ADDENDUM TO 2011 TAN SHEETS Tempers For Aluminum And Aluminum Alloy Products Metric Edition June, New and Revised Registrations

Transcription

1 s For Aluminum And Aluminum s Metric Edition June, 201 By Date Over Thru Basis 1 Ult. Yield 201T11 Sumitomo 0/01/2012 Drawn Tube 0 D or. A * Tentative 201T11 Sumitomo 12/1/2011 Drawn Tube * Tentative 22T1 Alcoa 0/22/2011 /22/201 Plate Min Min Fracture Toughness 1 Min K IC or K Q For thicknesses through 0.00 LT direction m TL direction m 22T Alcoa 01/2/2011 Plate Min 2 00 Cold rolled ~% and stretched ~1% after solution heat treating. Fracture Toughness 1 K IC or K Q For thicknesses LT direction m TL direction m 21T Alcan Global ATI 0/2/2011 Plate * Tentative Material is cold worked in the range of % after solution heat treatment For thicknesses 2.00 through Crings and tensile specimens machined and tested in accordance with ASTM G shall show no evidence of stress corrosion failure when tested in the short transverse direction at 2 and exposed for 0 days. Fracture Toughness 1 *M in K IC For thicknesses 2.00 through.00 LT direction m TL direction m SL direction 0 m (from 0.00 )

2 s For Aluminum And Aluminum s Metric Edition June, T Constellium 01/20/201 Extruded Bar D or. A For thicknesses over.00 through LT direction m TL direction m SL direction 0 m Solution heat treated, cold worked approximately % and artificially aged. For thicknesses over 0.00 thru.00 Tensile specimens machined and tested in accordance with ASTM G shall show no evidence of stress corrosion failure when tested in the short transverse direction at 00 and exposed for 0 days. 200T Alcan Constellium 0/2/200 0/0/2012 Plate Min Min Min For thicknesses Direct Crings and Tensile specimens machined and tested in accordance with ASTM G shall show no evidence of stress corrosion failure when tested in the short transverse direction at Mpa and exposed for Min Min Min Min days. Fracture Toughness 1 Min K Ic For thicknesses over 12.0 thru 0.00 LT direction m TL direction 2 m SL direction 2 m

3 s For Aluminum And Aluminum s Metric Edition June, D or. A Min Min For thicknesses over 0.00 thru 0.00 LT direction m TL direction 0 m SL direction 2 m Min Min For thicknesses over 0.00 thru 0.00 LT direction 1 m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru 0.00 LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses over thru.00 LT direction 2 m TL direction 22 m SL direction 20 m For thicknesses over.00 thru 1.00 LT direction 2 m TL direction 21 m SL direction 1 m

4 s For Aluminum And Aluminum s Metric Edition June, D or. A 20T Alcoa 01/1/201 Extrusion Solution heat treated and cold worked in the range 2% and artificially aged Cross Sectional Area less than or equal to and Circle Size less than or equal to Fracture Toughness 1 Min. K IC or K Q For thicknesses over through 0.00 LT direction 2 m TL direction 21 m T Alcoa 0/0/201 Plate Solution heat treated, cold worked approximately % and artificially aged. Fracture Toughness 1 Min K IC or K Q For thicknesses over thru 0.00 LT direction 2 m TL direction m 20T Constellium 0/1/201 Extrusion Solution heat treated, cold worked approximately % and artificially aged. 21T Constellium 0/0/2012 Sheet & Plate.20.0 Min 0 0 2

5 s For Aluminum And Aluminum s Metric Edition June, D or. A 21T1 Constellium 0/2/2011 Plate Developed to meet armor plate requirements of Mil STD21. Material is solution heat treated, cold worked in the range %, and underaged. 21 T11 2 Alcan Constellium /0/200 0/2/2012 Extrusion T1 Alcoa 0/01/2011 Extrusions Min 0 0 Stretched approximately 1 % and underaged. Material shall be capable of passing the stress corrosion cracking test described in ASTM G when tested in the LT direction at a stress of 2 for 0 days. Exfoliation Corrosion Resistance Specimens shall not exhibit exfoliation corrosion At a T/2 plane greater than that illustrated by Photo 2 (EB) from Figure 2 of ASTM G when specimens are exposed for 2 weeks according to the procedures in ASTM G Annex A2, using the drybottom MASTMAASIS Test Method. Fracture Toughness 1 Min K IC or K Q For thicknesses LT direction m

