ASD-STAN/D 4 - Metallic
D 04/WG 16 « Sealants (Mastics) » committee, will prepare, coordinate, and revise documents related to sealants (mastics) (e.g. sulphide based, silicone based, polyester based, acrylic based, epoxy based, polyurethane based, butyle based). Documents can be a technical specification and materials standards.
Metallic
D 04/WG 16 « Sealants (Mastics) » committee, will prepare, coordinate, and revise documents related to sealants (mastics) (e.g. sulphide based, silicone based, polyester based, acrylic based, epoxy based, polyurethane based, butyle based). Documents can be a technical specification and materials standards.
General Information
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 languagesale 10% offe-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 005 specifies the "Specific rules for steels".
- Standard24 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-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 languagesale 10% offe-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 004 specifies the "Specific rules for titanium and titanium alloys".
- Standard25 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted
Solution treated and precipitation treated
Sheets and strips
a ≤ 6 mm
1 070 MPa ≤ Rm ≤ 1 220 MPa
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted
Solution treated and precipitation treated
Bars for machining
a or D ≤ 200 mm
Rm ≥ 1 310 MPa
for aerospace applications.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X4CrNiMo16-5-1 (1.4418)
Air melted
Hardened and tempered
Bars
De ≤ 200 mm
900 MPa ≤ Rm ≤ 1 050 MPa
for aerospace applications.
NOTE Other common designations:
AIR: Z 8 CND 17 04.
Only the chemical composition of this document are considered.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X4CrNiMo16-5-1 (1.4418)
Air melted
Hardened and tempered
Forgings
De ≤ 200 mm
900 MPa ≤ Rm ≤ 1 050 MPa
for aerospace applications.
NOTE Other common designations:
AIR: Z 8 CND 17 04.
Only the chemical composition of this document are considered.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Steel X4CrNiMo16-5-1
Air melted
Hardened and tempered
Sheets and plates
0,3 mm ≤ a ≤ 50 mm
900 MPa ≤ Rm ≤ 1 050 MPa
for aerospace applications.
ASD-STAN designation: FE-PM 3504.
- Amendment4 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Amendment4 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Bars for machining
D < 300 mm
900 MPa ≤ Rm ≤ 1 160 MPa
for aerospace applications
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel 15CrMoV6 (1.7334)
Air melted
Hardened and tempered
Sheet and strip
0,5 mm ≤ a ≤ 6 mm
980 MPa ≤ Rm ≤ 1 180 MPa
for aerospace applications.
W.nr: 1.7334.
ASD-STAN designation: FE-PL1505.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This test method describes the principles applicable to infrared transmission spectrophotometric analysis of organic compounds (elastomers, basic resins, resin mixes or resin systems) used as the matrix in reinforced polymers, adhesives, bonding primers and, in general terms, all organic compounds.
The method could also be applied to some inorganic products.
It is intended to be used jointly with special test conditions specified in the materials specification invoking the test.
This document does not give any directions necessary to meet the health and safety requirements. It is the responsibility of the user of this document to adopt appropriate health and safety precautions.
- Standard27 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel 15CrMoV6 (1.7334)
Air melted
Hardened and tempered
Plates
6 mm ≤ a ≤ 20 mm
1 080 MPa ≤ Rm ≤ 1 280 MPa
for aerospace applications.
W.nr: 1.7334.
ASD-STAN designation: FE-PL1505.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel 15CrMoV6 (1.7334)
Air melted
Hardened and tempered
Sheets and strips
2 mm ≤ a ≤ 6 mm
1 080 MPa ≤ Rm ≤ 1 280 MPa
for aerospace applications.
W.nr: 1.7334.
ASD-STAN designation: FE-PL1505.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the requirements for micro-arc oxidation of aluminium and aluminium alloys for corrosion protection, wear, erosion, dielectric and thermal properties.
The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processors detailed process instructions.
This document relates only to micro-arc oxidation. It does not relate to finishing techniques, such as mechanical post treatment.
- Standard24 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the requirements for hexavalent chromium free anodic electrodeposition of organic coatings on aluminium and aluminium alloys for corrosion protection of parts.
The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processors detailed process instructions.
