01-150-9042
Aircraft Fairing
Nha 16B5886-5, effective 62 0077 9999, c/o fairing 16B5886-13, 2 supports, 1 outlet, 1 baffle
01-150-9044
Structural Component Air Support
01-150-9045
Structural Component Air Support
Used on acft model c/kc-135. located sta 173.50; nha 65-2516
01-150-9046
Structural Component Air Support
01-150-9047
Structural Component Air Support
01-150-9048
Structural Component Air Support
11.300" overall length c/o 1 channel, 1 guard strip
01-150-9049
Structural Component Air Support
C/o 1 channel, 1 clip assy, 1 guard strip, 4 nutplate
01-150-9050
Structural Component Air Support
C/o 1 channel, 1 clip assy, 1 guard strip, 4 nutplate
01-150-9051
Structural Component Air Support
C/o 1 angle, 5 nutplate
01-150-9058
Aircraft Former
106.000" overall length
01-150-9059
Aircraft Former
105.000" overall length
01-150-9060
Aircraft Former
Used on b-52 acft.
01-150-9061
Aircraft Former
10.500" overall length 1.500" overall width 0.025" material thickness
01-150-9062
Aircraft Former
5.600" overall length 1.200" overall width 0.032" material thickness
01-150-9063
Aircraft Former
5.600" overall length 1.200" overall width 0.032" material thickness
01-150-9064
Aircraft Former
13.000" overall length 3.000" overall width 0.040" material thickness
01-150-9065
Aircraft Former
28.000" overall length 15.600" overall width 0.050" material thickness
01-150-9066
Aircraft Former
28.000" overall length 15.600" overall width 0.050" material thickness
01-150-9067
Aircraft Former
14.000" overall length 7.500" overall width 0.050" material thickness
01-150-9068
Aircraft Former
14.000" overall length 7.500" overall width 0.050" material thickness
01-150-9069
Aircraft Former
Used on acft model b-52. 1.000" overall length 0.800" overall width 0.200" material thickness laminated thermosetting shgg per mil-p-15035
01-150-9070
Aircraft Former
Used on acft model b-52. 1.000" overall length 0.800" overall width 0.200" material thickness laminated thermosetting shgg per mil-p-15035
01-150-9071
Aircraft Former
Used on acft model b-52. 23.000" overall length made from bac-1490-2668
01-150-9072
Aircraft Former
Used on acft model b-52. 23.000" overall length made from bac-1490-2668
01-150-9078
Aircraft Skin
Used on B-52. 30.000" overall length 19.000" overall width
01-150-9079
Aircraft Skin
Used on B-52. 32.000" overall length 10.000" overall width
01-150-9080
Aircraft Skin
Used on B-52. 30.000" overall length 8.000" overall width
01-150-9081
Aircraft Skin
Used on B-52. 30.000" overall length 26.000" overall width
01-150-9083
Aircraft Window Panel
01-150-9394
Structural Component Aircraf Web
23.100" overall length 17.600" overall width 0.040" material thickness
01-150-9405
Structural Aircraft Plate
12.000" overall length 4.000" overall width 0.063" material thickness
01-150-9406
Structural Aircraft Plate
17.200" overall length 2.200" overall width 0.063" material thickness
01-150-9408
Aircraft Former
23.700" overall length 5.710" overall width 0.100" material thickness
01-150-9409
Aircraft Former
23.700" overall length 5.710" overall width 0.100" material thickness
01-150-9410
Aircraft Former
Used on acft model b52.
01-151-0232
Access Aircraft Door
Used on aircraft model f-18.
01-151-0332
Structural Aircraft Plate
Used on B-52. mfg stock BAC1506-1297 x 74.500 in. lg
01-151-0333
Structural Aircraft Plate
4.600" overall length 1.100" overall width 0.040" material thickness annealed; decarb limit per ams 6350; ht tr 180, 000-20, 000; opposite pn -509
01-151-0335
Structural Aircraft Plate
Used on B-52.
01-151-0336
Structural Aircraft Plate
Mfg stock BAC1505-1000357
01-151-0337
Structural Aircraft Plate
Used on B-52. mgf stock BAC1506-1295 x 43.000 in. lg
01-151-0338
Structural Aircraft Plate
Used on B-52. mfg stock BAC1506-1311 x 49.100 in. lg
01-151-0339
Structural Aircraft Plate
8.800" overall length 6.600" overall width 0.090" material thickness
01-151-0340
Structural Aircraft Plate
8.800" overall length 7.600" overall width 0.125" material thickness
01-151-0341
Structural Aircraft Plate
8.800" overall length 7.600" overall width 0.125" material thickness
01-151-0342
Structural Aircraft Plate
14.000" overall length 5.500" overall width 0.040" material thickness
01-151-0343
Structural Aircraft Plate
6.000" overall length 4.800" overall width 0.032" material thickness finish f-10.10; opposite pn -58
01-151-0344
Structural Aircraft Plate
6.000" overall length 4.800" overall width 0.032" material thickness opposite pn -57; finish f-10.10
01-151-0345
Structural Aircraft Plate
3.000" overall length 1.700" overall width 0.012" material thickness opposite pn -814
01-151-0346
Structural Aircraft Plate
3.000" overall length 1.700" overall width 0.012" material thickness opposite pn -813
