This document specifies the dimensions of a hose assembly which is in accordance with ISO 7313.
The hose assembly couples to the fittings specified in EN 3274, which are made out of titanium.
The hose is protected either by means of an anti-abrasive, anti-shock and anti-projection sleeve or by means of a fire resistant or fire proof sleeve in accordance with ISO 2685.

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This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Wires for rivets
1,6 mm ≤ D ≤ 10 mm
for aerospace applications.

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This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Bar for machining
a or D ≤ 150 mm
Rm ≥ 390 MPa
for aerospace applications.

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This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Bar for machining
a or D ≤ 150 mm
Rm ≥ 390 MPa
for aerospace applications.

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This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Wires for rivets
1,6 mm ≤ D ≤ 10 mm
for aerospace applications.

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This European standard specifies the characteristics, qualification and acceptance requirements for
bolts with MJ threads in TI-P64001, for aerospace applications.
Strength class: 1 100 MPa1.
It is applicable whenever referenced.

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This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Bar for machining
D ≤ 75 mm
for aerospace applications.

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This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Bar for machining
D ≤ 75 mm
for aerospace applications.

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This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Forgings
De ≤ 75 mm
for aerospace applications.

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This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Forgings
De ≤ 75 mm
for aerospace applications.

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This standard specifies the characteristics of the pipe coupling adapter, 60° spherical sealing face manufactured in titanium alloy with locking ring, for installing in a boss for aerospace applications.
These adapters shall be installed into port connections manufactured in accordance with EN 2602 using ISO 3601-1 sealing O-rings selected sizes. O-ring material depends on the system fluid and operation conditions. The installation shall be performed in accordance with EN 2608.
Nominal working pressure: up to 28000 kPa.
Temperature range: limited by elastomeric sealing ring, −54 °C to +135 °C

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This document specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium
alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa.
Temperature range: −55 °C to 135 °C.

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This European Standard specifies the requirements relating to:
Titanium TI-P99002
Not heat treated
Grade 2 forging stock, for annealed forgings
a or D ≤ 300 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Titanium TI-P99002
Not heat treated
Grade 2 forging stock, for annealed forgings
a or D  300 mm
for aerospace applications.

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This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa  ) / 315 °C  ).

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This standard specifies the characteristics of screws, 100° countersunk normal head, offset cruciform
recess, close tolerance shank, short thread, in titanium alloy, aluminium IVD coated.
Classification: 1 100 MPa1) / 425 °C2).

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This European Standard specifies the characteristics of equipped blind ferrules for pipe couplings 8°30’, in
titanium alloy, for aerospace applications.

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This European Standard specifies the characteristics of pressure plugs for pipe couplings 8°30’, in titanium
alloy, for aerospace applications.

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This standard specifies the characteristics of elbows 45°, for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa. Temperature range: – 55 °C to 135 °C.

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This European Standard specifies the specific rules for the drafting and presentation of titanium and titanium alloy material standards for aerospace applications. It should be used in conjunction with EN 4500-001.

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This European Standard specifies the requirements relating to: 1) Titanium alloy Ti-4Al-4Mo-2Sn Solution treated and aged Forgings De ≤ 150 mm for aerospace applications. NOTE Other common designation: Ti550, AECMA: TI-P63, ASD-STAN: TI-P63001.

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This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications. It comprises a series of sheets, by materials or by material family, which: - indicate the main titles, the typical chemical composition and the main characteristics, - contain recommendations for welding and brazing, - indicate a degree of weldability or brazeability for a given process under defined conditions. It is applicable without restriction for the manufacturing of new parts or for repair.

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This standard specifies the requirements relating to: Titanium alloy Ti-6Al-4V Annealed Bar and wire for forged fasteners De ≤ 50 mm for aerospace applications.

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This European Standard specifies the requirements relating to: Titanium alloy Ti-6Al-4V Annealed Sheet for superplastic forming a ≤ 6 mm for aerospace applications.

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This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Sheet for superplastic forming
a  6 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Bar and wire for forged fasteners
De £ 50 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:  )
Titanium alloy Ti-4Al-4Mo-2Sn
Solution treated and aged
Forgings
De < or = 150 mm
for aerospace application.
NOTE   Other designation: WL: 3.7184   
   Only the chemical composition of this standard must be considered.

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This European Standard specifies the specific rules for the drafting and presentation of titanium and titanium alloy material standards for aerospace applications.
It should be used in conjunction with EN 4500-001.

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This European Standard specifies the requirements relating to: Titanium alloy Ti-6Al-4V Annealed Plate 6 mm < a ≤ 100 mm for aerospace applications.

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This European Standard specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet and strip, hot rolled a ≤ 6 mm for aerospace applications.

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This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Plate
6 mm < a ≤ 100 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Sheet and strip, hot rolled
a ≤ 6 mm

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This European Standard specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Extruded section De ≤ 150 mm 900 MPa ≤ Rm ≤ 1 160 MPa.

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This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Forgings
De < (+/-) 150 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Titanium alloy TI-P64003
Cold worked and stress relieved
Seamless tube for pressure systems
4 mm £ D £ 51 mm
690 MPa £ Rm £ 1 030 MPa
for aerospace applications.

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This European Standard specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Extruded section
De < (+/-) 150 mm
900 MPa < (+/-) Rm < (+/-) 1 160 MPa
for aerospace applications.

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    8 pages
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This European Standard specifies the requirements relating to:
Titanium alloy Ti-6Al-4V
Annealed
Forgings
De < (+/-) 150 mm
for aerospace applications.

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    9 pages
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This European Standard specifies the requirements relating to:
Titanium alloy TI-P64003
Cold worked and stress relieved
Seamless tube for pressure systems
4 mm £ D £ 51 mm
690 MPa £ Rm £ 1 030 MPa
for aerospace applications.

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This European Standard specifies the requirements relating to: )
Titanium alloy TI P64001 (Ti 6Al 4V)
Not heat treated
Forging stock, for annealed forgings
De  360 mm
for aerospace applications.

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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy wire. 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 European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy pre-production and production forgings. 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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    26 pages
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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy forging stock. 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 European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy remelting stock. 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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    22 pages
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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy tube. 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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    28 pages
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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy pre-production and production castings. 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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    22 pages
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This European Standard specifies the requirements relating to: )
Titanium alloy TI P64001 (Ti 6Al 4V)
Not heat treated
Forging stock, for annealed forgings
De  360 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0,4Fe)
Rm >or= 1 300 MPa
Bars
De for aerospace applications.

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    8 pages
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This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of
titanium and titanium alloy bar and section. 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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    27 pages
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This standard specifies the requirements relating to:
Titanium Ti10V2Fe3Al
Bars
D < 110 mm
Rm >or= 1 240 MPa
for aerospace applications.

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    7 pages
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