01-221-1009
Aircraft Former
48.000" overall length 18.000" overall width 0.063" material thickness
01-221-1010
Aircraft Former
48.000" overall length 18.000" overall width 0.063" material thickness
01-221-1011
Aircraft Former
17.550" overall length 5.700" overall width 0.063" material thickness material per mms-1203 6al-6v-2sn
01-221-1012
Aircraft Former
Stock 68A332071-2005
01-221-1013
Aircraft Former
42.000" overall length 12.000" overall width 1.250" material thickness
01-221-1014
Aircraft Former
42.000" overall length 12.000" overall width 1.250" material thickness
01-221-1015
Aircraft Former
Stock 68A332041-2005
01-221-1016
Aircraft Former
45.000" overall length 12.400" overall width 1.500" material thickness
01-221-1017
Aircraft Former
34.700" overall length 22.000" overall width 0.036" material thickness material per mms-1203 6al-6v-2sn
01-221-1018
Airfoil Rib
Used on aircraft,b-52g.
01-221-1019
Airfoil Rib
Used on aircraft,b-52g.
01-221-1022
Aircraft Skin
Used on f-15a/b aircraft. 38.000" overall length 20.000" overall width per 6al-6v-2sn mms 1203
01-221-1023
Aircraft Skin
Used on F-15. 38.000" overall length 20.000" overall width per 6al-6v-2sn mms 1203
01-221-1233
Structural Aircraft Plate
Material per 68A331021-2007
01-221-1234
Structural Aircraft Plate
Material per 68A331021-2007
01-221-1235
Structural Aircraft Plate
13.200" overall length 1.500" overall width 0.056" material thickness
01-221-1236
Structural Component Air Support
Used on acft model f-16c/d usaf. consists of 1 support, 3 nut, rivet a/r; eff 37 0001 9999; nha 16P3130-5
01-221-1237
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 20.000 in. lg, 4.000 in. w, 0.125 in. thk
01-221-1238
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 20.000 in. lg, 4.000 in. w, 0.125 in. thk
01-221-1239
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 9.000 in. lg, 3.500 in. w, 0.063 in. thk
01-221-1240
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 6.400 in. lg, 1.600 in. w, 0.063 in. thk
01-221-1241
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.300 in. lg, 2.500 in. w, 0.045 in. thk
01-221-1242
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.300 in. lg, 2.500 in. w, 0.045 in. thk
01-221-1243
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition e anl, 4.200 in. lg, 2.500 in. w, 0.045 in. thk
01-221-1244
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition e anl, 4.200 in. lg, 2.500 in. w, 0.045 in. thk
01-221-1245
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.300 in. lg, 2.500 in. w, 0.045 in. thk
01-221-1246
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.300 in. lg, 2.500 in. lg, 0.045 in. thk
01-221-1247
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 3.450 in. lg, 2.250 in. w, 0.045 in. thk
01-221-1248
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 10.000 in. lg, 2.200 in. w, 0.036 in. thk
01-221-1249
Structural Component Air Support
Used on f-15 aircraft. material per mms 1203 6al-6v-2sn, 52.300 in. lg, 2.800 in. w, 0.040 in. thk
01-221-1250
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 14.800 in. lg, 2.700 in. w, 0.036 in. thk
01-221-1251
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 14.800 in. lg, 2.700 in. w, 0.036 in. thk
01-221-1252
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 12.400 in. lg, 2.400 in. w, 0.040 in. thk
01-221-1253
Structural Component Air Support
Used on f-15 aircraft. material per mms 1203 6al-6v-2sn, 3.500 in. lg, 3.310 in. w, 0.036 in. thk
01-221-1254
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 2.700 in. lg, 1.500 in. w, 0.032 in. thk
01-221-1255
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 11.020 in. lg, 3.680 in. w, 0.056 in. thk
01-221-1256
Structural Component Air Support
Used on f-15 aircraft. material per mms 1203 6al-6v-2sn, 7.200 in. lg, 2.600 in. w, 0.063 in. thk
01-221-1258
Structural Component Air Support
Used on f-15 aircraft. titanium alloy per mil-t-9046 type 3 composition c anl, 8.400 in. lg, 2.200 in. w, 0.036 in. thk
01-221-1262
Aircraft Former
01-221-1263
Aircraft Former
Stock 68A332041-2005
01-221-1264
Aircraft Former
Stock 68A332071-2005
01-221-1265
Aircraft Former
45.000" overall length 12.400" overall width 1.500" material thickness
01-221-1266
Aircraft Former
9.840" overall length 6.300" overall width 0.056" material thickness
01-221-1267
Aircraft Former
01-221-1268
Aircraft Former
49.250" overall length 16.350" overall width 0.063" material thickness
01-221-1269
Aircraft Former
26.200" overall length 8.700" overall width 0.045" material thickness
01-221-1270
Aircraft Former
2.730" overall length 1.110" overall width 0.050" material thickness
01-221-1272
Aircraft Former
15.350" overall length 6.300" overall width 0.040" material thickness
01-221-1273
Aircraft Former
15.350" overall length 6.500" overall width 0.040" material thickness
01-221-1274
Aircraft Former
16.200" overall length 6.400" overall width 0.040" material thickness
