49.025.15 - Non-ferrous alloys in general
ICS 49.025.15 Details
Non-ferrous alloys in general
Nichteisenmetalle im allgemeinen
Alliages non ferreux en general
Neželezove zlitine na splošno
General Information
Frequently Asked Questions
ICS 49.025.15 is a classification code in the International Classification for Standards (ICS) system. It covers "Non-ferrous alloys in general". The ICS is a hierarchical classification system used to organize international, regional, and national standards, facilitating the search and identification of standards across different fields.
There are 232 standards classified under ICS 49.025.15 (Non-ferrous alloys in general). These standards are published by international and regional standardization bodies including ISO, IEC, CEN, CENELEC, and ETSI.
The International Classification for Standards (ICS) is a hierarchical classification system maintained by ISO to organize standards and related documents. It uses a three-level structure with field (2 digits), group (3 digits), and sub-group (2 digits) codes. The ICS helps users find standards by subject area and enables statistical analysis of standards development activities.
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This document specifies the requirements for the hexavalent chromium free chemical conversion process of magnesium and magnesium alloys to ensure an adhesion base before bonding and painting.
The purpose of this document is to specify design, quality and manufacturing requirements. It does not specify complete in-house process instructions; these are specified in the processors detailed process instructions.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the hexavalent chromium free chemical conversion process of magnesium and magnesium alloys to ensure an adhesion base before bonding and painting.
The purpose of this document is to specify design, quality and manufacturing requirements. It does not specify complete in-house process instructions; these are specified in the processors detailed process instructions.
- Standard14 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications.
This Part 001 specifies the "General rules" framework valid for all parts.
- Standard26 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 003 specifies the "Specific rules for heat resisting alloys".
- Standard26 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications.
This Part 002 specifies the "Specific rules for aluminium, aluminium alloys and magnesium alloys".
- Standard28 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 003 specifies the "Specific rules for heat resisting alloys".
- Standard26 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 006 specifies the "Specific rules for filler metals for brazing".
- Standard20 pagesEnglish languagee-Library read for1 day
The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications.
This Part 001 specifies the "General rules" framework valid for all parts.
- Standard26 pagesEnglish languagee-Library read for1 day
This document specifies the general organization of metallic material standards for aerospace applications, their links with other types of European standards and their use.
It corresponds to level 0 (see 4.2).
From the date of publication of this document, specifications for different welding and brazing products can be written in only one standard instead of separated material standards. Already existing material standards for filler metals for welding and for brazing can continue to follow this organization.
- Standard15 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal. It is presupposed to be applied when referred to and in conjunction with the product procurement specification unless otherwise specified on the drawing, order or inspection schedule.
- Standard29 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal. It is presupposed to be applied when referred to and in conjunction with the product procurement specification unless otherwise specified on the drawing, order or inspection schedule.
- Standard29 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting nickel base alloy NiCr20Co3Fe3
Rm ≥ 650 MPa
Sheets and strips, cold rolled
0,25 mm < a ≤ 3 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted (ESR or VAR)
Solution treated and precipitation treated (H1025)
Bars for machining
a or D ≤ 250 mm
1 070 MPa ≤ Rm ≤ 1 200 MPa
Premium quality (pq)
for aerospace applications.
NOTE Other designation: The ASD-STAN designation of this material is FE-PM1802.
Only the chemical composition of this document are to be considered.
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting nickel base alloy NiCr20Co3Fe3
Rm ≥ 650 MPa
Sheets and strips, cold rolled
0,25 mm < a ≤ 3 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document defines the general terms to be used in the standards of metallic materials for aerospace applications. It is intended only to give terms which are truly general and where definition, in this context, is required. The definitions of more specific terms are to be found in the technical specifications, test methods, etc. which are referenced in the material standard concerned.
- Standard22 pagesEnglish, French and German languagee-Library read for1 day
This document specifies the rules for the drafting and presentation of technical specifications for metallic materials.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the rules for the drafting and presentation of test method standards.
