DLA AN105301 THRU AN105400 REV 3-1986 BOLT - CRES HEX HEAD 625-18.pdf

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1、r AN105301 THRU AN105400 REV 3 53 W 7999915 0000263 5 W I FED. : 4.125 4.250 4.500 4.625 4.375 4.750 4.875 5.000 5.125 +. O00 -. 060 2.500 AN105331 2.625 AN105332 2 750 AN105333 2. a75 AN105334 3.000 AN105335 3.125 AN105336 3 * 250 AN105337 3.375 AN105338 3.500 AR105339 3.625 105340 3.750 AN105341 3

2、.875 AN105342 4 e O00 AN105343 4.125 AN105344 6.000 I 5.000 I AN105351 1 (1) SHANK SHALL BE STRAIGHT WITHIN .O02 FIR. PER INCH OF BOLT LENGTH. (2) THE CONCENTRICLTY OF THREAD PD IN RELATION TO THE SHANK SHALL BE WITHIN .O06 FIR. (3) THE CONCENTRICITY OF THE SHANK IN RELATION TO THE WASHER FACE DIAHE

3、TER AND HEXAGON SHALL BE WITHIN .O28 FIR. INACTIVE FOR DESIGN AFTER 27 DEC 1966 NO SUPERSEDING STANDARD. HATERIAL: CORROSION RESISTANT STEEL - SEE MANUFACTURING SPECIFICATION SURFACE ROUGHNESS: AS107 MANUFACTURING SPECIFICATION: AUS 7472 BREAK SHARP EDGES .003-.O15 UNLESS OTHERWISE SPECIFIED. DIHENS

4、IONS IN INCHES. UNLESS OTHERWISE SPECIFIED: TOLERANCES; LINEAR DIMENSIONS t.010, ANGULAR DO NOT USE UNASSIGNED PART NUMBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILLTY PARTS COHMITTEE OF THE CAE. P.A. Other Cusc 1 INSPECTION: ALL PARTS SHALL UNDERCO FLUORESCENT P

5、ENETRANT INSPECTION IN ACCORDANCE WITH AMS2645. DIMENSIONS t2. AIR FORCE-NAVY AERONAUTICAL STANDARD AN I 0530 I USAF - II Navy - AS Army - AV AN I 88400 BOLT - CRES HEX HEAD .625-18 .u1 VI“.IxIeiT PpIITI*cLIIIIcL IWl-Ill-IIYII, Project No. 5306-1037 /- . THIS DOCUMENT CONTAINS PAGES. 1 -1 Licensed by Information Handling Services