49.025.05 - Ferrous alloys in general

This document specifies the requirements relating to:
Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13)
As forged
Forging stock
a or D ≤ 200 mm
for aerospace applications.

This document is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258.
This document has been prepared in accordance with EN 4500-003.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Bars and sections
De ≤ 100 mm

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21)
Solution treated and precipitation treated
Forgings
De  100 mm
for aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCOMoW21-20)
Solution treated and descaled
Sheet and plate
3 mm < a ≤ 50 mm
for aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
for aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Sheets and strips
a ≤ 3 mm
for aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

This document specifies the requirements relating to:
Heat resisting alloy X4NiCrMoTi43-13
As forged
Forging stock
a or D ≤ 200 mm
for aerospace applications.
ASD-STAN designation: FE-PA2501.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCOMoW21-20
Solution treated and descaled
Sheets and plates
3 mm < a ≤ 50 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Sheets and strips
a ≤ 3 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Bars and sections
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated and precipitation treated
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 Softened and cold worked Bar for forged fasteners D ≤ 50 mm 1 100 MPa ≤ Rm ≤ 1 300 MPafor aerospace applications.

This document specifies the requirements relating to:
Heat resisting alloy FE-PA2601
Softened and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 100 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.

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.

This document specifies the requirements for the radiographic inspection 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 inspection schedule.

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.