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SAE Industry Technologies Consortia - AS650-9

AS650-699 Labels

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Organization: SAE Industry Technologies Consortia
Publication Date: 1 August 1986
Status: active
description:

No scope available.

Document History

AS650-9
August 1, 1986
AS650-699 Labels
No scope available.

References

This document references:
AS650 - HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METAL BRAID, MEDIUM PRESSURE, FLARELESS, 45° TO 45°
Published by SAE International on February 1, 1994
A description is not available for this item.
This document references:
AS651 - HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METAL BRAID, MEDIUM PRESSURE, FLARELESS, 45° TO 90°
Published by SAE International on February 1, 1994
A description is not available for this item.
This document references:
AS652 - HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METAL BRAID, MEDIUM PRESSURE, FLARELESS, 90° TO 90°
Published by SAE International on February 1, 1994
A description is not available for this item.
This document references:
AS654 - CABLE, SPECIAL PURPOSE, ELECTRICAL: WIRE, ELECTRICAL (IGNITION, HIGH-TENSION)
Published by SAE International on July 1, 1994
This Aerospace Standard covers insulated, high-tension, shielded, special purpose cable and unshielded electrical cable for ignition systems of internal combustion engines for aircraft.
This document references:
AS665 - TAPERED AXLE COLLAR DIMENSIONS
Published by SAE International on July 9, 2007
A description is not available for this item.
This document references:
AS666 - CAVITY DESIGN AND O-RING SELECTION FOR STATIC SEAL USE IN AIRCRAFT TUBELESS TIRE WHEELS
Published by SAE International on November 1, 1963
This standard applies to the cavity design and the selection of O-rings for tubeless tire wheels.
This document references:
AS678 - GASKET - 18MM FOLDED STEEL AIRCRAFT
Published by SAE International on August 1, 1960
A description is not available for this item.
This document references:
AS686 - PILOTED RING SEAL TUBE SWIVEL CONNECTION ASSEMBLY
Published by SAE International on March 15, 1969
This standard presents the designer with sufficient information to fully define the configuration of the connection and to determine the limits of application for given conditions.
This document references:
AS692 - IGNITER, SPARK, AERONAUTICAL ENGINE (HIGH TENSION)
Published by SAE International on November 1, 1962
This specification establishes the qualification and acceptance limits for aeronautical engine high tension spark igniters.
This document references:
AS696 - Aircraft Constant Displacement Hydraulic Motor
Published by SAE International on December 16, 2002
A description is not available for this item.
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