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Viewing 35551 to 35580 of 35878
HISTORICAL
2000-09-01
Standard
AS5385
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: a. cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or b. non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
CURRENT
2017-10-30
Standard
AS5371A
This SAE Aerospace Standard (AS) establishes requirements for the manufacture of shim-type reference standards containing artificial flaws (notches) for use in the magnetic particle inspection process.
HISTORICAL
2002-07-15
Standard
AS5385A
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
HISTORICAL
2004-11-17
Standard
AS5385B
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of NAS 3610, or non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
CURRENT
2017-05-08
Standard
AS5385D
This SAE Aerospace Standard (AS) aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22250 N (5000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain cargo on board civil transport aircraft during flight: cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, or non-unitized individual pieces of cargo, or pieces of, cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
HISTORICAL
2007-01-09
Standard
AS5385C
This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22,250 N (5,000 lbf) rated ultimate tension load capability, as used by the airline industry in order to restrain on board civil transport aircraft during flight: cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main/upper deck cargo systems and meeting the requirements of NAS 3610 or AS36100, or non-unitized individual pieces of cargo, or pieces of, cargo placed onto an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments of an aircraft.
HISTORICAL
2009-04-02
Standard
AS5553
This SAE Aerospace Standard standardizes practices to: maximize availability of authentic parts, procure parts from reliable sources, assure authenticity and conformance of procured parts, control parts identified as counterfeit, and report counterfeit parts to other potential users and Government investigative authorities.
HISTORICAL
2013-01-21
Standard
AS5553A
This SAE Aerospace Standard standardizes practices to: maximize availability of authentic parts, procure parts from reliable sources, assure authenticity and conformance of procured parts, control suspect or confirmed fraudulent/counterfeit EEE parts, and report suspect or confirmed fraudulent/counterfeit EEE parts to other potential users and Authority Having Jurisdiction. and assess, mitigate, control, and report parts which have been used, refurbished, or reclaimed, but represented as new product.
2017-01-18
WIP Standard
AS5553C
This standard is for use by organizations that procure and/or integrate EEE parts and/or assemblies containing such items. The requirements of this standard are generic and intended to be applied/flowed down, as applicable, through the supply chain to all organizations that procure EEE parts and/or assemblies, regardless of type, size, and product provided. The mitigation of counterfeit EEE parts in this standard is risk-based and these mitigation steps will vary depending on the application, desired performance, and reliability of the equipment/hardware. The requirements of this document are intended to supplement the requirements of a higher level quality standard (e.g., AS/EN/JISQ9100, ISO-9001, ANSI/ASQC E4, ASME NQA-1, AS9120, AS9003, and ISO/TS 16949 or equivalent) and other quality management system documents.
CURRENT
2016-09-12
Standard
AS5553B
This standard is for use by organizations that procure and/or integrate EEE parts and/or assemblies containing such items. The requirements of this standard are generic and intended to be applied/flowed down, as applicable, through the supply chain to all organizations that procure EEE parts and/or assemblies, regardless of type, size, and product provided. The mitigation of counterfeit EEE parts in this standard is risk-based and these mitigation steps will vary depending on the application, desired performance, and reliability of the equipment/hardware. The requirements of this document are intended to supplement the requirements of a higher level quality standard (e.g., AS/EN/JISQ9100, ISO-9001, ANSI/ASQC E4, ASME NQA-1, AS9120, AS9003, and ISO/TS 16949 or equivalent) and other quality management system documents.
HISTORICAL
2012-07-25
Standard
AS5653A
AS5653 may be applied to Air Vehicles and Stores implementing MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System.
HISTORICAL
2008-01-16
Standard
AS5653
AS5653 may be applied to Air Vehicles and Stores implementing MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System.
CURRENT
2017-10-11
Standard
AS6089
This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that this verification document only verifies the specific requirements from AS5653 and does not verify all of the requirements invoked by documents that are referenced by AS5653. The procuring authority may require further testing to verify the requirements not explicitly defined in AS5653 and in this verification document.
2014-04-22
WIP Standard
AS6129A
This standard defines a generic set of electrical interfaces between a host aircraft (“platform”) and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power.
CURRENT
2014-01-03
Standard
AS5653B
AS5653 may be applied to Air Vehicles and Stores implementing MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System.
CURRENT
2012-12-05
Standard
AS6129
This standard defines a generic set of electrical interfaces between a host aircraft (“platform”) and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power.
HISTORICAL
2012-05-01
Standard
AS6174
This SAE Standard standardizes practices to: maximize availability of authentic materiel, procure materiel from reliable sources, assure authenticity and conformance of procured materiel, including methods such as certification, traceability, testing and inspection appropriate to the commodity/item in question, control materiel identified as fraudulent/counterfeit, and report suspect or confirmed fraudulent/counterfeit materiel to other potential users and Authority Having Jurisdiction.
CURRENT
2013-02-14
Standard
AS6169
This standard defines the mechanical interface and specifies provisions for the electrical and environmental connectors between the host aircraft (“platform”) and a turreted electro-optic/infrared (EO/IR) sensor.
CURRENT
2014-07-29
Standard
AS6174A
This SAE Standard standardizes practices to: maximize availability of authentic materiel, procure materiel from reliable sources, assure authenticity and conformance of procured materiel, including methods such as certification, traceability, testing and inspection appropriate to the commodity/item in question, control materiel identified as fraudulent/counterfeit, and report suspect or confirmed fraudulent/counterfeit materiel to other potential users and Authority Having Jurisdiction.
HISTORICAL
2000-05-01
Standard
AMS5680H
This specification covers a corrosion and heat resistant steel in the form of welding wire.
CURRENT
2006-01-12
Standard
AMS5680J
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
HISTORICAL
1994-05-01
Standard
AMS5680G
This specification covers a corrosion and heat resistant steel in the form of welding wire.
HISTORICAL
1988-04-01
Standard
AMS5680F
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of corrosion and heat resistant steels and alloys, but usage is not limited to such applications.
HISTORICAL
1970-05-01
Standard
AMS5704A
This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock. These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.
2016-09-22
WIP Standard
AMS5680K
This specification covers a corrosion and heat resistant steel in the form of welding wire.

This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of corrosion and heat resistant steels and alloys, but usage is not limited to such applications.

HISTORICAL
1976-01-01
Standard
AMS5704B
This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock. These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.
HISTORICAL
1966-03-01
Standard
AMS5704
This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock. These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.
HISTORICAL
1939-12-01
Standard
AMS5680
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of corrosion and heat resistant steels and alloys, but usage is not limited to such applications.
HISTORICAL
1948-07-01
Standard
AMS5680A
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of corrosion and heat resistant steels and alloys, but usage is not limited to such applications.