1、AN127125 THRU AN327178 REV 3 53 W 7777935 O000351 2 / FE SUP CLASS. 5307 MIN FULL THD IN FULL THD CHAMFER .O62x45O SECTION THRU THREAD PROFILE BOTH THD SIZES STAIIP WE AllS200 .O10 HAX DEPlYi UNDERSIZE AND OVERSIZE IDENTIFICATION STAMP PER AM32800 .O10 MAX DEPTH UNDERSIZE AND OVERSIZE IDENTIFICATIOW
2、 PD BE PD AF PD LE L 1.930 2. i80 - RB PLATING R PU - THi A - L.OO.( 1.25 - .O03 I NG L B - - 75c .75c .495 -.500 .458-.4520 .4523-.4538 .4450-.4470 PART NMBER AN129137 AN129143 STANDARD . 0 .495 -.500 .4548-.4558 .4553-.4560 .4480-.4500 PART NUMBER AN129138 AN129144 +*O03 + .O06 + . O09 -495 -.500
3、-495 -.500 -504 -e509 .4578-.4588 .4600-.4610 .4630-.4648 .4503-.4598 .4613-.4628 .4643-.4650 .4510-.4530 .4540-.4560 .4570-.4590 PART NUMBER PART MIMBER PART NUMBER AN129139 AN129145 .4 AN129140 I AN129146 AN129141 I AN 129 14 7 +.o12 .SO4 -.509 .4660-.4670 -4600-.4620 ART NUMBER .4673-,46aa AN1291
4、42 AA129140 NOTE: PITCH DIAHETERS OF BOTH THREADED ENDS SHALL BE CONCENTRIC WITHIN .O06 FIR. (a) CROSS THREADING PERHISSABLE AT THREAD RUNOUTS ON SHORT STUDS. HATERIAL: STEEL AHS 6322 (AHS 6320 HATERIAL HAY ALSO BE USED FOR THESE PARTS UNTIL i JAN 1960) HARDNESS: ROCKWELL C26-32. FINISH: CADHIUH PLA
5、TE AHS 2400. DIHENSIONS ARE AFTER PLATING EXCEPT WHERE SHOWN. SURFACE ROUGHNESS: AS291 HANUFACTURING SPECIFICATION AMS 7456. BREAK SHARP EDGES .003-.O15 UNLESS OTHERWISE SPECIFIED. DIHENSIONS IN INCHES. UNLESS OTHERWISE SPECIFIED: OLERANCES; LINEAR DIHENSIONS t.010. DO NOT USE UNASSIGNED PART NUMBER
6、S. THIS STANDARD WAS DEVELOPED COOPERATIVELY WITH THE ENGINE AND PROPELLER UTILITY PARTS COHHITTEE OF THE SAE. )INSPECTION : ALL PARTS SHALL UNDERGO MAGNETIC INSPECTJON IN ACCORDANCE WITH AHS2640. 1 PA 11 CUST AV AS 11 AIR FORCE-NAVY AERONAUTICAL STANDARD STUD - STRAIGHT, DRILLED, .500-13 x .500-20 AN I29 I25 THRU AN 129178 II I I Project No. 5307-0358 PAGES* *U.s. GOVERNMENT PRINTING OFFICE: 1986 - 605-036/43906 .* Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
