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CURRENT
2017-04-26
Standard
AS9146
This standard defines FOD Prevention Program requirements for organizations that design, develop, and provide aviation, space, and defense products and services; and by organizations providing post-delivery support, including the provision of maintenance, spare parts, or materials for their own products and services. It is emphasized that the requirements specified in this standard are complementary (not alternative) to customer, 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.
2017-04-20
WIP Standard
AS9104/1A
These requirements are applicable to IAQG global sectors when utilizing Aerospace Industry Controlled Other Party (ICOP) schemes for the assessment and certidication of supplier quality systems in accordance with the requirements AS/EN/SJAC 9104.
2017-04-20
WIP Standard
AS9103B
This standard is primarily intended to apply to new parts and products, but can also be applied to parts currently in production. The standard shall be applicable to all production processes, that influence the variation of KCs, as well as maintenance processes in which KCs are identified. It applies to assemblies and all levels of parts within an assembly, down to the basic materials including castings and forgings, and to organizations that are responsible for producing the design characteristics of the product. It does not apply to lab-scale, pilot, or pre-production processes. However, particular management of some KCs might be required using other methods than those described in the standard, during these phases of a program, when required by the customer or deemed appropriate by the organization (e.g., Engineering department requirement).
2017-04-19
WIP Standard
AMS2420E
This specification covers the requirements for preparation of aluminum and aluminum alloys for soldering by zinc immersion pre-treatment followed by copper plating and tin or tin-zinc alloy plating.
2017-04-19
WIP Standard
AMS2429E
This specification covers the requirements for electrodeposited bronze plate and subsequent removal.
2017-04-19
WIP Standard
AMS2442B
This specification establishes acceptance criteria for discontinuities revealed by magnetic particle inspection of parts made from wrought, ferromagnetic materials.
2017-04-19
WIP Standard
AMS2447E
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.
2017-04-19
WIP Standard
AMS2487B
This specification describes the engineering requirements for producing an electrically-insulating, non-powdery anodic coating on titanium and titanium alloys and the properties of such coatings.
2017-04-19
WIP Standard
AMS2672H
This specification covers the requirements for producing brazed joints on aluminum and alumiinum alloys by torch or furnace brazing.
2017-04-19
WIP Standard
AMS2819C
This specification covers the procedures for identification and marking of bare welding wire by a color code system and marking of spools.
2017-04-19
WIP Standard
AMS2673F
This specification covers the requirements for producing brazed joints of aluminum and aluminum alloys by immersion in a molten flux bath.
2017-04-04
WIP Standard
AMS2249H
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer. When specifically referenced in the material specification, the purchaser may apply check analysis limits to determine the acceptability of parts and materials at purchaser final acceptance or verification testing operation. Check analysis limits are not for producers use at producer’s acceptance testing. Composition of parts and materials must conform to the limits of the material specification. Check limits are not permitted for ladle or ingot analysis.
CURRENT
2017-03-28
Standard
ARP9162A
The focus of Operator Self-Verification is on traditional manufacturing operations, and applications can be made wherever traditional inspection is employed. The practices recommended in this document are intended to identify the basic elements and provide a “guideline” for structuring Operator Self-Verification programs within the aerospace industry; applicable to producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines and composite components. Operator Self-Verification programs are applied to improve the overall efficiency and product quality of processes considered mature, as judged by the implementing organization. Operator Self-Verification programs are not stand-alone processes, but augment existing quality management systems.
CURRENT
2017-03-17
Standard
J3083_201703
This document should be used as guidance for non-handbook based reliability predictions conducted on automotive electronics products. It presents a method that utilizes warranty and field repair data to calculate the failure rates of individual electronic components and predict the reliability of the entire electronic system. It assumes that the user has access to a database containing field return data with classification of components, times to failure, and a total number of components operating in the field.
CURRENT
2017-03-13
Standard
J2995_201703
This recommended practice will specify a standard duty cycle and set of conditions for component-level durability testing. The "duty cycle" refers to a set of loading conditions (e.g. torque or pressure and cycling count), and the 'test conditions" refers to environmental conditions such as temperature, humidity, and part conditioning from prior exposure (e.g. heat aging).
2017-02-16
WIP Standard
AMS2745B
This specification defines the requirements for locally hardening steel parts by the induction hardening method.
CURRENT
2017-02-13
Standard
J1530_201702
This test method covers determination of abrasion resistance, fiber loss and bearding resistance of automotive carpet materials.
CURRENT
2017-02-13
Standard
AIR1922B
This SAE Aerospace Information Report presents the following factors that affect hydraulic pump life and performance: The need to supply hydraulic fluid at the correct pressure and quality to the pump inlet port Considerations for the pump output Factors to be considered for the pump case drain lines The mounting of the hydraulic pump Hydraulic fluid properties, including cleanliness
CURRENT
2017-02-10
Standard
AMSSTD595A
This standard defines a color index system used by, but not limited to, Government activities in a format suitable for color identification, color selection, color matching, and quality control inspection. It also describes the designation and use of color media that is available to conduct these activities. Use of the color index referenced in this standard is intended to promote standardization and consistency in the color of items produced for Government use. Color media is described as follows: Color Chip Representation, Fan Deck: Suitable for color identification and selection. Color Chip Representation, Color Book: Suitable for color identification and selection. Precise Color Matching, Individual Color Chips: Suitable for color matching and quality control inspection purposes. Precise Color Matching, Set of Color Chips: Suitable for color matching and quality control inspection purposes.
