DLA AN129065 THRU AN129124 REV 3-1986 STUD-STRAIGHT DRILLED 4375-14 X 4375-20.pdf

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1、AN127065 THRU AN127124 REV 3 53 M 7777735 0000350 O M _a-oi-/q - -. -. FED. SUP CLASS. 5307 UNDERSIZE AND OVERSIZE DENT I P I CATION D BEI D AP L - .688 .815 .938 RE PLATING R PLATING THREAD A B .a75 .62 1.156 .62 1.094 .62! - .o03 AN129071 AN129089 129083 STANDARD .473 -.438 .3951-.3967 .3962-.3977

2、 .891-.3911 PART NJMBER mi29018 AN129084 AN129090 +.O03 AN129079 AN129085 AN129091 + .o06 AN129080 AN129092 129086 +.o09 I +O12 AN129081 AN129087 AN129093 .442 -.447 .4077-.4081 .4082-.4091 .4011- .4031 PART AMER AA129082 AN129388 AA129094 INACTIVE FOR DESIGN AFTER 26 OCTOBER 1972. NO SUPERSEDING ST

3、ANDAW: NOTE: PITCH DIAMETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN .O06 FIR, (a) CROSS THREADING PERHISSABLE AT THREAD RUNOUTS ON SHORT STUDS. MATERIAL: STEEL AUS 6322 HARDNESS: ROCKWELL C26-32. FINISH: SURFACE ROUGHNESS: AS291 KANUFACTURING SPECIFICATION AH9 7456. BREAK SHARP EDGES .003-

4、.015 UNLESS OTHERWISE SPECIFIED. DIHENSIONS IN INCHES. UNLESS OTHERWISE SPEC1FLED:TOLERANCES; LINEAR DIHENSIONS f.010,ANGULAR DIMENSIONS ?5. DO NOZ USE UNASSIGNED PART NUMBERS. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COMMITTEE OF THE SAE. (AHS 6320 MATER

5、IAL HAY ALSO BEUSED FOR THESE PARTS UNTIL I JAN.1960) CADHIUH PLATE AIIS 2400. DIHENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. QINSPECTION: ALL PARTS SHALL UNDERGO HAGNETIC INSPECTION IN ACCORDANCE WITH AHS2640. AIR FORCE-NAVY AERONAUTICAL STANDARD AN I29065 THRU STUD - STRAIGHT, DRILLED, .4375-14 X .4375-20 y, AN129124 PA 11 CUST: AV, AS 11 *U.S. GOVERNMENT PRINTING OFFICE: 1988 - 806-036/43406 is km 4 d . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-