01-219-3230
Aircraft Former
01-219-3231
Aircraft Former
01-219-3232
Aircraft Former
01-219-3233
Aircraft Former
01-219-3234
Aircraft Former
01-219-3235
Aircraft Former
01-219-3236
Aircraft Former
01-219-3239
Aircraft Skin
Used on acft model kc-135. nha 65-41416-1
01-219-3240
Aircraft Skin
Used on acft model kc-135.
01-219-3241
Aircraft Skin
Used on acft model kc-135.
01-219-3242
Aircraft Skin
01-219-3710
Fluid Aircraft Manifold
Used on acft model f-111. to allow mfg of two piece manifold for easy replacement in wing without removing outer skin
01-219-3711
Fluid Aircraft Manifold
Used on acft model f-111. to allow mfg of two piece manifold for easy replacement in wing without removing outer skin
01-219-3737
Structural Aircraft Plate
Used on acft model kc-135. nha 65-41416-1
01-219-3739
Structural Aircraft Plate
25.300" overall length 1.300" overall width 0.050" material thickness used on windshield assembly
01-219-3759
Aircraft Former
01-219-3760
Aircraft Former
01-219-3761
Aircraft Former
8.200" overall length 3.800" overall width 0.090" material thickness
01-219-3762
Aircraft Former
8.200" overall length 3.800" overall width 0.090" material thickness
01-219-3764
Aircraft Skin
32.000" overall length 16.000" overall width
01-219-4610
Structural Component Air Support
01-219-4948
Filler Opening Cap
01-219-5000
Structural Component Air Support
01-219-5040
Structural Aircraft Plate
Used on mcdonnell p/n 32-33260 frame. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5, T3; matl 0.032 in. thk by 2.141 in. w by 4.000 in. lg; oval shape; w/ aperature; 4 mtg holes 0.250 in. dia; 1 rivet hole 0.196 in. min
01-219-5041
Structural Aircraft Plate
Used on mcdonnell p/n 32-33261-1 floor aircraft. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5; matl 0.040 in. thk by 3.750 in. w by 10.094 in. lg; right hand appl
01-219-5042
Structural Aircraft Plate
Used on mcdonnell p/n 32-33261-1 floor aircraft. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5; matl 0.040 in. thk by 3.750 in. w by 10.094 in. lg; left hand appl
01-219-5043
Structural Aircraft Plate
Used on mcdonnell p/n 32-33261-1 floor aircraft. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5, T3; matl 0.040 in. thk by 3.719 in. w by 9.000 in. lg; right appl
01-219-5044
Structural Aircraft Plate
Used on mcdonnell p/n 32-33261-1 floor aircraft. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5, T3; matl 0.040 in. thk by 3.719 in. w by 9.000 in. lg; left appl
01-219-5045
Structural Aircraft Plate
Used on 1560-00-484-4641. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, T651; matl 0.040 in. thk by 2.000 in. w by 6.703 in. lg
01-219-5046
Structural Aircraft Plate
Type/model designation:f-4e/gy/ steel comp 301 mil-s-5059 cond 1/2 hard; matl 0.032 in. thk by 2.641 in. w by 3.850 in. lg; double angle; 2 mtg slots 0.219 in. w by 0.328 in. lg
01-219-5048
Aircraft Fairing
01-219-5049
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-200/3, T4; 0.906 in. lg
01-219-5050
Structural Component Air Support
Used on 1560-00-484-4641. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, T651; matl 0.040 in. thk by 4.797 in. w by 9.000 in. lg; u cross section; tapered lg
01-219-5054
Structural Component Air Support
Used on 1560-00-030-4597. type/model designation:f-4e/gy/ aluminum alloy 6061 qq-a-250/11 cond o
01-219-5055
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 0.040 in. thk by 1.078 in. w by 1.547 in. lg
01-219-5057
Structural Component Air Support
Used on acft model f-111. c/o support steel casting per AMS5355 17-4 cres, bushing, nut
01-219-5058
Structural Component Air Support
Used on acft model f-111. c/o support steel casting per AMS5355 17-4 cres, bushing, nut
01-219-5064
Structural Aircraft Panel
Used on acft model b-52g/h. c/o 1 skin, 10 doublers, 6 stiffeners; opposite p/n -502; nha 35-1900
01-219-5065
Structural Aircraft Panel
01-219-5066
Structural Aircraft Panel
C/o skin, core, frame, as required adhesive, compound, sealer
01-219-5067
Former
Used on mcdonnell p/n 32-33258-1/-303 frame assy. 11.703" overall length 6.000" overall width 0.040" material thickness right appl
01-219-5068
Aircraft Former
01-219-5069
Aircraft Former
01-219-5070
Aircraft Former
01-219-5071
Aircraft Former
01-219-5072
Aircraft Former
28.000" overall length 4.000" overall width 0.050" material thickness
01-219-5074
Airfoil Rib
Used on F-15.
01-219-5075
Airfoil Rib
Used on F-15.
01-219-5076
Wing Section Center Rib
