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Viewing 271 to 300 of 1454
CURRENT
2012-05-07
Standard
JA1000/1_201205
The importance of reliability in design engineering has significantly grown since the early 1960’s. Competition has been a primary driver in this growth. The three realities of competition today are: world class quality and reliability, cost-effectiveness, and fast time-to-market. Formerly, companies could effectively compete if they could achieve at least two of these features in their products and product development processes, often at the expense of the third. However, customers today, whether military, aerospace, or commercial, have been sensitized to a higher level of expectation and demand products that are highly reliable, yet affordable. Product development practices are shifting in response to this higher level of expectation. Today, there is seldom time, or necessary resources to extensively test, analyze, and fix to achieve high quality and reliability.
2012-05-07
WIP Standard
J4001
SAE J4001 provides instruction for evaluating levels of compliance to SAE J4000. Component text (Sections 4 to 9) from SAE J4000 is included for convenience during the evaluation process. Applicable definitions and references are contained in SAE J4000. SAE J4000 tests lean implementation within a manufacturing organization and includes those areas of direct overlap with the organization's suppliers and customers. If applied to each consecutive organizational link, an enterprise level evaluation can be made. SAE J4001 relates the following approximate topic percentages to the implementation process as a whole: Element 4 Management/Trust 25% Element 5 People 25% Element 6 Information Element 7 Supplier/Organization/Customer 25% (combined) Element 8 Product Element 9 Process/Flow 25% SAE J4001 is to be applied on a specific component basis. Each of the fifty-two components tests part of, one, or multiples of the specific requirements of lean implementation.
CURRENT
2012-05-07
Standard
JA1002_201205
This SAE Standard provides a framework for the management of software reliability within system reliability requirements. It is based around the Software Reliability Plan and Software Reliability Case and emphasizes the importance of evaluating progress towards meeting software reliability requirements throughout the project life-cycle.
CURRENT
2012-04-30
Standard
J1693_201204
This SAE Recommended Practice specifies the general characteristics and test procedure to define the minimum characteristics, performance, and durability requirements. It is applicable to remanufactured assemblies (factory rebuild) only. This document applies to master cylinder assemblies and components of current established designs but does not cover fluid level sensors, integral proportioning valves or those master cylinders used in anti-lock brake or traction control systems. These will be covered by other standards. The minimum characteristics, performance, and durability requirements are specified in SAE J1694.
HISTORICAL
2012-04-26
Standard
AS9110B
This standard includes ISO 9001:20081 quality management system requirements and specifies additional aviation maintenance industry requirements, definitions, and notes as shown in bold, italic text. NOTE: Baseline aviation maintenance requirements originate from IAQG developed 9100:2009 standard; modifications were made, as required, to address maintenance industry specific requirements. It is emphasized that the requirements specified in this standard are complementary (not alternative) to contractual and applicable statutory and regulatory requirements. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the latter shall take precedence.
2012-04-11
WIP Standard
AMS2431/6D
This specification, in conjunction with the general requirements covered in AMS 2431 establishes the requirements for glass shot to be used for peening of metal parts.
2012-04-11
WIP Standard
AMS2431/3E
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431.
2012-04-11
WIP Standard
AMS2431/4D
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431.
CURRENT
2012-03-19
Standard
J2489_201203
This SAE Recommended Practice is intended as the definition of a standard test, but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutches with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. The specific purpose of this document is to define a Durability Test based on a specific power level selected from either the 3600 r/min Stepped Power Test or from the 6000 r/min Stepped Power Test, for the evaluation of wet friction system performance variation as a function of number of cycles. This standard procedure is intended for common use by both suppliers and end users to allow objective comparisons of wet friction material system performance.
CURRENT
2012-03-19
Standard
J1499_201203
This SAE Recommended Practice is intended as a guide toward implementation of a standard practice but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE band friction test machine is used to evaluate the frictional characteristics of automatic transmission band friction materials with automatic transmission fluids. It can also be used to conduct durability tests on wet friction systems.
CURRENT
2012-03-19
Standard
J286_201203
This SAE Recommended Practice is intended as a guide toward implementation of a standard practice but may be subject to frequent change to keep pace with experience and technical advances. This should be kept in mind when considering its use. The SAE No. 2 Friction Test Machine is used to evaluate the friction characteristics of automatic transmission plate clutch with automotive transmission fluids. It can also be used to conduct durability tests on wet friction systems. This document is intended for common use by both suppliers and end users to define minimum test machine requirements to allow objective comparisons of wet friction material system performance.
CURRENT
2012-03-07
Standard
ARP9113A
Supply Chain Risk Management (SCRM), defined in this guideline, can be applied proactively for the protection of all procured products and services; both flying and non-flying through all levels of the supply chain. The guideline focuses on Quality as a key risk assessment factor taking into accoutn elements from all aspects of the business having a direct link to global quality management.
CURRENT
2012-02-17
Standard
J1153_201202
This SAE Standard specifies the test procedure to determine minimum performance and durability characteristics for master cylinder assemblies of current established designs, components of which conform to SAE Standards. It is applicable to new assemblies from commercial production and remanufacture (factory rebuild). The minimum performance and durability requirements are specified in SAE J1154.
CURRENT
2012-02-03
Standard
AMS2518D
This specification covers an anti-seize compound in the form of a grease.
