01-155-8211
Structural Aircraft Plate
3.600" overall length 0.800" overall width 0.020" material thickness
01-155-8212
Structural Aircraft Plate
9.000" overall length 1.900" overall width 0.020" material thickness
01-155-8213
Structural Aircraft Plate
2.100" overall length 0.600" overall width 0.032" material thickness
01-155-8214
Structural Aircraft Plate
23.400" overall length 2.100" overall width 0.020" material thickness
01-155-8215
Structural Aircraft Plate
23.400" overall length 2.100" overall width 0.020" material thickness
01-155-8216
Structural Aircraft Plate
23.300" overall length 2.100" overall width 0.020" material thickness
01-155-8217
Structural Aircraft Plate
23.300" overall length 2.100" overall width 0.020" material thickness
01-155-8218
Structural Aircraft Plate
6.000" overall length 2.000" overall width 0.032" material thickness
01-155-8220
Structural Component Air Support
5.600" overall length 4.800" overall width 0.032" material thickness
01-155-8221
Structural Component Air Support
5.600" overall length 4.800" overall width 0.032" material thickness
01-155-8230
Aircraft Former
21.800" overall length 2.000" overall width 0.025" material thickness
01-155-8231
Aircraft Former
6.200" overall length 1.500" overall width 0.032" material thickness
01-155-8232
Aircraft Former
6.200" overall length 1.500" overall width 0.032" material thickness
01-155-8233
Aircraft Former
20.800" overall length 1.900" overall width 0.020" material thickness
01-155-8234
Aircraft Former
21.300" overall length 1.900" overall width 0.020" material thickness
01-155-8235
Aircraft Former
5.600" overall length 1.200" overall width 0.025" material thickness
01-155-8236
Aircraft Former
9.500" overall length 3.400" overall width 0.032" material thickness
01-155-8237
Aircraft Former
9.500" overall length 3.400" overall width 0.032" material thickness
01-155-8238
Aircraft Former
12.600" overall length 3.400" overall width 0.032" material thickness
01-155-8239
Aircraft Former
Used on F-111.
01-155-8244
Longeron
Used on A-10.
01-155-8247
Airfoil Rib
Used on F-15. 20.000" overall length 9.000" overall width 4.500" material thickness function-prevent flame propagation in event fuel vapors are ignited by anti-collision light
01-155-8248
Fuel Aircraft Tank
300 gal fus ctr line external fuel tank
01-155-9030
Structural Aircraft Panel
Used on B-52.
01-155-9031
Structural Aircraft Panel
Used on B-52. 11.600" overall length 6.200" overall width
01-155-9032
Structural Aircraft Plate
1.500" overall length 1.500" overall width 0.040" material thickness used as cowl
01-155-9033
Structural Aircraft Plate
Used on B-52. 1.850" overall length 0.600" overall width 0.120" material thickness material per bac 1524-120
01-155-9034
Structural Aircraft Plate
7.700" overall length 2.300" overall width 0.025" material thickness
01-155-9035
Structural Aircraft Plate
7.700" overall length 2.300" overall width 0.025" material thickness
01-155-9036
Structural Aircraft Plate
4.100" overall length 1.800" overall width 0.025" material thickness
01-155-9037
Structural Aircraft Plate
1.600" overall length 0.700" overall width 0.032" material thickness
01-155-9038
Structural Aircraft Plate
20.900" overall length 1.600" overall width 0.050" material thickness
01-155-9039
Structural Aircraft Plate
5.100" overall length 4.000" overall width 0.020" material thickness
01-155-9040
Structural Aircraft Plate
21.600" overall length 1.600" overall width 0.040" material thickness
01-155-9041
Structural Aircraft Plate
21.600" overall length 1.600" overall width 0.040" material thickness
01-155-9042
Structural Aircraft Plate
12.100" overall length 1.900" overall width 0.032" material thickness
01-155-9043
Structural Aircraft Plate
2.100" overall length 1.200" overall width 0.032" material thickness
01-155-9044
Structural Aircraft Plate
2.000" overall length 0.800" overall width 0.032" material thickness
01-155-9045
Structural Aircraft Plate
1.200" overall length 0.600" overall width 0.063" material thickness decarb per ams 6350
01-155-9046
Structural Aircraft Plate
6.400" overall length 1.600" overall width 0.100" material thickness decarb limit per ams 6358
01-155-9047
Structural Aircraft Plate
6.400" overall length 1.600" overall width 0.100" material thickness decarb limit per ams 6358
01-155-9048
Structural Aircraft Plate
Used on B-52. 0.850" overall length 0.600" overall width 0.062" material thickness make from bac 1524-6255
01-155-9049
Structural Aircraft Plate
2.400" overall length 1.200" overall width 0.032" material thickness
01-155-9050
Structural Aircraft Plate
2.900" overall length 1.200" overall width 0.032" material thickness
01-155-9051
Structural Aircraft Plate
2.800" overall length 1.200" overall width 0.032" material thickness
01-155-9052
Structural Aircraft Plate
1.700" overall length 1.300" overall width 0.020" material thickness annealed, cond 2d
01-155-9053
Structural Aircraft Plate
46.000" overall length 2.000" overall width 0.050" material thickness
01-155-9054
Structural Aircraft Plate
47.000" overall length 1.500" overall width 0.040" material thickness
01-155-9055
Structural Aircraft Plate
47.000" overall length 1.500" overall width 0.040" material thickness
01-155-9057
Structural Component Air Support
2.000" overall length 1.400" overall width 0.040" material thickness opp 39-14611-22; used as frame attachment on cowl body panel
