIUS AND FATIGUE TESTING ARE NOT REQUIRED FOR NAS66O3 BOLTS. LOCKING ELEN4ENT FOR SELF LOCKING BOLTS: PER NASMi59B1 AND MIL-DTL-18240, LOCKING ELEMENT ryPE, INCLUDING PATCH ryPE, IS OPTIONAL WHEN ''L'' CODE IS SPECIFIED. PATCH ryPE LOCKING ELEMENT (\\^iTTH NO METAL REI4OVED) IS REQUIRED WHEN ''P'' CODE IS SPECIFIED. LOCKING ELEMENT MUST BE SUPPTIED BY A QUALTFIED SOURCE LISTED IN QPL-18240 OR APPROVED FOR LISTING IN QPL-18240. SHIPPING NOTICE SHOULD IDENTIFY SUPPLIER OF BOLT AND LOCKING ELEMENT SEPARATELY. @ coruer-r-rElY REVISED

#{4 NATIONAL AEROSPACE STANDARD O COPYRIGHT 2OO9 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. ALL RIGHTS RESERVED c o c -I< a-- <=; or oF tl ;<. o IJSE OF OR RELIANCE UPON THIS DOCUMENT OR ANY NATIONAL AEROSPACE SIANDARD IS ENIIRELY VOLUNTARY. AIA DOES NOT QUALIFY SUPPLITRS OR CERIIFY :_".1:::jji:::ijliT:i:q?Y:r-?:y.?r1l1lt9f1l_1.!19:l1c!srtNDAR?: ArAMAKESNoREpREsENrArroNoRcLArN4REspEcnNG(1)rHEsurrABruryoF GRIP i DASH NO.) GRIP i LENGTH +i.015 /17lI.UIU I BASIC NUMBER AND THREAD SIZE i runsooo: | runsooo< I runsooos ] rua-ooo{rrrasoooz I .1900-32 | .2500_28 I .:tzs 24 | 3750_24 .4375_20 trrnsooq rrrn-sooog .5000-20 i .5625-18 iit; .062 . tlJ .1BB .250 407 470 533 595 .487 .5 50 .ot-J .675 )Jl 594 657 719 ,640 .703 .766 .B2B .756 .819 .BB2 .944 797 860 923 985 .902 .965 1.028 r.090 B .312 .375 .438 .500 .657 .720 .783 .845 737 800 B63 925 787 844 907 969 .890 .953 1.016 1.078 1.006 1.069 I.I32 1.r94 047 110 I/J 235 r.t52 I.215 1.278 1.340 le l1? )12 .562 .625 .68B .750 .907 .970 1.033 1.095 .987 1.050 I.Il.J t.175 1.031 1.094 |.157 |.219 r.140 r.203 1,.266 1.328 t.zlo 1.319 1.382 I.444 297 360 423 485 r.402 I.465 1.528 1.590 .tJ 1t) .6t 2 .875 .938 1.000 I.I57 L220 1.283 1.345 1.237 1.300 1.363 r.425 1.281 l. Jaa r.407 7.469 1.390 1.453 l.)1t) I .578 1.506 1.569 r.632 t.694 .547 .610 .673 .735 r.652 I./ I) 1.778 1.840I7 I.UOI I.t25 1.188 1.250 7.407 1.470 1.533 1.595 I.487 1.550 I.DlJ r.675 1.531 1.594 L,O) / |.7 1,9 1.640 |.703 L766 1.828 r./fo 1.819 1.882 7.944 797 860 923 985 1.902 1.965 2.028 2.090 )21 I22i )23 1 )Al r.312 1.375 1.438 1.500 r.657 7.720 1.783 1.845 1.737 1.800 1.863 1.925 I.7BI 7.844 1.907 1.969 1.890 1.953 2.016 2.078 2.006 2.069 2.1,32 2.t94 2.A47 2.I70 2.173 2.235 2.152 2.2r5 2.278 2.340 r.562 1.625 1.688 1 .750 r.907 |.970 2.033 2.09 5 1.987 2.050 2.113 2.175 2.031 2.094 2.157 2.2r9 2.r40 2.203 2.266 2.328 2.256 2.319 7.382 2.444 2.297 2.360 1.<+ 1J 2.485 2.402 2.465 2.528 2.590 1.812 1.875 1.938 2.000 2.157 2.220 2.283 2.345 2.237 2.300 2.363 2.425 2.281 2.344 2.407 2.469 2.390 2.453 2.516 2.578 2.s06 2.569 2.632 2.694 2.547 2.610 2.673 2.735 2.652 Z./ IJ 2.778 2.840 2.r25 2.250 2.375 2.500 2.470 2.595 2.720 2.845 2.550 2.675 2.800 2.925 2.594 2.719 2.844 2.969 2.703 2.828 2.953 3.078 2.819 2.944 3.069 3.r94 2.B60 2.985 3.1 10 3.235 2.965 3.090 3.215 3.340 z.oz) 2.750 2.875 3.000 2.970 3.095 3.220 3.345 3.050 3.175 3.300 J ..+ 15 3.094 3.219 3.344 3.469 3.203 3.328 3.453 3.578 3.319 3.444 3.569 3.694 3.360 3.485 3.610 3.735 3.465 3.590 )./ r) 3.840 3.125 3.250 3.375 3.500 3.470 3.595 3.720 3.845 3.550 J.O/f 3.800 3.925 3.594 3.7r9 3.844 3.969 3.703 3.828 3.953 4.078 3.819 3.944 4.069 4.194 3.860 3.985 4.1 10 4.235 3.965 4.090 4.215 4.340 3.625 3.750 3.875 4.000 3.970 4.095 4.220 4.345 4.050 4.175 4.300 4.425 4.094 4.219 4.344 4.469 4.203 4.328 4.453 4.578 4.319 4.444 4.569 4.694 4.360 4.485 4.610 4.735 4.465 4.590 4.7 15 4.840 TABLE II - GRIP AND LENGTH DIMENSIONS (CONTINUED ON NEXT PAGE) lal )4. i4( )4t fv is,ls(t- sr @ covrer-rrELY REVTsED REVISION I THRU 66 SHEET 5 LENGTH +1,.0r5 l17l ITEMS FOR A:{Y PARI]CUL-AR APPUCAT]ON OR (2) THE EXISTENCE OF OR APPLICAB]LIIY THERETO OF PATENT OR IRADEN1ARKS RIGHTS

