ALUMINIUM ALLOY SHEET

Alloy
Specification
Temper
Country
1200 L16/17
 
H4/O
 
UK
 
2014 AIR 9048.010/.030/.020/.040/.050
 
F(T42)/F(T62)/ T4/T6/T451
 
France
 
2014 clad
 
AMS QQ-A-250/3
 
O, T4, T6
 
USA
 
  AIR 9048.060/.080/.070/.090
 
F(T42)/F(T62)/T4/T6
 
France
 
2014A
 
EN 2089/2395
 
T6(T62)/T4(T42)
 
Europe
 
  3.1254 T4, T6
 
Germany
 
  L156/157/158*/159*
 
T4/T6/T4/T6
 
UK
 
2014A clad
 
EN 2087/2088
 
T6(T62)/T4(T42)
 
Europe
 
  L163/164/165
 
T3/F(T42), T4/T6
 
UK
 
  L166*/167*
 
F(T42), T4/T6
 
UK
 
2024 AMS QQ-A-250/4
 
O, T3
 
USA
 
  AMS 4037
 
T3
 
USA
 
  EN 4101
 
T4 forming quality
 
Europe
 
  AIR 9048.100/.110/.120
 
F(T42)/T3/T351
 
France
 
  ASNA 3010
 
T3
 
France
 
  3.1354 O(T42), T3
 
Germany
 
2024 clad
 
AMS QQ-A-250/5
 
O, T3
 
USA
 
  AMS 4041
 
T3
 
USA
 
  AIR 9048.130/.140
 
F(T42)/T3
 
France
 
  ASNA 3012
 
T3
 
France
 
  3.1364 O(T42), T3
 
Germany
 
  L109/110
 
T3/F(T42)
 
UK
 
2024 clad cmq
 
EN 2090/2091/2703/4001
 
T3/T4/T4(T42)/T351
 
Europe
 
2024 cmq
 
EN 3474/3997/3998/3999
 
T81/T3/T4(T42)/T351
 
Europe
 
2219 AMS QQ-A-250/30
 
O(T62), T31(T81), T37(T87)
 
USA
 
2524 BAMS 516-015
 
O, T3
 
USA
 
  CMMP008
 
T3
 
USA
 
2618A
 
AIR 9048.150
 
H28(T62)
 
France
 
2618A clad
 
AIR 9048.170
 
H28(T62)
 
France
 
  DTD DTD5070
 
T6
 
UK
 
3003 AMS QQ-A-250/2
 
O, H14
 
USA
 
3103 L59/60/61
 
H6/H2/O
 
UK
 
5086 AIR 9048.190/.200
 
O, H111/H22, H32
 
France
 
  ASNA 3044
 
H111
 
France
 
5251 L80/81
 
O/H6
 
UK
 
6013 CMMP018
 
T4, T6
 
USA
 
  AMS 4347
 
T4
 
USA
 
  AMS 4216
 
T6
 
USA
 
6061 AMS QQ-A-250/11
 
O, T4, T6
 
USA
 
  EN 2694/EN  3341
 
T6(T62)/T4(T42)
 
Europe
 
  AIR 9048.210/.220/.230/.240
 
O, H111(T42)/T4/ O, H111(T62)/T6
 
France
 
  3.3214 O(T62), T6
 
Germany
 
6082 L113
 
T4, T6
 
UK
 
7050 EN 4449/4450
 
T76/F(T762)
 
Europe
 
7075 AMS QQ-A-250/12
 
O, T6, T73
 
USA
 
  AMS QQ-A-250/24
 
T76
 
USA
 
  EN 2696
 
T6(T62)
 
Europe
 
  AIR 9048.260/.270
 
T6/T76
 
France
 
  3.4364 T6
 
Germany
 
7075 clad
 
AMS QQ-A-250/13
 
O, T6, T73
 
USA
 
  EN 2092
 
T6(T62)
 
Europe
 
  AIR 9048.280
 
T6
 
France
 
  3.4374 O(T62), T6
 
Germany
 
  L88
 
T6
 
UK
 
7075 clad with 7011
 
AMS QQ-A-250/26
 
T76
 
USA
 
7075 clad with 7072
 
AMS QQ-A-250/25
 
T76
 
USA
 
7475 EN 2802/3333
 
T761/F(T762)
 