- Standard20 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-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 languagesale 10% offe-Library read for1 day
This document specifies the dimensions and tolerances for drawn corrosion resisting steel lockwire for aerospace applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies a list of procurement specifications and standards for welding products authorized for the welding of parts.
- Standard44 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the Izod impact test method for steel products used 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 inspection schedule.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X4CrNiMo16-5-1 (1.4418)
Air melted
Hardened and tempered
Forgings
De ≤ 200 mm
1 150 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.
NOTE Other common designations:
- AIR: Z 8 CND 17-04.
- Only the chemical composition according to this document is considered.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X4CrNiMo16-5-1 (1.4418)
Air melted
Hardened and tempered
Bars
De ≤ 200 mm
1 150 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.
NOTE Other common designations:
- AIR: Z 8 CND 17-04.
- Only the chemical composition according to this document is considered.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu 17 4 (1.4542)
Air melted
Solution treated and precipitation treated
Sheets and strips
a ≤ 6 mm
Rm ≥ 1 070 MPa
for aerospace applications.
Material no (W.nr): 1.4542.
The ASD STAN designation of this material is FE PM3801.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted, softened
Forging stocks
a or D ≤ 300 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the sampling plan for acceptance testing of aramid, carbon fibre and textile glass filament yarns in terms of sample size and rejection criteria.
This document serves as a basis for the corresponding technical specification. It covers the inspection by attributes. The inspection by measurements (variables) will be added in subsequent edition. It is also planned to extend its scope of application to reinforcing woven fabrics.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu 17 4 (1.4542)
Air melted
Solution treated and precipitation treated
Plates
6 mm ≤ a ≤ 100 mm
Rm ≥ 1 070 MPa
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted
Solution treated and precipitation treated
Plates
6 mm < a ≤ 20 mm
1 070 MPa ≤ Rm ≤ 1 220 MPa
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of self-extinguishing and low smoke emission semi-finished polycarbonate sheets with and without UV radiation protection requirement, as used for aircraft equipment, such as internal panelling, simple internal glazing, sound-proofing panels, light covers, etc.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X3CrNiMoAl (13-8-2)
Vacuum induction melted and consumable electrode remelted
Solution treated and precipitation treated
Bars for machining
a or D ≤ 200 mm
1 200 MPa ≤ Rm ≤ 1 350 MPa
for aerospace applications.
Material no (W.L): 1.4534.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3)
Solution treated and precipitation treated
Bars and sections
De ≤ 200 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy AL-P6061-T4
Drawn tube for pressure applications
0,6 mm ≤ a ≤ 3 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel 36NiCrMo16
1 000 MPa ≤ Rm ≤ 1 200 MPa
Bars
100 mm ≤ D ≤ 250 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMnMoV26-15 (1.4944)
Softened and cold worked
Wire for forged fasteners
D ≤ 15 mm
1 100 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Standard13 pagesEnglish languagesale 10% offe-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 languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 5086
H111
Extruded bars
10 mm ≤ D ≤ 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Steel X4CrNiMo16-5-1
Air melted
Hardened and tempered
Sheets and plates
0,3 mm ≤ a ≤ 50 mm
900 MPa ≤ Rm ≤ 1 050 MPa
for aerospace applications.
ASD-STAN designation: FE-PM 3504.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general organization of the EN standards for non-metallic materials and their links with other types of standards for aerospace applications.
It corresponds to level 0 (see 4.1).
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements for a range of one part anaerobic polymerisable compounds
which polymerises upon the exclusion of oxygen and activation by a metal surface.
- Standard17 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general rules for drafting and presentation of EN aerospace series non-metallic material technical specifications.
- Standard21 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the rules for the drafting and presentation of test method standards.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the rules for the drafting and presentation of technical specifications for metallic materials.
- Standard18 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the method for depositing cadmium layers according to the vacuum deposition process, for use in aerospace construction.
According to this process, cadmium metal is vaporized under vacuum and deposited directly on the base material with an interlayer. The coating produced in this way is ductile and electrically conductive.
This document is applicable whenever referenced.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Steel X6CrNiTi18-10 (1.4541)
Air melted
Softened
Wires
0,25 mm ≤ De ≤ 3 mm
Rm ≤ 780 MPa
for aerospace applications.
Material number: 1.4541.
ASD-STAN designation: FE-PA3601.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day