- Standard15 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy CO-PH4101 (CoCr20W15Ni)
Vacuum melted
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document defines the general terms to be used in the standards of metallic materials for aerospace applications. It is intended only to give terms which are truly general and where definition, in this context, is required. The definitions of more specific terms are to be found in the technical specifications, test methods, etc. which are referenced in the material standard concerned.
- Standard22 pagesEnglish, French and German languagee-Library read for1 day
This document specifies the rules for the drafting and presentation of technical specifications for metallic materials.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the rules for the drafting and presentation of test method standards.
- Standard15 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy CO-PH4101 (CoCr20W15Ni)
Vacuum melted
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
SIGNIFICANCE AND USE
4.1 Advantages of Electrolytic Polishing:
4.1.1 For some metals, a high quality surface finish can be produced that is equivalent to, or better than, that which can be obtained by mechanical methods.
4.1.2 Once procedures have been established, satisfactory results can be obtained rapidly with reproducibility.
4.1.3 There can be a marked saving of time if many specimens of the same material are polished sequentially.
4.1.4 Electropolishing a selected area on the surface of a relatively large metal part can be accomplished nondestructively, that is, without the need for sectioning to remove a piece.
4.1.5 Soft, single-phase metals, which may be difficult to polish by mechanical methods, may be successfully electropolished.
4.1.6 The true microstructure of a specimen can be obtained because artifacts (such as disturbed metal, scratches, and mechanical twins) produced on the surface, even by careful grinding and mechanical polishing operations, can be removed. These features are important in low-load hardness testing, X-ray diffraction studies, and in electron microscopy, where higher resolution puts a premium on undistorted metal surfaces.
4.1.7 After electropolishing is completed, etching can often be accomplished by reducing the voltage (generally to about one-tenth that required for polishing) for a short time before it is turned off.
Note 2: Not all electropolishing solutions produce good etching results.
4.2 Disadvantages of Electrolytic Polishing:
4.2.1 Many of the chemical mixtures used in electropolishing are poisonous or dangerous if not properly handled (see Section 5). These hazards are similar to those involved in the mixing and handling of etchants, see Test Methods E407.
4.2.2 In multi-phase alloys, the polishing rate of each phase may be different. The result may be a non-planar surface.
4.2.3 Electropolished surfaces may be slightly undulated rather than perfectly planar and, therefore, may not be suitable for exami...
SCOPE
1.1 This guide deals with electrolytic polishing as a means of preparation of specimens for metallographic purposes. Procedures are described for polishing a variety of metals.
Note 1: References (1-133)2 on electrolytic polishing will provide the reader with specific information beyond the scope of this guide.
1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. Specific safety precautions are described in Section 5 and 6.3.1.
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
- Guide13 pagesEnglish languagesale 15% off
SIGNIFICANCE AND USE
3.1 This practice not only provides information on the accumulated effects of corrosion at specific time periods under a given set of conditions, but also provides information on the initial rate of corrosion of virgin metal, the corrosion rate of metal per unit time after long exposure, and the initial corrosion rate of virgin metal after long exposure of the corroding fluid to metal. The test also provides a means of determining the direction corrosion will take with time, although causes for increase or decrease in the corrosiveness and corrodibility of media and metal (such as passive film formation or destruction, depletion of corrosive contaminate, and so forth) as a function of time are not given.
SCOPE
1.1 This practice covers the determination of the corrosiveness of tank-type aircraft maintenance chemicals on aircraft metals and the corrodibility of metals in these maintenance chemicals with time. The determination is made under conditions of total immersion by a combination of weight change measurements and visual qualitative determinations of change.
1.2 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only.
1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific precautions, see Section 6.
