ALUMINIUM ALLOY PLATE
Alloy |
Specification |
Temper |
Company |
Country |
2014 |
AMS 4028/4029 |
O/T651 |
|
USA |
|
MMS 1580 |
T651 |
Boeing |
USA |
2014A |
L93 |
T651, T351 |
|
UK |
|
BAEM 0039/0128/0173 |
T351 (T651)/ T351 (T651)/T351 |
|
UK |
|
DTD 5010 |
T351 |
|
UK |
2024 |
EN 2419 |
T351 |
|
Europe |
|
EN 6000 |
T351 |
|
Europe |
|
ABS 5032 |
T351 |
|
Europe |
|
04-32-411 |
T351 |
Airbus |
France |
|
CR 1.1.0.36 |
T351 |
Dassault |
France |
|
ASN-A-3011 |
T351 |
Airbus |
France |
|
AIR 9048.630 |
T351 |
|
France |
|
AIMS 03-02-004/020 |
T351/T351HDT |
Airbus |
France |
|
3.1354 |
T351, T851 |
|
Germany |
|
ABM1-1005/BAEM 0172 |
T351 |
Airbus |
UK |
|
BAEM 0145 |
T651, T851 |
|
UK |
|
L97 |
T351 |
|
UK |
|
AMS 4035/4037 |
O/T351 |
|
USA |
|
AMS QQ-A-250/4 |
O, T351, T851 |
Boeing |
USA |
2027 |
AIMS 03-02-031 |
T351 |
Airbus |
France |
2124 |
EN 2422 |
T351 |
|
Europe |
|
AIMS 03-02-032 |
T851 |
Airbus |
France |
|
AMS 4101 |
T851 |
|
USA |
|
AMS QQ-A-250/29 |
T351, T851 |
|
USA |
|
DMS 2116 |
T851 |
Boeing |
USA |
|
MMS 149 |
T351, T851 |
Boeing |
USA |
|
FMS 3002/8 |
T851 |
Lockheed |
|
2214 |
EN 2124 |
T451, T651 |
|
Europe |
|
AIR 9048.610/.620 |
T451/T451 (T651), T651 |
|
France |
|
CR 1.1.0.31 |
T451, T651 |
Dassault |
France |
|
04-32-232 |
T351, T651 |
Airbus |
France |
2219 |
AMS QQ-A-250/30 |
O, T351, T37, T87, T851 |
|
USA |
2618A |
EN 2123 |
T351, T851 |
|
Europe |
|
ABM1-1006/BAEM 1103 |
T351, T651 |
|
Europe |
|
04-32-441 |
T351, T851 |
Airbus |
France |
|
AIMS 03-02-021 |
T851 |
Airbus |
France |
|
ASN-A-3355 |
T851 |
Airbus |
France |
|
AIR 9048.640 |
T351(T851), T851 |
|
France |
|
CR 1.1.0.42 |
T351, T651 |
Dassault |
France |
|
3.1924 |
T651 |
|
Germany |
|
BAEM 1101 |
T351 (T651) |
|
UK |
|
MSRR 8016 |
T651 |
Rolls-Royce |
|
|
MM 0531 |
T351, T651 |
BAE Systems |
|
6061 |
EN 4213 |
T651 |
|
Europe |
|
3.3214 |
T451, T651 |
|
Germany |
|
AMS 4025/4026/4027 |
O/T451/T651 |
|
USA |
|
AMS QQ-A-250/11 |
O, F, T451, T651 |
|
USA |
6082 |
L115 |
T651 |
|
UK |
7010 |
EN 2684/2687 |
W51, T7651, T7451 |
|
Europe |
|
ABM3-1029/1030 |
W51, T7651 |
|
Europe |
|
ABM3-1029/BAEM 1213 |
W51, T7651 |
|
Europe |
|
ABM3-1030/BAEM 1218 |
W51, T7651 |
|
Europe |
|
EN 4214 |
T651 |
|
Europe |
|
04-32-311/319/324 |
T7451/T651/T7651 |
Airbus |
France |
|
ASN-A-3005/3098/3101 |
T651/T7451/T7651 |
Airbus |
France |
|
CR 1.1.0.87 |
T7451 |
Dassault |
France |
|
3.4394 |
T7451 |
|
Germany |
|
BAEM 1211 |
T7351 |
|
UK |
|
BAEM 0200 |
W51, T7651 |
|
UK |
|
DTD 5120 |
T7651 |
|
UK |
|
DTD 5130 |
T7451 |
|
UK |
|
AMS 4203/4204/4205 |
T7351/T7651/T7451 |
|
USA |
|
MM 0533 |
W51, T7351 |
BAE Systems |
|
|
SMS 3206 |
T7451 |
Sonaca |
|
7010/7050 |
AIMS 03-02-022 |
T7451 |
Airbus |
France |
7040 |
AIMS 03-02-023 |
T7651 |
Airbus |
France |
