01-531-7781
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
01-531-7783
Metal Sheet
Used on fuselage f4f jet aircraft. thin layers approximately equal thickness of aluminum alloy 1230 anodic to 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
01-531-7784
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
01-531-7785
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
01-531-7786
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
01-531-7787
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
01-531-7788
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
01-531-7789
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
01-531-7790
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
01-531-7791
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
01-531-7792
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
01-531-7793
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
01-531-7794
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
01-531-7795
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
01-531-7796
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
01-531-7798
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
01-531-7799
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
01-531-7800
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
01-531-7801
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
