ADDENDUM TO 2011 TAN SHEETS. Tempers For Aluminum And Aluminum Alloy Products Metric July 16, New and Revised Registrations

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1 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0 mm 201T11 Sumitomo 0/01/2012 Drawn Tube D or. A * Tentative 201T11 Sumitomo 12/1/2011 Drawn Tube 22T1 Alcoa 0/22/2011 Plate * Tentative * Tentative Fracture Toughness 1 Min K IC or K Q For thicknesses 12.0 through 0.00 mm 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 mm LT direction m TL direction m

2 s For Aluminum And Aluminum s Metric July 1, T Alcan Global ATI By Date Over Thru Basis 1 Ult. Yield 0 mm 0/2/2011 Plate *Min D or. A * Tentative Material is cold worked in the range of % after solution heat treatment *Min *Min Stress Corrosion Resistance For thicknesses 2.00 through mm. 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 *Min K IC For thicknesses 2.00 through.00 mm LT direction m TL direction m SL direction 0 m (from 0.00 mm) For thicknesses over.00 through mm LT direction m TL direction m SL direction 0 m 200T Alcan Constellium 0/2/200 Plate 12.0 Revised 0/0/ Min Min Min Stress Corrosion Resistance For thicknesses mm 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 days.

3 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0 mm Min Min Min Min Min Min D or. A Fracture Toughness 1 Min K Ic For thicknesses over 12.0 thru 0.00 mm LT direction m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru 0.00 mm LT direction m TL direction 0 m SL direction 2 m For thicknesses over 0.00 thru 0.00 mm LT direction 1 m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru 0.00 mm LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru mm LT direction 2 m TL direction 2 m SL direction 2 m For thicknesses over thru.00 mm LT direction 2 m TL direction 22 m SL direction 20 m

4 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0 mm D or. A For thicknesses over.00 thru 1.00 mm LT direction 2 m TL direction 21 m SL direction 1 m 200T Alcoa 0/0/201 Plate *Tentative Solution heat treated, cold worked approximately % and artificially aged. Fracture Toughness 1 Min K IC or K Q For thicknesses mm LT direction 2 m TL direction m 21T Constellium 0/0/2012 Sheet & Plate.20.0 Min Min T1 Constellium 0/2/2011 Plate *Tentative Developed to meet armor plate requirements of Mil STD21. Material is solution heat treated, cold worked in the range %, and underaged.

5 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0 mm 21T11 2 Alcan /0/200 Constellium Revised 0/2/2012 Extrusion D or. A *Tentative 20T1 Alcoa 0/01/2011 Extrusions Min 0 0 Stretched approximately 1 % and underaged. Stress Corrosion Resistance 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. 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 mm LT direction m

6 s For Aluminum And Aluminum s Metric Edition July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 21T Alcoa 0/1/2011 Plate * Tentative Solution heat treated, cold worked approximately % and artificially aged. 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 mm 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 *Tentative Developed to meet armor plate requirements of MIL DTL02K *Max 1 0

7 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 0H12 Alcoa 11/1/2012 Sheet & Plate.00.00, 0 *Max, 21 *Tentative 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 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 July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 2 0H21 Alcoa 0/21/200 Sheet Revised 0/01/2012 *Max 0 1 * Tentative 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 Revised 0/01/2012 Plate.0.00 *Max *Max * Tentative 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).

9 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 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 2 of the Tan Sheets 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. The registered properties for the material are calculated in accordance with the procedure described under.c.1. on page ii of the Tan Sheets. 0T, & T11 Kaiser 12/21/200 Revised 12/1/2011 Extruded Rod, Bar, and Profiles The registered properties for this material are calculated in accordance with the procedure described under.c.1 on page ii of the Tan Sheets. 0 T2 2 OttoFuchs 0/0/2011 Hand Forgings Min Min Stress Corrosion Resistance See footnote.b. Fracture Toughness 1 Min K IC or K Q Min Min Min Min For thicknesses over 0.00 thru 0.00 mm LT direction m TL direction 2 m SL direction 2 m For thicknesses over 0.00 thru.00 mm LT direction m TL direction 2 m

10 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A SL direction 2 m For thicknesses over.00 thru mm LT direction m TL direction 2 m SL direction 2 m For thicknesses over thru mm LT direction m TL direction 21 m SL direction 2 m 2T1 Alcoa 0/11/2011 Plate See footnote 1.b. Min 2 Fracture Toughness 1 Min K IC For thicknesses mm LT direction 2 mm LT direction 2 mm Longitudinal Compressive Yield Strength for mm thickness: 0 minimum 0T11 Alcoa /2/2011 Plate *Tentative Solution heat treated, stretched 1. to %, and overaged for ballistic performance. Developed to meet armor plate requirements of MILDTL2 (MR). See footnote 1.b

11 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A T21 Alcoa /2/2011 Plate 12.0 *Tentative Solution heat treated, stretched 1. to %, and overaged for blast performance. Developed to meet armor plate requirements of MILDTL2 (MR). See footnote 1.b 0T1 Alcoa 02/0/200 Revised 0/0/2012 Plate Min Min Min Min Stress Corrosion Resistance See footnote.b Fracture Toughness 1 Min K IC or K Q For Thicknesses mm LT 0 m TL 0 m SL 0 m Min Min Min Min For thicknesses mm LT m TL 2 m SL 2 m For thicknesses mm LT 2 m TL 2 m SL 2 m For thicknesses mm LT 2 m TL 2 m SL 2 m

12 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 0T1 Kaiser 01/22/201 Plate *Tentative Stress Corrosion Resistance See Footnote.b *Min *Min *Min *Min 2 20

13 s For Aluminum And Aluminum s Metric July 1, 201 By Date Over Thru Basis 1 Ult. Yield 0mm D or. A 0T1` Kaiser 01/22/201 Plate *Tentative Stress Corrosion Resistance See Footnote.a *Min *Min *Min *Min 2 0 0

14 ADDENDUM TO 2011 EDITION OF TAN SHEETS s For Aluminum And Aluminum s July 1, 201 Tentative Removed By Revised Date 0T Extruded Rod, Bar, Kaiser 12/1/011 & T11 and Profiles T1 Plate Alcoa 0/2/2011 0O Sheet Alcoa 01/1/2011

15 ADDENDUM TO 2011 EDITION OF TAN SHEETS s For Aluminum And Aluminum s July 1, 201 Date Deactivated Deactivated Registrations 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 0/2/2012 Alclad 201O ++ Plate 0/2/2012 Alclad 201T2 ++ Plate 0/2/2012 Alclad 201T1 ++ Plate 0/2/2012 Alclad 201T2 ++ Plate 0/2/ Deactivation is limited to specific gauge range(s) for the product indicated.

16 ADDENDUM TO 2011 EDITION OF TAN SHEETS s For Aluminum And Aluminum s July 1, 201 Reactivated By Reactivation Date 200T Extrusion Alcoa 0/1/2012