DLA AN160701 THRU AN161000 REV 3-1987 STUD STEPPED DRILLED NECKED 1 5 DIA ENGAGEMENT 5625-12 X 500-20.pdf

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1、_I _I_-.-. ANLb0701 THRU ANlbL000 REV 3 CANC e1L5 0003LA7 707 FSC 530 I .350 - .WO OVERSIZE IDENTIFICATION STAMP PER AUS 2800 .O10 MAX DEPTH SEE TABLE FOR PD HOLE ON AXIS OF THD WITHIN .O05 ?fDE.SSIZE AND I -.O03 I STANDARD OVERSIZE IDENTIFICA TI ON - U C .557- .%i: ,557- ,562 PD BEFORE PLATINQ .510

2、4-.511- .2134-.5144 PD AFTER PLATINO. .5139-.5124 .135-.5154 PD LEAD THREAD .SO34 -, 5054 .5!%l-. 5084 L PART HUMBER PART NUMBER _ _-_I 4 Nl50714 .4 N153720 AN160726 A Hl50732 b.Nl07 8 AN160724 P Nl60750 AN160756 .hN160752 1NiO768 4 160774 .?N160780 A ti160786 4 Ni6079 1 A ti16 0792 3.210 ANI60803 A

3、N1608014 AAIOW n ti150798 3.3114 3.3!9 3. cZ$l 3.719 3.8$4 $:o,? 4 : 28 fl:3 4.719 A 160810 AN160828 AN160858 A N16 0864 AN160870 AN160876 ._ y AN160881 AN150882 495g AN160887 AN160888 5 094 AN160893 AN160894 AN160899 AN160900 :;i? AN160905 AN150906 5.45s AN150911 AN160912 5.j9i AN160917 AN160918 4

4、.a44 NOTE: PITCH DIAHETERS OF BOTH THREADED Was t.003 ,557- .562 .5164-.51 4 5169-. 5144 RN160715 RN15 072 1 4 Ni6 0727 AN160733 IN1607 9 AN160725 hN150751 AN160757 4N160763 4N 16 076 9 kN160787 4N160793 4 Ni60799 4N160805 411608.11 21160817 E%: l Ni6 082 3 iN160829 “1608 5 iN160821 Ni60847 !Ni60853

5、 Ni0853 1N160855 lN160871 Ni60877 IN160883 Ni60889 iN160895 iN160901 iN160907 iN160913 Ni60919 MLL BE CONC +.o06 t ,009 t .o12 AN160794 AN160795 AN1607% AN160800 AN160801 AN160802 AN160806 AN160807 AN160808 AN160812 AN160813 AN160814 AN160818 AN169819 AH160820 AH160824 AN160825 AN160826 AN160830 AN1

6、60831 AN360832 AN1608 7 AN1608 8 E% AN16Od3 AN160824 AN160850 AN160848 AN1608119 AN160854 ANld0860 AH160865 AN160872 AN360878 AN160884 AN160890 AN160896 AN160902 AN160908 AN160914 AN160920 AN160915 AN160921 16085 160862 AN160868 AN160886 AN169892 AN160898 AN160904 - O910 AN160936 AN160922 TRIC WITHI

7、N .o06 FIR. MATERIAL: srrrt US 63ia (AHS 6320 MTERIAL AY ALSO BE USED FOR THIS PART VUIITIL JANUARY i, iy57)! FINISH: CADP(1UII PLATE AWS 2400. DI#WSIONS ARE AFTER PLATINO i3CEPT WHERE SHOW. SURFACE ROUQHNESS: AS 107. MANIIFACTURINQ SPECIFICATION: AMS 7456. PARTS SWJECT TO HAONETIC INSPECTION PER AM

8、 2640. DIMENSIONS IN INCHES. p3SS OTAERWISB SPECIFIED: TOLERANCES; LINEAR DIIIBNSIONS I.010, HARDNESS: ROCKWELL C26-32. BREAK SHARP EWES .003-.015 UNLESS OTHERWISE SPECIFIED. ANQULAR DIHENSIONS i2 . 0 INACTIVE FOR DESIGN AFT R 26 OCTOBER 1972. NO SUPERSEDING STANDARD. Do NOT USE UNASSIQNED PART “BEA

9、S. 6 CANCELED AS OF 9 OCT 87 THIS STANDARD WAS DEVELOPED COOPEJUTNELY WITH THE ENOIXB AND PROPEUR UTILITY PARTS COIII(I“RE OF THi3 SAE. AN I 6 0 7 0 I CLCIFICATION PfWCUIILMLHT AIR FORCE-NAW AERONAUTICAL STANDARD THRU .6TUDrSTEPPED, DRILLFD NECKED, 1.5 DIA EWAOmNT, AN16 I O O0 IONE .56p6-12 x ,500-20 I I E-25-121 Project 5307-0399 - I - -_ql- #- y Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-