1、- 1 AN10360L THRU AN103700 REV 3 53 m 7747415 000024b 5 W 3-17- 19 - PART NO. AN103617 AN103619 103618 103620 103621 AN103622 AN10362 AN103622 AN103625 AN103626 AN103627 AN103629 103628 103630 B L 3 * 375 3.625 3.5 3.750 .875 2.000 4.125 4.250 4.375 4.500 4.625 4.675 4.750 5.000 K TO FULL THD .O16 O
2、R CHAW -_- SPEC MIL-S-7742 DIA BOTH ENDS - L I +.o00 -.o60 SECTION T“ THREAD PROF PART NO. AN103606 AN103607 mi03608 mi03609 103610 mi03611 mi03612 AN10361 AN103612 AN103615 AN103616 L 2.188 2.250 2.312 2.375 2.438 2.500 2.562 2.625 2.688 . 2.750 2.875 3.000 3.125 3.250 K +.O00 - . O60 .438 .500 .56
3、2 .625 .688 -750 .E12 .875 .938 1 .o00 1.125 1.250 1.375 1.500 2.000 2.062 2.125 THIS SURPACE MIST BE SQUARE WITH SHANK WITHIN 003 FIR. ,250 .375 .312 LCHAMFER 30 TO 1.062 DIA (OPPOSITE SIDE OPTIONAL) P :iJ$T. NAVY-As ARMY - AV ANI0 3700 BOLT - DRILLED HEX EAD, 1 HOLE, -750-16 K + * ooc 1.625 - 1.75
4、0 1.875 2.000 2.125 2.250 2.375 2.500 2.750 2.875 3.000 3.125 3.250 2.625 - *NI03631 5.125 AN103632 I/ 5.250 mi03633 5.375 AN103634 5.500 AN103635 11 5.625 u103636 5.750 K +.OW - .o60 3.375 3.500 3.625 3 -750 3.875 4.000 4.125 4.250 PART NO. AN 10364 5 AN103646 AN103648 AN103650 103647 103649 mi0365
5、1 AN103652 _. (a) THREAD TO HEAD. UAXIUUU TWO IUPERFECT THREADS. I NOTE: (I) SHANK SHALL BE STRAIGHT WITHIN ,002 FIR PEP INCH OF BOLT LENGTH. (2) THE CONCENTRICITY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN ,006 FIR. (3) THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER PACE DIAUET
6、BR AND HXXACON SHALL BE WITHIN .O32 FIR. MTERIAL: STEEL AUS6322 HARDNESZ: POUGHNESS C26 32 FINISH: CADUIUU PLATE AUS2400 SUPPACE ROUGHNESS: AS107 MANUFACTUPING SPECIFICATION: AUS7452 INSPECTION: ALL PARTS SHALL UNDERGO UAGNETIC INSPECTION IN ACCORDANCE WITH AUS2640 BREAK SHARP EDGES .O03 - .O15 UNLE
7、SS OTHERWISE SPECIFIED. DIUENSIONC IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERENCES; LINEAR DIUENSIONS t .OIO, ANGULAR DIIIENSIONS t2. DO NOT USE UNASSIGNED PART NUMBERS. INACTIVE FOR NEW DESIGN AFTER 3 MARCH i969 No SUPEASEDINO STANDARD. THIS STANDARD WAS DEVELOPED COOPERATIVELY BY THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. I AIR FORCE-NAVY AERONAUTICAL STANDARD I AN103601 Project No. 5306-1021 THIS DOCUMENT CONTAINS PAGES. -. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
