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MS20001

Genuine Aircraft
Part Number MS20001
Manufacturer Genuine Aircraft
Description Hinge / Butt / Structural / Extruded
Published Nov 6, 2014
Detailed Description Genuine Aircraft Hardware Co. Hinge, Butt, Structural, Extruded MS20001 TABLE I * CANCELLED - NO SUPERSEDING PART NUM...
Datasheet PDF File MS20001 PDF File

MS20001
MS20001

Overview
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.
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Genuine Aircraft Hardware Co.
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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 THAT ANY THREE INCH LENGTH WILL HAVE AT LEAST ONE COMPLETE IDENTIFICATION IN FIGURES NOT LESS THAN .
060 INCHES HIGH.
SEE NOTE 5.
Hinge, Butt, Structural, Extruded MS20001 4.
COMPLETE HINGES SHALL BE FURNISHED AS AN ASSEMBLY WITH CAD PLATED CRES HINGE PINS OF THE SAME LENGTH IN ACCORDANCE WITH MS20253.
UNLESS TITANIUM HINGE PINS IN ACCORDANCE WITH MS20253 ARE SPECIFIED (SEE PART NUMBERING).
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