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2、o, 15406 105408 AN105407 AA105409 AN105410 AN105411 AN105412 ANlU5413 ni054i4 AN10915 AN105416 -750-16 UNF-SA SPEC UIL-S-7742 LTHIS SIIRFAOE WUST RE SQUARE HITH SHANK Y!“IN .O03 FULL DICAT(R umma cmnm 300 TOLWDYL (OPPOSITE SIDE OPTIONAL) L K +.o00 -.O60 1.938 -812 2.000 .875 2.125 1.000 2.250 1.125
3、2.500 1.375 -I 2.375 1.250 2.625 1.500 1.625 1.750 3.000 1.m5 3.l25 2.000 3.250 2.l.25 3.375 P-P50 3.500 P-375 - L 5.375 4.250 AHlOYt4! 5.500 4.375 AlO9hi 5.625 II 4.500 AN10544; (1) SHANK SHALL BE STRAICHT WITHIN ,002 Flu. PER INCH OF BOLT LEWCIH. (2) THE CONCENTIICITY OF THREAD PD IN RELAIION TO T
4、HE SHANK SHALL E WITUIN .O06 FIR. (3) THE CONCENTRICITY OF THE SHANK IN RELATIOH i0 THE WASHER FACE DlAHETEP AH0 HEXAGON SHALL BE YITBIY .O32 FIR. INACTIVE FOR DESIGN AFTER 27 DEC I966 NO SUPERSEDING STANDARD. HATERIAL: CORROSION FiBSISTANT STEEL - SEE HAEUFACTURINC SPECIFICATION SULFACL IWUCHHESS:
5、ASIOI IiANFACTUklHC PECIFICATlOh: AH5 lrl? 1hSPECTIOH. ALL PARTS ShALL UNDERGO FLUORESiChI PENETHAN INSPLCTIOH LH ACCORDANCE b1TH AH52645 BREAK SHARP EDGES .001-.015 UNLESS OTHERWISE SPECIFIED. DIHENSIONS IH INCHES. LhLLSS OTHERWISE SPECIFIED: TOLERANCES; LIHEAR DIHCNSIOHS 1.010, AHCULAR Cc0 NOT U5L
6、 IINASSICPILD PAKT HHBLRI. THIS STAIIDARD YAS DEVELOPED LOOPERATIVELY WITH THE ENGINE ANO PROPELLER UTILITY PARTS COHHlTTEE OF THE SAL. P.A ufher Curt DIHENSIOHC 12. AIR FORCE-NAVY AERONAUTICAL SANDARD AN i 95 40 I kSAF - II hauv - AS BOLT - CRES HEX HEAD .750-15 ,Army - AV AN I &SOO cnjecl Nin. 5“h-l IF Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-