49.025 - Materials for aerospace construction
ICS 49.025 Details
Materials for aerospace construction
Materialien der Luft- und Raumfahrttechnik
Materiaux pour la construction aeronautique
Materiali za letalsko in vesoljsko gradnjo
General Information
Frequently Asked Questions
ICS 49.025 is a classification code in the International Classification for Standards (ICS) system. It covers "Materials for aerospace construction". 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 2116 standards classified under ICS 49.025 (Materials for aerospace construction). 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 relating to:
Steel GX5CrNiCuNb16-4 (1.4525)
Homogenized
Solution treated and precipitation hardened
Investment casting
De ≤ 50 mm
Rm ≥ 900 MPa
for aerospace applications.
ASD-STAN designation FE-CM3801
Material number 1.4525
- Standard9 pagesEnglish languagee-Library read for1 day
This document gives guidance on the use of regrinds and recycled materials for thermoplastic parts for aerospace use.
This document does not apply to reinforced thermoplastic materials, such as short fibre-reinforced plastics, due to their distinct processing characteristics, material degradation concerns, and stringent aerospace performance requirements.
The intended manufacturing processes for these virgin/regrind blends include standard thermoplastic methods such as injection moulding, extrusion, and blow moulding, among others as appropriate to the application.
- Standard5 pagesEnglish languagee-Library read for1 day
This document is applicable to the tensile testing and specifies the requirements of metallic materials at elevated temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard29 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel GX5CrNiCuNb16-4 (1.4525)
Homogenized
Solution treated and precipitation hardened
Investment casting
De ≤ 50 mm
Rm ≥ 900 MPa
for aerospace applications.
ASD-STAN designation FE-CM3801
Material number 1.4525
- Standard9 pagesEnglish languagee-Library read for1 day
This document is applicable to the tensile testing and specifies the requirements of metallic materials at elevated temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard29 pagesEnglish languagee-Library read for1 day
This document gives guidance on the use of regrinds and recycled materials for thermoplastic parts for aerospace use.
This document does not apply to reinforced thermoplastic materials, such as short fibre-reinforced plastics, due to their distinct processing characteristics, material degradation concerns, and stringent aerospace performance requirements.
The intended manufacturing processes for these virgin/regrind blends include standard thermoplastic methods such as injection moulding, extrusion, and blow moulding, among others as appropriate to the application.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of screws, 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated.
Classification: 1 100 MPa1/235 °C2.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated.
Classification: 1 250 MPa/425 °C.
- Standard9 pagesEnglish languagee-Library read for1 day
This document is applicable to material testing and specifies the requirements for the tensile testing of metallic materials at ambient temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard28 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel 40CrMoV12 (1.8523)
Consumable electrode remelted
Hardened and tempered
Forgings
De ≤ 50 mm
1 250 MPa ≤ Rm ≤ 1 400 MPa
for aerospace applications.
W.nr: 1.8523.
ASD-STAN designation: FE-PL1507.
- Standard9 pagesEnglish languagee-Library read for1 day
This document is applicable to material testing and specifies the requirements for the tensile testing of metallic materials at ambient temperature for aerospace applications.
It is applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard28 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel 40CrMoV12 (1.8523)
Consumable electrode remelted
Hardened and tempered
Forgings
De ≤ 50 mm
1 250 MPa ≤ Rm ≤ 1 400 MPa
for aerospace applications.
W.nr: 1.8523.
ASD-STAN designation: FE-PL1507.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of a collar, swage locking, shear type, in aluminium alloy 3003, with a maximum operating temperature of 80 °C for aerospace application. This document is applicable in combination with EN 6050, EN 6100 or EN 6120.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of a collar, swage locking, shear type, in aluminium alloy 6061-T7, with a maximum operating temperature of 80 °C for aerospace application.
This document is applicable in combination with EN 6050, EN 6100 or EN 6120.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
Rm ≥ 960 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X4NiCrTiMoV26-15 (1.4680)
Consumable electrode remelted
Not heat treated
Forging stock
a or D ≤ 250 mm
for aerospace applications.
W.nr: 1.4680.