Europe
 
  AIR 9048.290
 
T76
 
France
 
  DMS 2281
 
O, T761
 
USA
 
7475 clad
 
EN 2803/3332
 
T761/F(T762)
 
Europe
 
  3.4377 T76
 
Germany
 
  DMS 2234
 
O, T761
 
USA
 
7475 SPF
 
EN 3335
 
O
 
Europe
 


COUNTRY SPECIFICATION ALLOY TEMPER
       
EUROPE EN 2087/2088 2014A clad T6(T62)/T4(T42)
(AECMA) EN 2089/2395 2014A T6(T62)/T4(T42)
  EN 2090/2091/2703/4001 2024 clad cmq T3/T4/T4(T42)/T351
  EN 3474/3997/3998/3999 2024 cmq T81/T3/T4(T42)/T351
  EN 4101 2024 T4 forming quality
  EN 2694/EN 3341 6061 T6(T62)/T4(T42)
  EN 2092 7075 clad T6(T62)
  EN 2696 7075 T6(T62)
  EN 2802/3333 7475 T761/F(T762)
  EN 2803/3332 7475 clad T761/F(T762)
  EN 3335 7475 SPF O
  EN 4449/4450 7050 T76/F(T762)
FRANCE AIR 9048.010/.030/ 2014 F(T42)/F(T62)/
(AIR) .020/.040/.050 2014 T4/T6/T451
  AIR 9048.060/.080/ 2014 clad F(T42)/F(T62)/
  .070/.090 2014 clad T4/T6
  AIR 9048.100/.110/.120 2024 F(T42)/T3/T351
  AIR 9048.130/.140 2024 clad F(T42)/T3
  AIR 9048.150 2618A H28(T62)
  AIR 9048.170 2618A clad H28(T62)
  AIR 9048.190/.200 5086 O, H111/H22, H32
  AIR 9048.210/.220/ 6061 O, H111(T42)/T4/
  .230/.240 6061 O, H111(T62)/T6
  AIR 9048.260/.270 7075 T6/T76
  AIR 9048.280 7075 clad T6
  AIR 9048.290 7475 T76
GERMANY 3.1254 2014A T4, T6
(Werkstoff) 3.1354 2024 O(T42), T3
  3.1364 2024 clad O(T42), T3
  3.3214 6061 O(T62), T6
  3.4364 7075 T6
  3.4374 7075 clad O(T62), T6
  3.4377 7475 clad T76
UK L16/17 1200 H4/O
(BS) L59/60/61 3103 H6/H2/O
  L80/81 5251 O/H6
  L88 7075 clad T6
  L109/110 2024 clad T3/F(T42)
  L113 6082 T4, T6
  L156/157/158*/159* 2014A T4/T6/T4/T6
  L163/164/165 2014A clad T3/F(T42), T4/T6
  L166*/167* 2014A clad F(T42), T4/T6
  DTD DTD5070 2618A clad T6
USA AMS QQ-A-250/2 3003 O, H14
(AMS) AMS QQ-A-250/3 2014 clad O, T4, T6
  AMS QQ-A-250/4 2024 O, T3
  AMS QQ-A-250/5 2024 clad O, T3
  AMS QQ-A-250/11 6061 O, T4, T6
  AMS QQ-A-250/12 7075 O, T6
  AMS QQ-A-250/13 7075 clad O, T6
  AMS QQ-A-250/24 7075 T76
  AMS QQ-A-250/25 7075 clad with 7072 T76
  AMS QQ-A-250/26 7075 clad with 7011 T76
  AMS QQ-A-250/30 2219 O(T62), T31 (T81), T37 (T87)






































