CURRENT
2017-02-08
Standard
AMS2629E
This specification covers a mixture of liquid hydrocarbons and soluble additives.
CURRENT
2017-02-07
Standard
AMS2503G
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
CURRENT
2017-02-02
Standard
J379_201702
Hardness measurements are used as a quality control check of the consistency of formulation and processing of brake linings. Gogan hardness is nondestructive (the penetrator causes shallow surface deformation.). Gogan hardness method alone does not show anything about a lining’s ability to develop friction or to resist fade when used as a friction element in brakes. The hardness and the range of hardness are peculiar to each formulation, thickness, and contour; therefore, the acceptable values and ranges must be established for each formulation and part configuration by the manufacturer.
CURRENT
2017-02-02
Standard
J380_201702
Specific gravity is a nondestructive test used as a quality control check of the consistency of formulation and processing of brake lining. The specific gravity and the range of specific gravity are peculiar to each formulation and, therefore, the acceptable values or range must be established for each formulation by the manufacturer. Specific gravity alone shows nothing about a materials in use performance. The specific gravity of sintered metal powder friction materials, particularly those which have steel backing members, is usually determined somewhat differently. Reference ASTM B 376.
CURRENT
2017-02-01
Standard
AS9115A
The requirements of 9100 apply with the following clarification for software. This standard supplements the 9100 standard requirements for deliverable software and contains quality management system requirements for organizations that design, develop, and/or produce deliverable software and services for the aviation, space, and defense industry. This includes, as required, support software that is used in the development and maintenance of deliverable software and services. The deliverable software may be stand-alone, embedded, mobile application, or loadable into a target computer. This deliverable software may also be part of services (e.g., cloud environment, web hosted solutions or platforms).
2016-12-24
WIP Standard
TAHB0009A
This handbook provides "how to" guidance to industry and government for the reliability Activities and Methods contained in ANSI/GEIA-STD-0009 for developing reliable products and systems, successfully demonstrating them during test and evaluation, and sustaining them throughout the system/product life cycle. ANSI/GEIA-STD-0009 requires the developers and customer/users working as a team to plan and implement a reliability program that provides systems/products that satisfy the user's requirements and expectations using a systems engineering approach. The four Objectives of ANSI/GEIA-STD-0009 are listed below: Objective 1: Understand Customer/User Requirements and constraints. The team (developer, customer, and user), includes the Activities necessary to ensure that the user's requirements and product needs are fully understood and defined, so that a comprehensive design specification and Reliability Program Plan are generated. Objective 2: Design and redesign for reliability.
2016-12-14
WIP Standard
ARP5890B
This document establishes guidelines for a Reliability Assessment Plan (herein also called the Plan), in which Electronic Engine Control manufacturers document their controlled, repeatable processes for assessing reliability of their products. Each Electronic Engine Control manufacturer (the Plan owner) prepares a Plan, which is unique to the Plan owner. This document describes processes that are intended for use in assessing the reliability of Electronic Engine Controls, or subassemblies thereof. The results of such assessments are intended for use as inputs to safety analyses, certification analyses, equipment design decisions, system architecture selection and business decisions such as warranties or maintenance cost guarantees.
CURRENT
2016-11-12
Standard
AIR5120A
For Engine Monitoring Systems to meet their potential for improved safety and reduced operation and support costs, significant attention must be focused on their reliability and validity throughout the life cycle. This AIR will provide program managers, designers, developers and customers a concise reference of the activities, approaches and considerations for the development and verification of a highly reliable engine monitoring system. When applying the guidelines of this AIR it should be noted that engine monitoring systems physically or functionally integrated with the engine control system and/or performing functions that affect engine safety or are used to effect continued operation or return to service decisions shall be subject to the Type Investigation of the product in which they'll be incorporated and have to show compliance with the applicable airworthiness requirements as defined by the responsible Aviation Authority.
CURRENT
2016-11-10
Standard
J2318_201611
This procedure provides test performance requirements for service, spring applied parking, and double diaphragm combination air brake actuators with respect to durability, function, and environmental performance when tested in accordance to SAE J1469.
CURRENT
2016-11-08
Standard
AS9162
This document identifies the basic elements and provides a standard for structuring operator self-verification programs within the aviation, space, and defense industry for producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines, and composite components. 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.
CURRENT
2016-11-08
Standard
AS9145
This standard establishes requirements for performing and documenting APQP and PPAP. APQP begins with conceptual product needs and extends through product definition, production planning, product and process validation (i.e., PPAP), product use, and post-delivery service. This standard integrates and collaborates with the requirements of the 9100, 9102, 9103, and 9110 standards. 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.
Viewing 1 to 30 of 1425