7040/7050 |
AIMS 03-02-019 |
T7451 |
Airbus |
France |
7050 |
EN 3982/3983 |
T7451/T7651 |
|
Europe |
|
ABM3 1029 |
T7651 |
|
Europe |
|
ABM3 1030 |
T7651 |
|
Europe |
|
ABS 5323 |
T7451 |
|
Europe |
|
AIR 9048.74 |
T7451 |
|
France |
|
CR 1.1.0.98 |
T7451 |
Dassault |
France |
|
3.4144 |
T7451 |
|
Germany |
|
AMS 4050/4201 |
T7451/T7651 |
|
USA |
|
BMAS/CMS 516-01 |
T7651 |
Bombardier |
USA |
|
BAMS 516-03 |
T7451 |
Bombardier |
USA |
|
BMS 7-323 types I & III |
T7451 |
Boeing |
USA |
|
DMS 2233 |
W51, T7651, T7451 |
Boeing |
USA |
|
MMS 1420 |
T7451 |
Boeing |
USA |
|
MEP 02-014 |
T7451 |
Embraer |
S.America |
|
MM 566 |
W51, T7451 |
BAE |
Systems |
|
LMA-M7050 |
T7451 |
Lockheed |
|
7055 |
AIMS 03-02-017/024 |
T7751/T7951 |
Airbus |
France |
7075 |
EN 2126 |
W51, T651 |
|
Europe |
|
EN 2511 |
T7351 |
|
Europe |
|
ASN-A-3009 |
T7351 |
Airbus |
France |
|
04-32-471 |
T7351 |
Airbus |
France |
|
AIR 9048.680/.690/.700/.710 |
T651/T7351/T7351/T7651 |
|
France |
|
CR 1.1.0.76 |
T651, T7351 |
Dassault |
France |
|
3.4364 |
T651, T7351 |
|
Germany |
|
ABM3-1074 |
W51, T651, T651 |
|
UK |
|
(L95*) BAEM 0150 |
T351 (T651) |
|
UK |
|
BAEM 1204 |
T7351 |
|
UK |
|
AMS 4044/4045/4078 |
O/T651/T7351 |
|
USA |
|
AMS QQ-A-250/12 |
O, F, T651,T7351 |
Boeing |
USA |
|
AMS QQ-A-250/24 |
T7651 |
|
USA |
|
MMS 159 |
T7351 |
Boeing |
USA |
|
MM 0532 |
T7351 |
BAE Systems |
|
7085 |
AIMS 03-02-025 |
T7651 |
Airbus |
France |
7150 |
ABM3-1031/BAEM 1219 |
W51, T651 |
|
Europe |
|
AIMS 03-02-011/026 |
T651/T7751 |
Airbus |
France |
|
AMS 4252 |
T7751 |
|
USA |
|
BAMS/CMS 516-06 |
T7751 |
Bombardier |
USA |
7175 |
EN 2512 |
T7351 |
|
Europe |
|
04-32-471A |
T3751 |
Airbus |
France |
|
AIMS 03-02-008 |
T7351 |
Airbus |
France |
|
CR 1.1.0.88 |
T7351 |
|
France |
|
ASN-A-3050 |
T7351 |
Airbus |
France |
|
ABS 5064 |
T7351 |
|
France |
|
3.4364 |
T7351 |
|
Germany |
|
Air 9048 |
T7351 |
|
France |
7449 |
AIMS 03-02-015/016/028 |
T651/T7951/T7651 |
Airbus |
UK |
|
ABSS 23713 |
T7651 |
|
UK |
7475 |
EN 2805/4457 |
T7651/T7351 |
|
Europe |
|
AIMS 03-02-009 |
T7351 |
Airbus |
France |
|
AIR 9048.720/.730 |
T7351/T7651 |
|
France |
|
BAMS/CMS 516-02 |
T7351 |
Bombardier |
USA |
|
3.4384 |
T7351 |
|
Germany |
|
AMS 4089/4090/4202 |
T7651/T651/T7351 |
|
USA |
|
DMS 2184 |
T7351 |
Boeing |
USA |
|
MEP 02-013 |
T7351 |
Embraer |
S.America |
|
FMS 3004 |
T7351, T7651 |
Lockheed |
|
|
MM 0565 |
W51, T7351 |
BAE Systems |
|
COUNTRY |
SPECIFICATION |
ALLOY |
TEMPER |
|
|
|
|
EUROPE |
EN 2123 |
2618A |
T351, T851 |
(AECMA) |
EN 2124 |
2214 |
T451, T651 |
|
EN 2126 |
7075 |
W51(T651) |
|
EN 2419 |
2024 |
T351 |
|
EN 2422 |
2124 |
T351 |
|
EN 2511 |
7075 |
T7351 |
|
EN 2512 |
7175 |
T7351 |
|
EN 2684/2687 |
7010 |
W51(T7651)/T7451 |
|
EN 2805/4457 |
7475 |
T7651/T7351 |
|
