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MS27039

Genuine Aircraft Hardware

Pan Head / Structural Screws / Phillips Drive

Genuine Aircraft Hardware Co. Pan Head, Structural Screws, Phillips Drive MS27039 Series ORDER BY MS27039 NUMBERS Las...


Genuine Aircraft Hardware

MS27039

File Download Download MS27039 Datasheet


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Genuine Aircraft Hardware Co. Pan Head, Structural Screws, Phillips Drive MS27039 Series ORDER BY MS27039 NUMBERS Last two numbers ( xx ) are the same for both. Old NAS Part # NAS220 - ( xx ) NAS221 - ( xx ) NAS222 - ( xx ) MS27039 - 08 ( xx ) MS27039 - 1- ( xx ) MS27039 - 4- ( xx ) New MS Part # TENSILE STRENGTH, 125,000 PSI. (Minimum), Head Marking ( - ) for Alloy steel, ( C ) for Corrosion resistant steel “A286” MS27039 - (SIZE) = ALLOY STEEL PARTS ARE PLATED, CADMIUM II (GOLD IN APPEARANCE) MS27039C (SIZE) = CORROSION RESISTANT STEEL, PARTS ARE UNPLATED Supersedes NAS220 - NAS222 SEE THE CHART Example of Part Numbers: MS27039 - 0809 = 8-32 Threads, .594 Overall length under the head, .094 grip length. Alloy steel, Cadmium II plating MS27039C0809 = 8-32 Threads, .594 Overall length under the head, .094 grip length. Corrosion and heat resistant steel (A286) The tolerance for Overall Length is plus .032, minus .015 The tolerance for Grip Length is + or - .015 34 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. Free Datasheet http://www.datasheet4u.com/ ...




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