And Foil; Nonferrous Base Metal Strip Sheet Plate - Supply Class (FSC) 9535

01-531-7802

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished sheet thickness

9535-01-531-7803

01-531-7803

Metal Plate

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished plate thickness

9535-01-531-7806

01-531-7806

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished sheet thickness

9535-01-532-0294

01-532-0294

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0297

01-532-0297

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0298

01-532-0298

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0308

01-532-0308

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0309

01-532-0309

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished sheet thickness; tensile strength 32000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0310

01-532-0310

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 5.0 percent of composite thickness or 4.0 percent of finished sheet thickness; tensile strength 30000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0311

01-532-0311

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished sheet thickness; tensile strength 32000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0315

01-532-0315

Metal Sheet

Used on fuselage f4f jet aircraft. thin layers approximately equal thickness, of aluminum alloy 1230 anodic to the core are bonded to both surfaces; cladding thickness for each layer to be 2.5 percent of composite thickness or 2.0 percent of finished sheet thickness; tensile strength 32000.0 pounds per square inch; yield strength 14000.0 pounds per square inch

9535-01-532-0506

01-532-0506

Metal Sheet