EN 3982/3983 |
7050 |
T7451/T7651 |
|
EN 4213 |
6061 |
T651 |
|
EN 4214 |
7010 |
T651 |
|
EN 6000 |
2024 |
T351* |
FRANCE |
AIR 9048.610/.620 |
2214 |
T451/T451(T651), T651 |
(AIR) |
AIR 9048.630 |
2024 |
T351 |
|
AIR 9048.640 |
2618A |
T351(T851), T851 |
|
AIR 9048.680/.690/.700/.710 |
7075 |
T651/T7351/T7351/T7651 |
|
AIR 9048.720/.730 |
7475 |
T7351/T7651 |
|
AIR 9048.740 |
7050 |
T7451 |
GERMANY |
3.1354 |
2024 |
T351, T851 |
(WERKSTOFF) |
3.1924 |
2618A |
T651 |
|
3.3214 |
6061 |
T451, T651 |
|
3.4144 |
7050 |
T7451 |
|
3.4364 |
7075 |
T651, T7351 |
|
3.4384 |
7475 |
T7351 |
|
3.4394 |
7010 |
T7451 |
UK |
L93 |
2014A |
T651 |
BS(L) |
L95*** |
7075 |
T651 |
|
L97 |
2024 |
T351 |
|
L115 |
6082 |
T651 |
(DTD) |
DTD 5010 |
2014A |
T651 |
|
DTD 5120 |
7010 |
T7651 |
|
DTD 5130 |
7010 |
T7451 |
USA |
AMS 4025/4026/4027 |
6061 |
O/T451/T651 |
(AMS) |
AMS 4028/4029 |
2014 |
O/T651 |
|
AMS 4035/4037 |
2024 |
O/T351 |
|
AMS 4044/4045/4078 |
7075 |
O/T651/T7351 |
|
AMS 4050/4201 |
7050 |
T7451/T7651 |
|
AMS 4089/4090/4202 |
7475 |
T7651/T651/T7351 |
|
AMS 4101 |
2124 |
T851 |
|
AMS 4203/4204/4205 |
7010 |
T7351/T7651/T7451 |
|
AMS 4252 |
7150 |
T7751 |
|
AMS QQ-A-250/4 |
2024 |
O, T351, T851 |
|
AMS QQ-A-250/11 |
6061 |
O, F, T451, T651 |
|
AMS QQ-A-250/12 |
7075 |
O, F, T651, T7351 |
|
AMS QQ-A-250/24 |
7075 |
T7651 |
|
AMS QQ-A-250/29 |
2124 |
T351, T851 |
|
AMS QQ-A-250/30 |
2219 |
O, T351, T37, T87, T851 |
COMPANY |
SPECIFICATION |
ALLOY |
TEMPER |
|
|
|
|
AIRBUS |
04.32.170 |
5086 |
O, H111 |
FRANCE |
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-3011 |
2024 |
T351 |
|
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 03.02.004 |
2024 |
T351 |
|
AIMS 03.02.008 |
7175 |
T7351 |
|
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 |
BAEM 0120/ABM2-6027 |
6061 |
T4(T42) |
CIVIL |
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 1.1.0.36 |
2024 |
T351 |
|
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 |
|
CR 1.1.0.88 |
7175 |
T7351 |
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, 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 ) 57-A, KHATARGALLI, THAKURDWAR, MUMBAI - 400002, INDIA. TEL.No. 0091-22-23858802 TEL.No. 0091-22-23823963 FAX No. 0091-22-23898724 Email : rolexmetal@vsnl.net Website : www.rolexalloys.com CHAIRMAN - chairman@rolexalloys.com DIRECTOR MANAGING - managingdirector@rolexalloys.com DIRECTOR TECHNICAL - technicaldirector@rolexalloys.com INTERNATIONAL SALES - salesinternational@rolexalloys.com DOMESTIC SALES - salesdomestic@rolexalloys.com INFORMATION GENERAL - info@rolexalloys.com GENERAL SALES - sales@rolexalloys.com SERVICE - service@rolexalloys.com RECRUITMENT - career@rolexalloys.com WEBMASTER - webmaster@rolexalloys.com
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