ASD-STAN designation: FE-PA2602.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of self-locking serrated shank nuts in FE-PA2601, for aerospace applications.
Classification: 1 100 MPa /650 °C .
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Not heat treated
Forging stock
a or D ≤ 200 mm
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of close tolerance pins, swage locking, 100° countersunk reduced head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 °C for aerospace application.
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Bars and sections
a or D ≤ 100 mm
Rm ≥ 900 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting (cobalt, nickel and iron-based alloys) alloy plates, sheets and strips. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard31 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy wires. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard32 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy forging stock. It is presupposed to be applied when referred to and in conjunction with the EN material standard 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 pre-production and production forgings in steel and heat-resisting alloys.
- Standard33 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy remelting stock. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard26 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy tubes. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard32 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy bars and sections. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard37 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X4NiCrTiMoV26-15 (1.4680)
Consumable electrode remelted
Not heat treated
Forging stock
a or D ≤ 250 mm
for aerospace applications.
W.nr: 1.4680.
ASD-STAN designation: FE-PA2602.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
Rm ≥ 960 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Not heat treated
Forging stock
a or D ≤ 200 mm
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Bars and sections
a or D ≤ 100 mm
Rm ≥ 900 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu17-4 (1.4542)
Air melted
Solution treated and precipitation treated
Forgings
a or D ≤ 200 mm
Rm ≥ 1 310 MPa
for aerospace applications.
W.nr: 1.4542.
ASD-STAN: FE-PM3801.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Sheets, strips and plates
0,5 ≤ a ≤ 10 mm
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu17-4 (1.4542)
Air melted
Solution treated and precipitation treated
Forgings
a or D ≤ 200 mm
Rm ≥ 930 MPa
for aerospace applications.
W.nr: 1.4542.
ASD-STAN: FE-PM3801.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Softened and cold worked
Wires for forged fasteners
D ≤ 15 mm
900 MPa ≤ Rm ≤ 1 100 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting (cobalt, nickel and iron-based alloys) alloy plates, sheets and strips. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard31 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy remelting stock. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard26 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy tubes. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard32 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy bars and sections. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard37 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of pre-production and production forgings in steel and heat-resisting alloys.
- Standard33 pagesEnglish languagee-Library read for1 day
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat-resisting alloy forging stock. It is presupposed to be applied when referred to and in conjunction with the EN material standard 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 steel and heat-resisting alloy wires. It is presupposed to be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
- Standard32 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu17-4 (1.4542)
Air melted
Softened
Forging stock
a or D ≤ 300 mm
for aerospace applications.
W.nr: 1.4542.
ASD-STAN: FE-PM3801.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel 36NiCrMo16 (1.6773)
1 250 MPa ≤ Rm ≤ 1 400 MPa
Bars
De ≤ 75 mm
for aerospace applications.
W.nr: 1.6773.
ASD-STAN designation: FE-PL2108.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel 31NiMoCr10-5-3
1 230 MPa ≤ Rm ≤ 1 420 MPa
Forgings
De ≤ 40 mm
for aerospace applications.
ASD-STAN designation: FE-PL73.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel 31NiMoCr10-5-3
1 230 MPa ≤ Rm ≤ 1 420 MPa
Bars
De ≤ 40 mm
for aerospace applications.
ASD-STAN designation: FE-PL73.
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu17-4 (1.4542)
Air melted
Solution treated and precipitation treated
Sheets and strips
a ≤ 6 mm
Rm ≥ 930 MPa
for aerospace applications.
W.nr: 1.4542.
ASD-STAN: FE-PM3801.
- Standard8 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy AL-P7010
Forging stock
for aerospace applications.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Steel X5CrNiCu17-4 (1.4542)
Air melted
Solution treated and precipitation treated
Forgings
a or D ≤ 200 mm
Rm ≥ 930 MPa
for aerospace applications.
W.nr: 1.4542.
ASD-STAN: FE-PM3801.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Solution treated and precipitation treated
Sheets, strips and plates
0,5 ≤ a ≤ 10 mm
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.
- Standard9 pagesEnglish languagee-Library read for1 day