COMPANY SPECIFICATION ALLOY TEMPER
       
AIRBUS FRANCE 04.32.170 5086 O, H111
  04.32.210 2024 O(T4), T3
  04.32.211 2024 clad O(T4), T3
  04.32.261 7075 clad O(T6), T4(T6), T6
  ASN-A-3001/3046/3047 6061 O/T4/T6
  ASN-A-3010/3045/3362/3373 2024 T3/T42/T351/T3
  ASN-A-3012/3042/3374 2024 clad T3/T42/T3
  ASN-A-3043 2618A T62
  ASN-A-3044 5056 O, H111
  ASN-A-3051 7075 clad T6
  ASN-A-3397 7475 SPF O
  ASN-A-3399 5083 SPF O
AIRBUS AIMS 03-04-009/013*/022*HDT 2024 clad cmq T351
  AIMS 03-04-010/012*/023*HDT/ 2024 clad O, F(T42)
  035**/37* ** 2024 clad O, F(T42)
  AIMS 03-04-011*/014/031*HDT 2024 clad T3
  AIMS 03-04-016* 5083 SPF F, O
  AIMS 03-04-019* 7475 SPF T4(T762)
  AIMS 03-04-024** 2024 clad T4
  AIMS 03-04-027* 6056 T78
  AIMS 03-04-029* 7475 clad cmq T761
  AIMS 03-04-030* 7475 clad O(T762)
  AIMS 03-04-033 7449 cmq T7651
  AIMS 03-04-034* 6013/6056 clad cmq T4(T62)
  AIMS 03-04-036 2618A clad H28(T62)
  AIMS 03-04-038 2024 T3
  AIMS 03-04-040*HDT 6013/6156 T4(T62)
  AIMS 03-04-041* 2219 cmq T31(T81)
  AIMS 03-04-042 6061 O(T62), T4(T62)
  AIMS 03-04-045 7475 T761
  AIMS 03-04-047 5086 H111
AIRBUS UK & BAEM 0003/0004 2024 clad T3/T4
BAE SYSTEMS – CIVIL BAEM 0120/ABM2-6027 6061 T4(T42)
  BAEM 0133/ABM2-6028 6061 T4(T62)
  BAEM 0155/0196/0197 2014A clad F(T62)/F(T42)/OO(T42)(T62)
  BAEM 0163/0164 2024 clad T3/T4
  BAEM 0194/0195/1005/1006 2014A F(T42)/OO(T42)(T62)/T4/T6
  BAEM 1007/ABM1-7018*** 2014A clad T4
  BAEM 1008/ABM1-7019*** 2014A clad T6
  BAEM 1009/ABM1-7067*** 2024 clad T3
  BAEM 1010/ABM1-7068*** 2024 clad O(T42)
  BAEM 1020/ABM1-6013*** 2014A T4
  BAEM 1021/ABM1-6014*** 2014A T6
  BAEM 1029/ABM1-6015 2024 T3
  BAEM 4001/ABM3-7045 7050 clad T76
  BAEM 4049 2618A clad F(T62)
BAE SYSTEMS – 2014A F(T42),T4  
MILITARY MM 0550/S07-1006 2014A T6
  MM 0551/S07-1007 2014A clad T4
  MM 0552/S07-1008 2014A clad T6
  MM 0553/S07-1020 2014A T4
  MM 0554/S07-1021 2014A T6
DASSAULT CR 1.1.0.7 2024 F(T42), T3
  CR 1.1.0.8 2024 clad F(T42), T3
  CR 1.1.0.13 2014 F(T42), T4(T4, T6)
  CR 1.1.0.18 5754 O, H111
  CR 1.1.0.26 2017A F(T42), T3
  CR 1.1.0.48/60 2014 clad T6/F(T42), T4(T4, T6)
  CR 1.1.0.56 5086 O, H111
  CR 1.1.0.61 6061 O(T42), T4, T6
EMBRAER MEP 02-012**** 7475 bare/clad O(T761)
  MEP 02-015**** 2024 clad O(T42), T3(T42,T81), T4(T42)



























































































Inspection & Approval Certificates : C/W Certificate (Calibration Works Certificate) EN10204 3.1 / DIN 50049 3.1 / ISO 10474 3.1 Mill Test Certificate, NACE MR-0103 / NACE MR-0175 / ISO 15156, CE Marked, European Pressure Equipment Directive PED-97/23/EC, AD-2000-WO, ASME Boiler & Pressure Vessel Code Sec.II Part A Ed. 2008, API 6A (American Petroleum Institute), with 3.2 certificate duly Certified & Approved by LRS (Lloyd's Register), GL (Germanischer Lloyd), BV (Bureau Veritas), DNV (Det Norske Veritas), ABS (American Bureau of Shipping), SGS, TUV, RINA, IRS, NORSOK Approved Standard M-630, M-650 Rev.3, NADCAP Certified in accordance with SAE Aerospace Standards


If you have any requirement of above items, please feel free to contact us


Regards,


CONTACT PERSON :


MUKESH SHAH
Director
MOBILE No. 0091- 9820292499
Email :
rolexmetal@vsnl.net

ROLEX ALLOYS INTERNATIONAL
( High Nickel Alloy & Super Alloy Materials )
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