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

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

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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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    9 pages
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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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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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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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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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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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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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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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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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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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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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    11 pages
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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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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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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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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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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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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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    9 pages
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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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    34 pages
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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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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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