Most of what goes out our door is aluminum, and the first question is never the shape. It's the alloy and temper. Get that wrong, and the print doesn't matter.
2024 in T3, T3511, or T4 is still what most structural angle, tee, zee, and channel gets made from. It's been on airframes since the 1930s for a reason: it tolerates damage, and it holds up under fatigue. 7075 shows up where the designer needs more strength per pound: stringers, spar caps, longerons, seat tracks. T6 and T6511 are the common tempers; when somebody's worried about stress corrosion, they'll call out T73511 instead, and we stock both. 6061-T6 and 6063 cover everything that isn't primary structure: ducting, interior framing, tooling, GSE. Cheap, easy to machine, anodizes well, and you can weld it, which you can't say for 2024 or 7075.
Then there's the odd stuff. 6013 and 7150 on newer programs. 7050 in thicker sections. 2014 and 2219 on airplanes that were designed before most of our customers were born. We chase those down too.
Material is certified to AMS-QQ-A-200 and the alloy-specific AMS specs (AMS 4152, AMS 4154, AMS 4160, AMS 4161, AMS 4166, and so on), or to ASTM B221 when the drawing calls for it. We carry the AND10133, AND10134, AND10136, and AND10138 standard shapes and can run Boeing BAC, Douglas, Lockheed, and Northrop proprietary profiles.
We also source stainless in 304, 316 and 17-4PH for galleys, lavs and hydraulic bays where aluminum corrodes. Titanium extrusions in 6Al-4V and commercially pure grades for engine and landing gear areas. Magnesium for a handful of legacy weight-critical parts. Brass, bronze and copper when the job needs conductivity or a bearing surface.