01-220-1171
Structural Component Air Support
Used on 1560-00-894-4179. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, T651; made from p/n 1M2310 nsn 9540-01-009-6795 structural angle; 1.000 in. lg; l cross section; left appl
01-220-1172
Structural Component Air Support
Used on 1560-00-894-4179. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/15; matl 0.040 in. thk by 1.703 in. w by 5.297 in. lg; l cross section; right appl
01-220-1173
Structural Component Air Support
Used on 1560-00-894-4179. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/15; matl 0.040 in. thk by 1.703 in. w by 5.297 in. lg; l cross section; left appl
01-220-1174
Structural Component Air Support
Used on 1560-00-894-4179. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/15; matl 0.063 in. thk by 4.297 in. w by 15.297 in. lg, u cross section; right appl
01-220-1181
Structural Aircraft Panel
28.600" overall length 21.000" overall width material per mms-1203 6al-6v-2sn
01-220-1194
Aircraft Former
01-220-1195
Aircraft Former
01-220-1196
Aircraft Former
01-220-1197
Aircraft Former
01-220-1198
Aircraft Former
01-220-1199
Aircraft Former
01-220-1200
Aircraft Former
01-220-1201
Aircraft Former
01-220-1202
Aircraft Former
01-220-1203
Aircraft Former
01-220-1204
Aircraft Former
01-220-1205
Aircraft Former
01-220-1206
Aircraft Former
01-220-1207
Aircraft Former
01-220-1208
Aircraft Former
6.500" overall length 4.000" overall width 1.250" material thickness
01-220-1209
Aircraft Former
10.250" overall length 2.500" overall width 2.500" material thickness
01-220-1210
Aircraft Former
10.250" overall length 3.000" overall width 2.500" material thickness
01-220-1211
Aircraft Former
01-220-1214
Longeron
Used on F-15. material per 1MT0039A01X122.00
01-220-1215
Longeron
Used on F-15. material per 1MT0039A01X122.00
01-220-1216
Longeron
Used on F-15. material per 1MT360A01-10008 x 36.000 in. lg
01-220-1218
Aircraft Stringer
83.500" overall length material per 1MT363A01-10006
01-220-1219
Aircraft Stringer
83.500" overall length material per 1MT363A01-10006
01-220-1220
Aircraft Stringer
34.600" overall length material per 1MT363A01-10016
01-220-1221
Aircraft Stringer
34.600" overall length material per 1MT363A01-10016
01-220-1222
Aircraft Stringer
01-220-1223
Aircraft Stringer
27.000" overall length stock 1MT363A01-10016
01-220-1224
Aircraft Stringer
27.000" overall length stock 1MT363A01-10016
01-220-1225
Aircraft Stringer
34.000" overall length material per 1MT363A0-10016
01-220-1226
Aircraft Stringer
34.700" overall length material per 1MT363A01-10016
01-220-2840
Structural Aircraft Plate
5.650" overall length 4.700" overall width 0.045" material thickness
01-220-2841
Structural Aircraft Plate
5.650" overall length 4.700" overall width 0.045" material thickness
01-220-2842
Structural Aircraft Plate
6.200" overall length 4.500" overall width 0.050" material thickness material per mms-1203 6al-6v-2sn
01-220-2843
Structural Aircraft Plate
5.400" overall length 3.500" overall width 0.050" material thickness
01-220-2844
Structural Aircraft Plate
3.600" overall length 2.200" overall width 0.063" material thickness
01-220-2845
Structural Aircraft Plate
11.800" overall length 2.000" overall width 0.063" material thickness
01-220-2846
Structural Aircraft Plate
16.400" overall length 2.600" overall width 0.050" material thickness
01-220-2847
Structural Aircraft Plate
16.400" overall length 2.600" overall width 0.050" material thickness
01-220-2848
Structural Aircraft Plate
5.400" overall length 3.600" overall width 0.032" material thickness
01-220-2849
Structural Aircraft Plate
17.300" overall length 2.600" overall width 0.050" material thickness
01-220-2850
Structural Aircraft Plate
17.300" overall length 2.600" overall width 0.050" material thickness
01-220-2851
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 3.000 in. lg, 1.800 in. w, 0.036 in. thk
01-220-2852
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 3.000 in. lg, 1.800 in. w, 0.036 in. thk
01-220-2853
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 16.500 in. lg, 2.400 in. w, 0.080 in. thk
01-220-2854
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 16.500 in. lg, 2.400 in. w, 0.080 in. thk