6 s For Aluminum And Aluminum s Metric Edition June, 201 By Date Over Thru Basis 1 Ult. Yield 21T Alcoa 0/1/2011 Plate D or. A * Tentative Solution heat treated, cold worked approximately % and artificially aged. Exfoliation Corrosion Resistance Specimens shall not exhibit exfoliation corrosion at a T/ plane greater than that illustrated by Photo 2 (EA) from Figure 2 of ASTM G when specimens are exposed for 2 weeks according to the procedures in ASTM B Annex A2, using the drybottom MASTMAASIS Test Method. Fracture Toughness 1 Min K IC or K Q For thicknesses through 0.00 LT direction m TL direction m 00H22 Alcoa 0/12/2011 Sheet Used for tread plate applications. H11 Alcoa 11/2/2012 Sheet Max 2 Used for tread plate applications H11 Alcoa 0/22/2012 Plate *Max *Max Developed to meet armor plate requirements of MIL DTL02K *Max 1 0

7 s For Aluminum And Aluminum s Metric Edition June, 201 0H12 Alcoa 11/1/2012 /0/201 Sheet & Plate , *Max,, *Max,, *Max,, *Max, D or. A Exfoliation Corrosion Resistance After a postproduction thermal treatment of 0 C (212 F) for 1 week, this material shall be capable of exhibiting no evidence of exfoliation corrosion and a pitting rating of PB or better, when subjected to the test described in ASTM Test Method G (ASSET). Intergranular Corrosion Resistance After a postproduction thermal treatment of 0 C (212 F) for 1 week, this material shall be capable of exhibiting massloss no greater than 1 mg/cm 2 [0 mg/in. 2 ] when tested in accordance with ASTM Test Method G (NAMLT). H21 Constellium 02//2012 Sheet & Plate Max Max Exfoliation Corrosion Resistance This material shall be capable of exhibiting no evidence of exfoliation corrosion and a pitting rating of PB or better, when subjected to the test described in ASTM Test Method G (ASSET). Intergranular Corrosion Resistance This material shall be capable of exhibiting resistance to intergranular corrosion as required by ASTM B 2 when subjected to the test described in ASTM Test Method G (NAMLT).

8 s For Aluminum And Aluminum s Metric Edition June, 201 0H21 Alcoa 0/21/200 0/01/2012 Sheet *Max D or. A * Tentative Exfoliation Corrosion Resistance This material shall be capable of exhibiting no evidence of exfoliation corrosion and a pitting rating of PB or better, when subjected to the test described in ASTM Test Method G (ASSET). Intergranular Corrosion Resistance This material shall be capable of exhibiting resistance to intergranular corrosion as required by ASTM B 2 when subjected to the test described in ASTM Test Method G (NAMLT). 0H21 Alcoa 0/0/200 0/01/2012 Plate.0.00 *Max *Max * Tentative Exfoliation Corrosion Resistance This material shall be capable of exhibiting no evidence of exfoliation corrosion and a pitting rating of PB or better, when subjected to the test described in ASTM Test Method G (ASSET). Intergranular Corrosion Resistance This material shall be capable of exhibiting resistance to intergranular corrosion as required by ASTM B 2 when subjected to the test described in ASTM Test Method G (NAMLT). T Werner 01/2/2012 Extrusion The registered properties for this material are calculated in accordance with the procedure described under.c.1 of page ii of the Tan Sheets

9 s For Aluminum And Aluminum s Metric Edition June, D or. A 01T & T11 Alcoa 0/11/2012 Extrusions, Rod & Seamless Tube T2 Alcoa 0/1/2011 Sheet Min 0 1 0T Rio Tinto Alcan 02/2/2011 Extrusion T signifies higher mechanical properties than 0T. 0T, & T11 02T, & T11 Kaiser 12/21/200 12/1/2011 Alcoa SAPA 0/11/200 12/0/201 Extruded Rod, Bar, and Profiles 0 OttoFuchs 0/0/2011 Hand T2 22 Forgings The registered properties for the material are calculated in accordance with the procedure described under.c.1. on page ii of the Tan Sheets The registered properties for this material are calculated in accordance with the procedure described under.c.1 on page ii of the Tan Sheets. Extrusion Min Min See footnote.b Min Min Fracture Toughness 1 Min. K IC or K Q For thicknesses over 0.00 thru 0.00 LT direction m Min Min 2 TL direction 2 m SL direction 2 m Min Min For thicknesses over 0.00 thru.00 LT direction m

10 s For Aluminum And Aluminum s Metric Edition June, D or. A TL direction 2 m SL direction 2 m For thicknesses over.00 thru LT direction m TL direction 2 m SL direction 2 m For thicknesses over thru LT direction m TL direction 21 m SL direction 2 m 2T1 Alcoa 0/11/2011 0/1/201 Plate Min Exfoliation Corrosion Resistance See footnote 1.b. Fracture Toughness 1 Min K IC For thicknesses LT direction 2 LT direction 2 Longitudinal Compressive Yield Strength for thickness: 0 minimum 0T1 Alcoa 0/12/201 Plate See footnote b Fracture Toughness 1 Min K IC or K Q For thicknesses 2.00 thru 0.00 LT direction m

11 s For Aluminum And Aluminum s Metric Edition June, D or. A TL direction m For thicknesses 0.00 thru 0.00 LT direction 0 m TL direction 2 m For thicknesses 0.00 thru LT direction m TL direction 0 m SL direction 2 m For thicknesses 0.00 thru 0.00 LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses 0.00 thru LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses thru.00 LT direction 2 m TL direction 2 m SL direction 2 m 0T1 Alcoa 0/12/201 Plate See footnote a.

