49.025.30 - Titanium

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

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.

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.

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

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.

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

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

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

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

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...view more

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.

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.

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.

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  ).

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).

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

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

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.

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.