a c z g o -Ad -- - Z 2>-.)-- *to7;Z az OF Z-r tJ oE ==x IdL NATIONAL AEROSPACE STANDARD o coPYRIGHT 2OO9 AEROSPACE INOUSTRIES ASSOCIATTON OF AMERICA, INC. ALL RIGHTS RESERVED USE OF OR RELIANCE UPON IHIS DOCUMENT OR ANY NATIONAL AEROSPACE STANDARD IS E^ITIRELY VOLUNTARY. AIA DOES NOI'QUALIFY SUPPLJERS OR CERTIFY CONFORN1ANCEOF1TEI4SPRODUCEDUNDERNATIONALAEROSPACESTANDARDS. AIAMAKESNOREPRESENTAT]ONORCLA1MRESPECTING(1)THESUITABILITYOF ITEMS FOR ANY PART]CULAR APPLICAT]ON OR (2) IHF EX]STENCE OF OR APPLICABILITY THERETO OF PATENT OR TRADFMARKS RIG}1T5 E o TABLE II - GRIP AND LENGTH DIMENSIONS (CONTINUED) @ cover-rrELY REVISED REVISION NA56603 THRU SHEET 6 GRIP DASH NO. tr Kl l- r.010 LENGTH +/-.01s /17l BASIC NUMBER AND THREAD SIZE I25I N45661O .6250-18 NA56612 .7500-16 N456614 .8750- 14 N456616 1.0000- 1 2 NAS661B 1.1250-12 NAS662O 1.2500 12 a .062 .t25 .1BB .250 .964 r.027 1.090 r.r52 1.103 _1. 100 L229 r.29t t.246 1.309 r.372 r.434 |.371 t.434 r.497 1.559 520 sB3 646 708 1 708 I ,771 1.834 1.896 I 3t2 375 438 500 L274 1,.277 1.340 r.402 1.353 r.'i r o 1.479 1.541 7.496 1.559 t.622 1.684 t.62r 1.684 1.747 1.809 .770 .833 .896 .958 1.958 2.02r

2 AB4

2.146 562 625 6BB 750 |.464 r.527 1.590 r.652 1.603 1.666 1,.729 t.791, 1.746 1.809 7.872 1.934 1.871 7.934 1.997 2.059 2.020 2.083 2.t46 2.208 2.208 2.27r 2.334 2.396 IO .Bt2 .875 .938 1.000 L.7 14 r.777 1.840 t.902 1.853 1.916 1..979 2.041 1.996 2.059 2.1,22 2.184 2.t27 2.184 2.247 2.309 2.270 2.333 2.396 2.458 2.458 2.52r 2.584 2.646 r.062 1.T25 I.1BB L.lJU t.964 2.027 2.090 2.t52 2.r03 2.L66 2.229 2.297 2.246 2.309 2.372 2.434 2.37r 2.434 2.497 2.559 2.520 2.583 2.646 2.708 2.708 2.777 2.834 2.896 z.+ 1.3r2 r.375 1.438 1.500 2.2r4 2.277 2.340 2.402 1.5)J 2.416 2.479 2.54r 2.496 2.559 2.622 2.684 t.ozr 2.684 2.747 2.809 2.770 2.833 2.896 2.958 2.958 3.021 3.084 3.\\46 t.562 L,OZ3 1.688 1.750 2.464 2.527 2.590 2.652 2.603 2.666 2.729 2.791 2.746 2.809 2.872 2.934 2,871 2.934 2.997 3.059 3.020 3.083 3.146 3.208 3.208 3.27r 3.334 3.396 1.812 1.875 r.938 2.000 2.774 2.777 2.840 2.902 2.853 1.9 LO 2.979 3.041 2.996 3.059 3.122 3.184 3.12r 3.184 3.247 3.309 3.270 3.333 3.396 3.458 3.458 3.521 3.584 3.646 J.-l 2.125 2.250 2.375 2.500 3.027 3.t52 3.277 3.402 3.166 3.29r 3.416 3.54r 3.309 3.434 3.5 59 3.684 3.434 3.559 3.684 3.809 3.583 3.708 3.833 3.958 3.771 3.896 4.O2r 4.146 .tz 2.625 2.750 2.875 3.000 3.527 3.652 3.777 3.902 3.666 3.79r 3.916 4.041 3.809 3.934 4.059 4.t84 3.934 4.059 4.r84 4.309 4.083 4.208 4.333 4.458 4.27r 4.396 4.52r 4.646 qn 3.125 3.250 3.375 3.500 4.027 4.r52 4.277 4.402 .t.100 4.29r 4.416 4.541 4.309 4.434 4.559 4.684 4.434 4.559 4.684 4.809 4.583 4.708 4.833 4.958 4.77 7 4.896 5.021 5.146 3.625 3.750 3.875 4.000 4.527 4"652 4.777 4.902 4.666 4.791 4.916 5.041 4.809 4.934 5.059 5.184 4.934 5.059 5.184 5.309 5.083 5.208 5.333 5.458 5.277 5.396 5.521 5.646