01-219-5077
Wing Section Center Rib
01-219-5078
Aircraft Skin
Used on f111 aircraft.
01-219-5079
Aircraft Skin
Used on F-111. 23.000" overall length 22.000" overall width
01-219-5488
Structural Component Air Support
4.750" overall width
01-219-6168
Aircraft Fairing
0.063" material thickness le flap upper wg seal nbr 6436
01-219-6813
Structural Aircraft Panel
01-219-6819
Fuselage Aircraft Fairing
01-219-6822
Thermal Aircraft Insulation
Used on eh-60 HELIC0pter, side wall , fuselarge station 379 to 398
01-219-7367
Structural Component Air Support
Steel, aisi 1095 or 4140 or 4340 or 6150 or 8740 or steel, mil-s-8844, class 1; heat treated, mil-h-6875, rockwell scale c, 43.0 min, 46.0 max; magnetic particle inspected, mil-i-6868; cadmium
01-219-8168
Access Aircraft Door
Used on ac-130h acft.
01-219-8234
Access Hole Aircraft Frame
01-219-8235
Aircraft Fairing
01-219-8246
Structural Aircraft Plate
01-219-8247
Structural Aircraft Plate
P/o side door assy modification, 105 mm gun dome
01-219-8248
Structural Aircraft Plate
34.500" overall length 3.000" overall width 1.000" material thickness p/o lower, door assembly modification, 105mm gun dome
01-219-8249
Structural Aircraft Plate
34.500" overall length 3.000" overall width 1.380" material thickness p/o upper door assembly modification, 105mm gun dome
01-219-8250
Structural Aircraft Plate
36.820" overall length 3.000" overall width 1.500" material thickness p/o door assembly modification, 105mm gun dome
01-219-8251
Structural Aircraft Plate
P/o door assembly modification, 105mm gun dome
01-219-8252
Structural Aircraft Plate
21.100" overall length 8.410" overall width 0.050" material thickness p/o door assembly modification, 105mm gun dome
01-219-8253
Structural Aircraft Plate
Type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5; matl 0.063 in. thk by 6.000 in. w by 9.000 in. lg
01-219-8254
Structural Component Air Support
2.200" overall length 0.875" overall width
01-219-8255
Structural Component Air Support
34.980" overall length
01-219-8256
Structural Component Air Support
34.500" overall length
01-219-8257
Structural Component Air Support
01-219-8258
Structural Component Air Support
01-219-8259
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13; matl 0.040 in. thk by 1.656 in. w by 9.797 in. lg; l cross section; right appl
01-219-8260
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13; matl 0.040 in. thk by 1.656 in. w by 9.797 in. lg; l cross section; left appl
01-219-8261
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/14; matl 0.050 in. thk by 1.820 in. w by 9.406 in. lg; u/w nas 1055-5 rivets
01-219-8262
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 4.750 in. lg; u cross section; left appl
01-219-8263
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 4.406 in. lg; u cross section; right appl
01-219-8264
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 5.000 in. lg; u cross section; left appl
01-219-8265
Structural Component Air Support
Used on 1560-00-484-4641. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5, T3; matl 0.071 in. thk by 1.125 in. w by 1.797 in. lg
01-219-8266
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 4.797 in. lg; u cross section
01-219-8270
Aircraft Former
15.000" overall length
01-219-8271
Aircraft Former
01-219-8272
Aircraft Former
01-219-8273
Aircraft Former
01-219-8274
Aircraft Former
01-219-8277
Aircraft Skin
49.880" overall length 37.140" overall width 105mm gun dome
01-219-8278
Aircraft Skin
01-219-8279
Aircraft Skin
01-219-8280
Aircraft Skin
01-219-8721
Access Aircraft Door
01-219-9288
Structural Aircraft Plate
4.000" overall length 9.300" overall width 0.028" material thickness
01-219-9289
Structural Aircraft Plate
13.680" overall length 1.080" overall width 0.056" material thickness
01-219-9290
Structural Aircraft Plate
13.680" overall length 1.080" overall width 0.056" material thickness
