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49.025.10 - Steels

ICS 49.025.10 Details

Steels

Stahle

Acier

Jekla

General Information

Parent
49.025 - Materials for aerospace construction

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Standardization Organization
Technical Committee
Directive
Mandate
50
SIST
SIST EN 4877-001:2024(Main)
Aerospace series - Filler metals for welding - Part 001: Technical specification
EN 4877-001:2024

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.

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EN 4877-001:2024(Main)
Aerospace series - Filler metals for welding - Part 001: Technical specification
SIST EN 4877-001:2024

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.

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SIST
SIST EN 3524:2024(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm ≤ a ≤ 6 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa
EN 3524:2023

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.

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SIST EN 3525:2024(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Plates - 6 mm ≤ a ≤ 20 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa
EN 3525:2023

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.

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SIST EN 3526:2024(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 0,5 mm ≤ a ≤ 6 mm - 980 MPa ≤ Rm ≤ 1 180 MPa
EN 3526:2023

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.

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SIST
SIST EN 2516:2024(Main)
Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel or cobalt base alloys
EN 2516:2023

This document specifies several chemical methods of passivation for corrosion resisting steels (austenitic, ferritic, martensitic and precipitation hardenable) and of decontamination for nickel or cobalt base alloys.

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EN 3525:2023(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Plates - 6 mm ≤ a ≤ 20 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa
SIST EN 3525:2024

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.

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EN 3526:2023(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 0,5 mm ≤ a ≤ 6 mm - 980 MPa ≤ Rm ≤ 1 180 MPa
SIST EN 3526:2024

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.

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EN 3524:2023(Main)
Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm ≤ a ≤ 6 mm - 1 080 MPa ≤ Rm ≤ 1 280 MPa
SIST EN 3524:2024

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.

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SIST
SIST EN 3628:2023(Main)
Aerospace series - Lockwire, drawn - Corrosion resisting steel
EN 3628:2023

This document specifies the dimensions and tolerances for drawn corrosion resisting steel lockwire for aerospace applications.

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SIST
SIST EN 4842:2023(Main)
Aerospace series - 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)
EN 4842:2023

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.

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EN 3628:2023(Main)
Aerospace series - Lockwire, drawn - Corrosion resisting steel
SIST EN 3628:2023

This document specifies the dimensions and tolerances for drawn corrosion resisting steel lockwire for aerospace applications.

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SIST
SIST EN 2886:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 2886:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, close tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/ 235 °C2.

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SIST EN 2885:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 2885:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/235 °C2.

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SIST
SIST EN 2003-2:2023(Main)
Aerospace series - Steels - Test methods - Part 2: Izod impact test
EN 2003-002:2023

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.

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EN 2003-002:2023(Main)
Aerospace series - Steels - Test methods - Part 002: Izod impact test
SIST EN 2003-2:2023

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.

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SIST EN 4904:2023(Main)
Aerospace series - Steel 36NiCrMo16 (1.6773) - 1 000 MPa ≤ Rm ≤ 1 200 MPa - Bars - 100 mm ≤ D ≤ 250 mm
EN 4904:2022

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.

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SIST EN 3479:2023(Main)
Aerospace series - 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
EN 3479:2022

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.

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SIST EN 4628:2023(Main)
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bars - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa
EN 4628:2022

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.

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SIST EN 3364:2023(Main)
Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted, softened - Forging stocks - a or D ≤ 300 mm
EN 3364:2022

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.

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SIST
SIST EN 3434:2023(Main)
Aerospace series - Nuts, hexagon, slotted/castellated, self-locking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 3434:2022

This standard specifies characteristics of self-locking hexagonal slotted/castellated nuts, in steel, cadmium plated, MoS2 lubricated, for aerospace applications.
Classification: 900 MPa /235 °C .

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SIST EN 4884:2023(Main)
Aerospace series - Steel X3CrNiMoAl (1.4534) - 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
EN 4884:2022

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.

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SIST EN 4627:2023(Main)
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa
EN 4627:2022

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.

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SIST EN 4883:2023(Main)
Aerospace series - Steel X5CrNiCu 17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Plates - 6 mm ≤ a ≤ 100 mm - Rm ≥ 1 070 MPa
EN 4883:2022

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.
W.nr: 1.4542.
The ASD-STAN designation of this material is FE-PM3801.

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SIST EN 4882:2023(Main)
Aerospace series - Steel X5CrNiCu 17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Sheets and strips - a ≤ 6 mm - Rm ≥ 1 070 MPa
EN 4882:2022

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.
W.nr: 1.4542.
The ASD-STAN designation of this material is FE-PM3801.

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CEN
EN 4904:2022(Main)
Aerospace series - Steel 36NiCrMo16 (1.6773) - 1 000 MPa ≤ Rm ≤ 1 200 MPa - Bars - 100 mm ≤ D ≤ 250 mm
SIST EN 4904:2023

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.

