MS20001

Genuine Aircraft Hardware Co. Hinge, Butt, Structural, Extruded MS20001 TABLE I * CANCELLED - NO SUPERSEDING PART NUMBER ( a ) TOLERANCES FOR DIMENSIONS ON PITCH SHALL NOT BE CUMULATIVE. ( b ) DIMENSIONS K MUST NEVER EXCEED A FULL LOOP OR TANG, AND BOTH ENDS MUST BE EQUAL WITHIN .020 INCH. INTERCHANGEABILITY RELATIONSHIP: MS20001 HINGES ARE NOT UNIVERSALLY INTERCHANGEABLE WITH AN252 HINGES. FOR INTERCHANGEABILITY RELATIONSHIP SEE TABLE II. PROCUREMENT SPECIFICATION: NONE SUPERSEDES: AN252 THIS INFORMATION FROM MILITARY STANDARD MS20001L PAGE 1 OF 1, REVISED OCTOBER 30, 1989, SOME DETAILS MAY HAVE BEEN OMITTED FOR CLARITY. TABLE I I INTERCHANGEABILITY TABLE INACTIVE AND CANCELLED AN252-1 AN252-2 AN252-4 AN252-6 AN252-8 AN252-10 UNIVERSALLY INTERCHANGEABLE ------------------MS20001-2 MS20001-4 MS20001-6 MS20001-8 MS20001-10 REPLACEABLE -----------------------------------------------------------------------------------------------------------WITH 154 All Original Text, Tables and Drawings are Copyright © by Genuine Aircraft Hardware Co. 2005 Documents in this book for REFERENCE ONLY, not intended for design. Not guaranteed for accuracy. Continued... Genuine Aircraft Hardware Co. Continued... REQUIREMENTS: 1. MATERIAL: 2. FINISH: 3. MARKING: ALUMINUM ALLOY 2024-T3511, PER QQ-A-200/3, OR ALUMINUM ALLOY 7075-T3511, PER QQ-A-200/11 (SEE PART NUMBERING). ANODIZED IN ACCORDANCE WITH MIL-A-8625, TYPE II; CHEMICAL SURFACE TREAT IN ACCORDANCE WITH MIL-C-5541; (ENDS OF ALL H...