CURRENT
2012-01-31
Standard
AS9104/1
The purpose of this standard is to define the requirements and industry-accepted practices for managing the ICOP scheme, which provides confidence to aviation, space, and defense customers and organizations that their suppliers with certification of their quality management systems, issued by accredited CBs, meet the applicable AQMS standard requirements. The requirements established in this standard are applicable to the IAQG and its three sectors for managing AQMS certification and associated activities. The requirements are applicable to IAQG working groups [e.g., SMS, Other Party Management Team (OPMT)], IAQG member companies, ABs, CBs, Certification Body Management Committees (CBMCs), AABs, TPABs, Training Providers (TPs), and organizations seeking/obtaining AQMS standard certification.
HISTORICAL
2012-01-09
Standard
J1390_201201
Three levels of fan structural analysis are included in this practice: Initial Structural Integrity In-vehicle Testing Durability Test Methods The Initial Structural Integrity section describes analytical and test methods used to predict potential resonance and, therefore, possible fatigue accumulation. The In-vehicle (or machine) section enumerates the general procedure used to conduct a fan strain gage test. Various considerations that may affect the outcome of strain gage data have been described for the user of this procedure to adapt/discard depending on the particular application. The Durability Test Methods section describes the detailed test procedures that may be used depending on type of fan, equipment availability, and end objective. Each of the previous levels builds upon information derived from the previous level. Engineering judgment is required as to the applicability of each level to a different vehicle environment or a new fan design.
CURRENT
2012-01-06
Standard
AMS2672G
This specification covers the requirements for producing brazed joints on aluminum and aluminum alloys by torch or furnace brazing.
CURRENT
2012-01-06
Standard
AMS2447D
This specification covers the requirements for thermal spray coatings applied using the high velocity oxygen fuel (HVOF) combustion process. This specification is not intended to be used for duplex coatings, i.e., the application of the coating over a previously applied coating.
CURRENT
2012-01-06
Standard
AMS2673E
This specification covers the requirements for producing brazed joints of aluminum and aluminum alloys by immersion in a molten flux bath.
CURRENT
2011-12-01
Standard
AIR4276A
This Aerospace Information Report (AIR) is the primary vehicle for providing the survey results to industry and government. The Institute of Defense Analysis (IDA), has performed a study which concludes that computerized techniques must be developed to integrate RM&S into product design in order to permit design influence from inception throughout the product life cycle. This AIR addresses the DoD initiative for developing Computer Aided Acquisition and Logistic Support (CALS) and industry's role in its evolution. AIR 4276 provides the detailed results of an industry/government survey inquiring into the extent of computerization of RM&S into the design process. Background information describes the evolution of the survey and why it was developed.
CURRENT
2011-11-22
Standard
AMS2431/5B
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS2431.
CURRENT
2011-11-22
Standard
AMS2700E
This specification covers the requirements for a process to assure removal of free iron or other less noble contaminants from the surfaces of corrosion resistant steel parts.
CURRENT
2011-11-21
Standard
J2958_201111
This report is applicable to the reliability characteristics of unmanned ground vehicles.
CURRENT
2011-11-16
Standard
J2940_201111
This SAE standard outlines the steps and known accepted methodologies and standards for linking Model V&V with model based product reliability assessments. The standard’s main emphasis is that quantified values for Model-based product reliability must be accompanied by a quantified confidence value if the users of the model wish to claim use of a “Verified and Validated” model, and if they wish to further link into business and investment decisions that are informed by quantitative second-order risk and benefit cost considerations.
CURRENT
2011-10-05
Standard
J2388_201110
This SAE Recommended Practice establishes a uniform procedure for assuring the manufactured quality, installed utility and performance of automotive products to the relocation, alteration, replacement and/or extension of secondary controls and systems other than those provided by the vehicle manufacturer (OEM). These products are intended to provide driving capability to persons with physical disabilities. These products function as adaptive modifications to compensate for lost or reduced function in the extremities of the driver. These include, but are not limited to the following: Cruise Control; Door Locks; Gear Selector; Hazard Flasher; Headlight Beam Selector; Heater/Vent/Air Conditioner (HVAC); Horn; Ignition/Starter; Light controls; Mirrors; Parking Brake; Power Seats; Turn Signals; Power Window Controls; and Windshield Wiper/Washer and defogger; Rear Accessories (Defogger, Wiper/Washer).
CURRENT
2011-10-05
Standard
AMS2429D
This specification covers the requirements for electrodeposited bronze plate and subsequent removal .
HISTORICAL
2011-09-23
Standard
AMS2770J
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (See 8.8.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (See 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
2011-09-21
WIP Standard
ARP9107A
Limited to the Commercial Aerospace industry where a request is made for a Production Organization (PO) to have Direct Delivery Authorization (DDA), which includes an Appropriate Arrangement (AA) between the PO and the Design Organization (DO). In this process the DO is responsible for ensuring the continuous updating of design and airworthiness data to the PO, whilst the PO is responsible for assurance that the manufactured article conforms to Approved Design and Airworthiness Data. The PO is responsible to provide airworthiness release documentation.
CURRENT
2011-09-19
Standard
AMS2434D
This specification covers the requirements for the electrodeposited tin-zinc alloy plating.
HISTORICAL
2011-09-13
Standard
AMS2773C
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts made of cast nickel or cobalt alloys and of fabricated assemblies in which cast nickel or cobalt alloys are the primary structural components. It is not intended to provide requirements for heat treating operations that are a responsibility of the casting supplier in meeting the requirements of the casting commodity specification.
Viewing 271 to 300 of 1454