1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
- Standard5 pagesEnglish languagesale 15% off
This document specifies the requirements relating to:
Heat resisting nickel base alloy (NI-P101HT)
Cold worked and solution treated
Bars for machining for fasteners
3 mm ≤ D ≤ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1)
Consumable electrode remelted
Cold drawn wire for the manufacture
of the thread inserts
D 3 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for penetrant testing of metallic materials for aerospace applications. It is limited to the direction of surface-breaking defects, e.g. cracks, laps, seams and inclusions.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard9 pagesEnglish languagee-Library read for1 day
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the radiographic testing of castings for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or testing schedule.
- Standard7 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting nickel base alloy Ni-P96-HT
Cold drawn and precipitation treated
Wire
D ≤ 10 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the test for the determination of the resistance of non-metallic materials in part or in whole to flame and glow propagation and to flame penetration.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the 45° Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard15 pagesEnglish languagee-Library read for1 day
This document specifies the test method for the determination of the vertical flame propagation and after flame time of non-metallic materials in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the vertical Bunsen burner test:
a) with a flame application time of 60 s;
b) with a flame application time of 12 s.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the test method for the determination of the horizontal flame propagation of non-metallic materials when subjected to a small flame in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the horizontal Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to:
Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1)
Consumable electrode remelted
Cold drawn wire for the manufacture
of the thread inserts
D 3 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting nickel base alloy Ni-P96-HT
Cold drawn and precipitation treated
Wire
D ≤ 10 mm
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for penetrant testing of metallic materials for aerospace applications. It is limited to the direction of surface-breaking defects, e.g. cracks, laps, seams and inclusions.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard9 pagesEnglish languagee-Library read for1 day
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the radiographic testing of castings for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or testing schedule.
- Standard7 pagesEnglish languagee-Library read for1 day
This document specifies the test for the determination of the resistance of non-metallic materials in part or in whole to flame and glow propagation and to flame penetration.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the 45° Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard15 pagesEnglish languagee-Library read for1 day
This document specifies the test method for the determination of the horizontal flame propagation of non-metallic materials when subjected to a small flame in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the horizontal Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the test method for the determination of the vertical flame propagation and after flame time of non-metallic materials in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the vertical Bunsen burner test:
a) with a flame application time of 60 s;
b) with a flame application time of 12 s.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the designation rules for metallic semi-finished products given in Table 1, used in aerospace construction.
It is applicable only if referred to in the metallic semi-finished product standard.
- Standard27 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard defines the determination of density according to displacement method for metallic materials.
- Standard4 pagesEnglish languagee-Library read for1 day
This standard specifies the requirements relating to:
This European Standard specifies the requirements relating to:
Heat resisting
Nickel base alloy Ni-Cr20Co3Fe3
Annealed
Bars
for aerospace applications.
- Standard7 pagesEnglish languagee-Library read for1 day
This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal for brazing for aerospace applications. It shall be applied when referred to in the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard22 pagesEnglish languagee-Library read for1 day
This standard specifies the requirements relating to:
This European Standard specifies the requirements relating to:
Heat resisting
Nickel base alloy Ni-Cr20Co3Fe3
Annealed
Bars
for aerospace applications.
- Standard7 pagesEnglish languagee-Library read for1 day
This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal for brazing for aerospace applications. It shall be applied when referred to in the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard22 pagesEnglish languagee-Library read for1 day
This European Standard specifies the rules for establishing the conventional designation of unalloyed, commercially pure and alloyed metallic materials used for aerospace applications.
NOTE Information relating to former ASD-STAN designations for nickel base or cobalt base alloys, steel, commercially pure titanium and titanium base alloys, is contained in Annex (informative).
- Standard30 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm
for aerospace applications.
NOTE Other designation: Only the chemical composition of this standard must be considered.
- Standard8 pagesEnglish languagee-Library read for1 day
This European Standard specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm
for aerospace applications.
NOTE Other designation: Only the chemical composition of this standard must be considered.
- Standard8 pagesEnglish languagee-Library read for1 day
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