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EN 4883:2022(Main)
Aerospace series - Steel X5CrNiCu 17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Plates - 6 mm ≤ a ≤ 100 mm - Rm ≥ 1 070 MPa
SIST EN 4883:2023

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.

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EN 4628:2022(Main)
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bars - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa
SIST EN 4628:2023

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.

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EN 4882:2022(Main)
Aerospace series - Steel X5CrNiCu 17-4 (1.4542) - Air melted - Solution treated and precipitation treated - Sheets and strips - a ≤ 6 mm - Rm ≥ 1 070 MPa
SIST EN 4882:2023

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.

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CEN
EN 4884:2022(Main)
Aerospace series - Steel X3CrNiMoAl (1.4534) - 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
SIST EN 4884:2023

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.

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CEN
EN 3479:2022(Main)
Aerospace series - 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
SIST EN 3479:2023

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.

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CEN
EN 4627:2022(Main)
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Forgings - De ≤ 200 mm - 1 150 MPa ≤ Rm ≤ 1 300 MPa
SIST EN 4627:2023

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.

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EN 3364:2022(Main)
Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted, softened - Forging stocks - a or D ≤ 300 mm
SIST EN 3364:2023

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.

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CEN
EN 4890:2022(Main)
Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered - Sheets and plates - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
SIST EN 4890:2022

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.

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SIST
SIST EN 2573:2022(Main)
Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Wires - 0,25 mm ≤ De ≤ 3 mm - Rm ≤ 780 MPa
EN 2573:2022

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 application.
W.nr: 1.4541.
ASD-STAN designation: FE-PA3601.

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EN 2573:2022(Main)
Aerospace series - Steel X6CrNiTi18-10 (1.4541) - Air melted - Softened - Wires - 0,25 mm ≤ De ≤ 3 mm - Rm ≤ 780 MPa
SIST EN 2573:2022

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.

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SIST EN 2287:2022(Main)
Aerospace series - Bush, plain, in corrosion resisting steel with self-lubricating liner - Dimensions and loads
EN 2287:2022

This European Standard specifies the characteristics of plain bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 C to 163 C and assembly with an interference fit into fixed and moving aerospace parts.

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SIST EN 4890:2022(Main)
Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered - Sheets and plates - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
EN 4890:2022

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

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SIST EN 3228:2022(Main)
Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 3228:2022

This document specifies the characteristics of plain hexagonal nuts, reduced height, normal across flats,
in steel, cadmium plated, for aerospace applications.
Classification: 900 MPa/235 °C1.

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SIST
SIST EN 4850:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4850:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated, for aerospace applications.
Classification: 1 100 MPa /235 °C .

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SIST EN 4847:2022(Main)
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4847:2022

This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive
Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated, for
aerospace applications.
Classification: 1 100 MPa1/235 °C2.

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SIST EN 4844:2022(Main)
Aerospace series - Screws, 100° countersunk normal head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
EN 4844:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal
head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated, for
aerospace applications.

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SIST EN 4845:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, short thread, in heat resisting steel FE-PA2601 (A286), passivated - Classification: 900 MPa (at ambient temperature)/650 °C
EN 4845:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal
head, Spiral Drive Recess, short thread, in heat resisting steel FE-PA2601, passivated, for aerospace
applications.
Classification: 900 MPa
1/650 °C2.

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SIST EN 4851:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4851:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated, for aerospace applications.
Classification: 1 100 MPa /235 °C .

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SIST
SIST EN 4846:2022(Main)
Aerospace series - Screws, pan head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
EN 4846:2022

This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive
Recess, threaded to head, in heat and corrosion resisting steel, passivated, for aerospace applications.
Classification: 1 100 MPa1/425 °C2.

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CEN
EN 4700-002:2021(Main)
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bars and sections
SIST EN 4700-002:2021

This document defines the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy bars and sections. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

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CEN
EN 4825:2021(Main)
Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 100 MPa
SIST EN 4825:2021

This document specifies the requirements relating to:
Steel X12CrNiMoV12-3 (1.4938)
Air melted and consumable electrode remelted
Hardened and tempered
Bars
De ≤ 150 mm
900 MPa ≤ Rm ≤ 1 100 MPa
for aerospace applications.

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SIST
SIST EN 4700-002:2021(Main)
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section
EN 4700-002:2021

This document defines the requirements for the ordering, manufacture, testing, inspection and delivery of steel and heat resisting alloy bars and sections. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

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SIST
SIST EN 4825:2021(Main)
Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 100 MPa
EN 4825:2021

This document specifies the requirements relating to:
Steel X12CrNiMoV12-3 (1.4938)
Air melted and consumable electrode remelted
Hardened and tempered
Bars
De ≤ 150 mm
900 MPa ≤ Rm ≤ 1 100 MPa
for aerospace applications.

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SIST
SIST EN 6057:2021(Main)
Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series
EN 6057:2020

This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265)
- a rod end with internal threaded shank
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.

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