MS20001 - Genuine Aircraft

MS20001 Hinge / Butt / Structural / Extruded

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 UNIVERSALL.

Features

nd 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 HINGES SHALL BE FINISHED). INK STAMP MS20001 (DASH NUMBER) REGULAR INTERVALS ALONG LENGTH OF HINGE SO.