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SAE Industry Technologies Consortia - AS5550-4

AS5550-5605 Chain (8m/m Pitch) and Fittings Assembly Code. Non-Reversible Control

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Organization: SAE Industry Technologies Consortia
Publication Date: 11 June 1951
Status: active
description:

No scope available.

Document History

AS5550-4
June 11, 1951
AS5550-5605 Chain (8m/m Pitch) and Fittings Assembly Code. Non-Reversible Control
No scope available.

References

This document references:
AS5550 - FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI
Published by SAE International on October 28, 2005
A description is not available for this item.
This document references:
AS5551 - Fitting Assembly - 24° Cone Flareless per AS5827, 5080 psi, Port Connection Port Preparation, Installation and Removal of AS5550 and AS5865
Published by SAE International on October 28, 2005
This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is...
This document references:
AS5553 - Counterfeit Electronic Parts; Avoidance, Detection, Mitigation, and Disposition
Published by SAE International on April 2, 2009
This SAE Aerospace Standard standardizes practices to: a maximize availability of authentic parts, b procure parts from reliable sources, c assure authenticity and conformance of procured parts, d...
This document references:
AS5562 - Ice and Rain Minimum Qualification Standards for Pitot and Pitot-static Probes
Published by SAE International on February 11, 2020
This SAE Aerospace Standard (AS) establishes minimum ice and rain performance criteria for electrically-heated pitot and pitot-static probes intended for use on the following classes of fixed-wing...
This document references:
AS5586 - Aerospace - General Requirements for Hydraulic System Reservoirs
Published by SAE International on February 16, 2005
This SAE Aerospace Standard (AS) specifies the general requirements for hydraulic system reservoirs that are installed in commercial and military aircraft and helicopters and also in missile...
This document references:
AS5587 - CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFT
Published by SAE International on June 25, 2004
A description is not available for this item.
This document references:
AS5590 - Connectors, Fiber Optic, Advanced, Circular or Rectangular, Plug and Receptacle, Environment Resistant, Removable Termini, General Specification For
Published by SAE International on February 24, 2004
This specification covers the performance requirements for a plug and receptacle, multiple termini, fiber optic connector. Fiber optic connectors using removable termini, and are capable of operating...
This document references:
AS5603 - Digital Fiber Optic Link Loss Budget Methodology for Aerospace Platforms
Published by SAE International on November 20, 2007
This SAE Technical Report is an Aerospace Standard, compliant with the Organization and Operating Guide for the Aerospace Council of the SAE Technical Standards Board. It is consistent with the...
This document references:
AS5604 - Compass; Magnetic, Pilot's Standby
Published by SAE International on April 1, 1999
This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot's standby compasses as specified herein.
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