12 s For Aluminum And Aluminum s Metric Edition June, D or. A Fracture Toughness 1 Min K IC or K Q For thicknesses 2.00 thru 0.00 LT direction m TL direction 0 m For thicknesses 0.00 thru LT direction m TL direction 0 m For thicknesses 0.00 thru 0.00 LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses 0.00 thru 0.00 LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses 0.00 thru LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses thru.00 LT direction 2 m TL direction 22 m SL direction 22 m

13 s For Aluminum And Aluminum s Metric Edition June, D or. A 0T11 Alcoa /2/2011 Plate Solution heat treated, stretched 1. to %, and overaged for ballistic performance. Developed to meet armor plate requirements of MILDTL2 (MR). Exfoliation Corrosion Resistance See footnote 1.b 0T21 Alcoa /2/2011 Plate Solution heat treated, stretched 1. to %, and overaged for blast performance. Developed to meet armor plate requirements of MILDTL2 (MR). Exfoliation Corrosion Resistance See footnote 1.b 0T1 Alcoa 02/0/200 0/0/2012 Plate Min Min See footnote.b Min Min Fracture Toughness K IC or K Q For Thicknesses LT direction 0 m Min Min TL direction 0 m SL direction 0 m Min Min For thicknesses LT direction m TL direction 2 m SL direction 2 m

14 s For Aluminum And Aluminum s Metric Edition June, D or. A For thicknesses LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses LT direction 2 m TL direction 2 m SL direction 2 m 0T1 Kaiser 01/22/201 Plate See Footnote.b

15 s For Aluminum And Aluminum s Metric Edition June, D or. A 0T1 Kaiser 01/22/201 Plate See Footnote.a

16 s For Aluminum And Aluminum s Metric Edition June, 201 Tentative Removed By Date 0T Extruded Rod, Bar, Kaiser 12/1/011 & T11 and Profiles T1 Plate Constellium 0/2/201 T1 Plate Alcoa 0/2/2011 0O Sheet Alcoa 01/1/2011 Corrections to Table of Mechanical Property Limits Designation Correction H11 2 Sheet and Plate The maximum UTS limits for thickness ranges and are corrected to read 00.

17 s For Aluminum And Aluminum s Metric Edition June, 201 Reactivated s Reactivated Thickness, By Date 0 200T Alcoa 0/11/ 0/0/0 Alcoa 0/1/2012 Extrusion D or. A Min

18 ++ Deactivation is limited to specific Gauge Range(s) for the product indicated. ADDENDUM TO 2011 TAN SHEETS s For Aluminum And Aluminum s Metric Edition June, 201 Deactivated Registrations Date Deactivated 200T Extrusion 0/0/ T Sheet 12/21/2011 0T2 Sheet 0/0/2011 Alclad 201O ++ Plate 0/2/2012 Alclad 201T2 ++ Plate 0/2/2012 Alclad 201T1 ++ Plate 0/2/2012 Alclad 201T2 ++ Plate 0/2/2012 Alclad 201T1 ++ Plate 0/2/2012 Alclad 221O ++ Plate 0/2/2012 Alclad 221T2 ++ Plate 0/2/2012 Alclad 01O ++ Plate 0/2/2012 Alclad 01T2 ++ Plate 0/2/2012 Alclad 01T1 ++ Plate 0/2/2012 Alclad 01T2 ++ Plate 0/2/2012 Alclad 01T1 ++ Plate 0/2/2012 Alclad 0O ++ Plate 0/2/2012 Alclad 0T2 ++ Plate 0/2/2012 Alclad 0T1 ++ Plate 0/2/2012 Alclad 0T1 ++ Plate 0/2/2012 Alclad 0T1 ++ Plate 0/2/ ½% Alclad 0O ++ Plate 0/2/ ½% Alclad 0T2 ++ Plate 0/2/ ½% Alclad 0T1 ++ Plate 0/2/ ½% Alclad 0T1 ++ Plate 0/2/ ½% Alclad 0T1 ++ Plate 0/2/2012 Alclad One Side 0O ++ Plate 0/2/2012 Alclad One Side 0T2 ++ Plate 0/2/2012 Alclad One Side 0T1 ++ Plate 0/2/ ½% Alclad One Side 0O ++ Plate 0/2/ ½% Alclad One Side 0T2 ++ Plate 0/2/ ½% Alclad One Side 0T1 ++ Plate 0/2/ T1 Plate 0/2/201