01-148-4213
Structural Aircraft Plate
1.470" overall length 1.250" overall width 0.062" material thickness matl bac 1524-6255
01-148-4214
Structural Aircraft Plate
20.000" overall length 2.300" overall width 0.125" material thickness
01-148-4215
Structural Aircraft Plate
31.000" overall length 2.300" overall width 0.125" material thickness
01-148-4216
Structural Aircraft Plate
01-148-4217
Structural Aircraft Plate
Opposite p/n 25-2308-75
01-148-4218
Structural Aircraft Plate
Function-web assembly
01-148-4219
Structural Aircraft Plate
6.300" overall length 5.000" overall width 0.160" material thickness
01-148-4220
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059, comp d annealed, surf cond 2d; location-pp station-270.00 to 280.65, pp water line 108.40; tail fairing installation, outboard strut
01-148-4221
Structural Component Air Support
12.200" overall length 12.000" overall width 0.020" material thickness
01-148-4222
Structural Component Air Support
01-148-4223
Structural Component Air Support
6.300" overall length 1.400" overall width 0.045" material thickness
01-148-4224
Structural Component Air Support
01-148-4225
Structural Component Air Support
9.100" overall length 8.400" overall width 0.040" material thickness
01-148-4231
Aircraft Former
Used on B-52. function-stiffener; extrusion
01-148-4232
Aircraft Former
Used on B-52. function-chord assembly
01-148-4233
Aircraft Former
Used on B-52. extrusion
01-148-4235
Aircraft Former
26.400" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-4236
Aircraft Former
19.300" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-4237
Aircraft Former
9.300" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-4238
Aircraft Former
37.400" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-4239
Aircraft Former
37.400" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-4240
Aircraft Former
5.100" overall length 2.300" overall width 0.063" material thickness
01-148-4241
Aircraft Former
120.000" overall length 1.400" overall width 0.063" material thickness
01-148-4242
Aircraft Former
Used on B-52.
01-148-4243
Aircraft Former
Used on B-52. function-stiffener assembly
01-148-4246
Aircraft Former
01-148-4249
Airfoil Rib
20.000" overall length 9.000" overall width 4.500" material thickness prevents flame propagation in event fuel vapors are ignited by anti-collision light; special quality
01-148-4250
Aircraft Skin
Used on B-52. 60.000" overall length 29.000" overall width 6A1-4v annealed, bms 7-39; finishf 10.10
01-148-4251
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v annealed, bms 7-39; finishf 10.10
01-148-4252
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v annealed, bms 7-39; finish f 10.10; opposite p/n -503
01-148-4253
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v annealed, bms 7-39; finish f 10.10; opposite p/n -10
01-148-5520
Aircraft Frame
24.000" overall length 12.000" overall width 0.071" material thickness
01-148-5521
Aircraft Frame
24.000" overall length 12.000" overall width 0.071" material thickness
01-148-5525
Aircraft Spar
01-148-5613
Structural Aircraft Plate
21.000" overall length 12.000" overall width 0.040" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10; opposite p/n -510
01-148-5614
Structural Aircraft Plate
21.000" overall length 12.000" overall width 0.040" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10; opposite p/n -509
01-148-5615
Structural Aircraft Plate
10.000" overall length 7.000" overall width 0.064" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10; opposite -21
01-148-5616
Structural Aircraft Plate
3.000" overall length 1.600" overall width 0.063" material thickness used as doubler
01-148-5617
Structural Aircraft Plate
21.700" overall length 2.500" overall width 0.090" material thickness
01-148-5618
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059, comp d, annealed, surf cond 2d; location-near pp station 286.25, tail fairing installation-outboard strut
01-148-5619
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet, aisi 302 per mil-s-5059, comp d, annealed, surf cond 2d; location-at pp station 236.25, tail fairing installation-outboard strut
01-148-5620
Structural Aircraft Plate
9.190" overall length 5.369" overall width 1.200" material thickness
01-148-5621
Aircraft Fairing
Opposite -4
01-148-5622
Aircraft Fairing
Opposite -3
01-148-5623
Aircraft Fairing
Opposite -4
01-148-5624
Aircraft Fairing
Opposite -3
01-148-5625
Aircraft Fairing
01-148-5626
Structural Component Air Support
