Aircraft Quality tubing

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15CDV6 Aero

25CD4S Aero

35CD4 Aero
Généralités

Seamless cold drawn tubes

15CDV6 Aerospace quality
• Cleanliness Class 2 / AIR 0819
• Chemical composition WL W.-Nr. 1.7734
• Manufactured acc. ASNA 3114 - ASNA 3108 - ASNA 6078 - ASNA 6079 - AIR 9160
Werkstoff WL 1.7734/3/4/5 - Dassault C.R. 1.3.0.26
• OASIS Identification : 6127818124
• AS 9100 / EN9100 / JISQ 9100 N° 00017787
Approuved by Airbus, Airbus Helicopters, Safran Helicopter Engines
• Airbus ARP-ID 161592
• Airbus Helicopters : autorization L030 03-002
• Safran Helicopter Engines : Supplier code 2000789

Seamless cold drawn tubes

25CD4S Aerospace quality
• Cleanliness Class 2 / AIR 0819 & BS S100
• Chemical composition WL W.-Nr.1.7214
• Manufactured acc. ASNA 6080 - AIR 9160 - British Standard Aerospace T60/T77 - Werkstoff WL 1.7214-5/6/7

• OASIS Identification : 6127818124
• AS 9100 / EN9100 / JISQ 9100 N° 00017787
Approuved by Airbus, BAE Systems
• Airbus ARP-ID 161592
• BAE : autorization N° ACO/O/LT/JJH/5940

Seamless cold drawn tubes

35CD4 Aerospace quality
• Cleanliness Class 2 / AIR 0819
• Chemical composition WL W.-Nr. 1.7220/1.2330
• Manufactured acc. ASNA 3115- ASNA 3116 - AIR 9160

• OASIS Identification : 6127818124
• AS 9100 / EN9100 / JISQ 9100 N° 00017787
Approuved by Airbus, Airbus Helicopters
• Airbus ARP-ID 161592
• Airbus Helicopters : autorization L030 03-002

Caractéristiques Mécaniques
Annealed condition:
Hardness ≤ 87 HRb
Rm ≤ 610 Mpa


Condition TR700:
Hardness ≥ 222 HV
Rm ≥ 700MPa
Rp0,2% ≥ 550 Mpa
A% ≥ 12%
Condition TR880:
Hardness ≥ 94 HRb
880 MPa ≤ Rm ≤ 1080 Mpa
Rp0,2% ≥ 680 Mpa
A% ≥ 12%
Condition TR980:
Hardness ≥ 29 HRc
980MPa ≤ Rm ≤ 1180MPa
Rp0,2% ≥ 790 Mpa
A% ≥ 10%
Condition TR1080:
Hardness ≥ 33 HRc
1080MPa ≤ Rm ≤ 1280MPa
Rp0,2% ≥ 930 MPa
A% ≥ 10%
Annealed condition:
Hardness ≤ 95 HRb
Rm ≤ 740 Mpa


Condition Normalized:
190 HB ≤ Hardness ≤ 250 HB
660MPa ≤ Rm ≤ 860MPa
Rp0,2% ≥ 490 Mpa (520 Mpa for WL)
A% ≥ 15%
Condition TR880:
267 HV ≤ Hardness ≤ 324 HV
880 MPa ≤ Rm ≤ 1080 Mpa
Rp0,2% ≥ 690 Mpa
A% ≥ 10%
Condition TR1080:
Hardness ≥ 320 HV
1080 MPa ≤ Rm ≤ 1250 Mpa
Rp0,2% ≥ 885 Mpa
A% ≥ 7%
Condition TR1150:
350 HV ≤ Hardness ≤ 425 HV
1150 MPa ≤ Rm ≤ 1350 MPa
Rp0,2% ≥ 1050 MPa
A% ≥ 6%
Annealed condition:
Hardness ≤ 96 HRb
Rm ≤ 750 Mpa


Condition TR1080:
Hardness ≥ 33 HRc
1080MPa ≤ Rm ≤ 1200MPa
960 MPa ≤ Rp0,2% ≤ 1120 MPa
A% ≥ 12%
Condition TR1350:
Hardness ≥ 410 HV
1350 MPa ≤ Rm ≤ 1450 Mpa
1230 MPa ≤ Rp0,2% ≤ 1350 MPa
A% ≥ 8%
Lien(s) Utile(s) PDF sheet
Aerospace applications
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Aerospace applications
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Aerospace applications