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SAE Industry Technologies Consortia - AS7473-4

AS7473-7493 B.S.1 Chain (8mm Pitch) and Fittings Assembly Code

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Organization: SAE Industry Technologies Consortia
Publication Date: 13 January 1969
Status: active
description:

No scope available.

Document History

AS7473-4
January 13, 1969
AS7473-7493 B.S.1 Chain (8mm Pitch) and Fittings Assembly Code
No scope available.

References

This document references:
AS7473 - BOLTS AND SCREWS Roll Threaded
Published by SAE International on February 1, 1991
This procurement specification covers aircraft quality bolts and screws made from carbon steels, high expansion steels, or corrosion and heat resistant steels of the type identified under the Unified...
This document references:
AS7474 - BOLTS AND SCREWS, STEEL, CORROSION RESISTANT 140 000 psi Tensile Strength Forged Head, Heat Treated, Roll Threaded
Published by SAE International on May 1, 1995
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant martensitic iron base alloy of the type identified under the Unified Numbering System...
This document references:
AS7475 - BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded After Aging
Published by SAE International on January 17, 1991
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the...
This document references:
AS7477 - BOLTS AND SCREWS, STEEL, CORROSION AND HEAT RESISTANT Upset Headed, Heat Treated, Roll Threaded 1800°F Solution and Precipitation Heat Treated
Published by SAE International on December 5, 1990
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant precipitation hardenable iron base alloy of the type identified under the Unified...
This document references:
AS7478 - BOLTS AND SCREWS, STEEL, CORROSION AND HEAT RESISTANT 1800°F Solution Heat Treated Precipitation Heat Treated After Roll Threaded
Published by SAE International on July 1, 1991
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering...
This document references:
AS7479 - BOLTS AND SCREWS, STEEL, CORROSION AND HEAT RESISTANT 1650°F SOLUTION HEAT TREATED PRECIPITATION HEAT TREATED BEFORE ROLL THREADED
Published by SAE International on May 1, 1995
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering...
This document references:
AS7481 - STUDS, STEEL, CORROSION AND HEAT RESISTANT 1800°F Solution Heat Treated Precipitation Heat Treated After Roll Threaded
Published by SAE International on January 7, 1991
This procurement specification covers aircraft quality studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS...
This document references:
AS7482 - STUDS, STEEL, CORROSION AND HEAT RESISTANT 1800°F Solution Heat Treated Precipitation Heat Treated Before Roll Threaded
Published by SAE International on August 16, 2011
This procurement specification covers aircraft quality studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS...
This document references:
AS7489 - Standard Requirements for Aerospace Organic Coatings Applicator Certification
Published by SAE International on February 21, 2017
This standard establishes the minimum requirements for training, examination, and certification of aerospace coatings application personnel applying liquid organic coatings to interior structural or...
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