Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire 4.4Cu - 1.5Mg - 0.60Mn (2024) Solution Heat Treated and Naturally Aged (T4) Solution Heat Treated, Cold Worked, and Naturally Aged (T351)
Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged
Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated
Aluminum Alloy, Rolled or Cold Finished Bars and Rods 4.4Cu - 1.5Mg - 0.60Mn (2024-T851) Solution Heat Treated, Cold Worked, and Artificially Aged
Aluminum Alloy, Extruded Profiles (2024-T432) 4.4Cu - 1.5Mg - 0.6Mn Annealed, Stretch Formed, Solution Heat Treated and Stress Relieved by Stretching
Tube, Aluminum Alloy, Drawn, Seamless, 5086 (Stabilized: Feb 2018)
Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0Mg - 0.80Si - 1.8Cu - 0.20Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged
Tube, Aluminum and Aluminum Alloy, Drawn, Seamless, General Specification for (Stabilized: Feb 2018)
Wrought Nickel and Nickel-Related Alloys (Stabilized: Feb 2018)
INSERT, SCREW THREAD, HELICAL COIL, METRIC SERIES, FREE RUNNING, CRES, DRY FILM LUBRICATED (Stabilized: Feb 2018)
Design of Aircraft Deicing Facilities
HOSE ASSEMBLY, PTFE, PARA-ARAMID REINFORCED, STANDARD DUTY, 3000 PSI, 275 °F, TITANIUM FITTINGS, BEAM SEAL, 45° TO 90° (Stabilized: Feb 2018)