01-147-8322
Radome
Used on b-1b aircraft. u/a: radome, tail tip cone; u/o: 001 & subq; c/o: -003 outer skin, -005 core, -007 web, -009 core, -013 inner skin, -015 shim, -017 core, -019 core, -023 strip, -015 block, jumpers, expandable adhesive, & misc hardware; next assy: L3005999
01-147-8370
Structural Aircraft Plate
Used on acft model c/kc-135. titanium sheet ti-6al-4v per mil-t-9046 type iii, composition c annealed; finish f-10.10; 40.000 in. lg, 6.000 in. w, 0.080 in. thk; opposite p/n -608
01-147-8371
Structural Aircraft Plate
Used on acft model c/kc-135. titanium sheet ti-6al-4v per mil-t-9046 type iii, composition c annealed; finish f-10.10; 40.000 in. lg, 6.000 in. w, 0.080 in. thk; opposite p/n -607
01-147-8372
Structural Aircraft Plate
15.000" overall length 5.000" overall width 0.080" material thickness
01-147-8373
Structural Aircraft Plate
4.900" overall length 2.300" overall width 0.125" material thickness
01-147-8374
Structural Aircraft Plate
4.900" overall length 2.300" overall width 0.125" material thickness
01-147-8375
Aircraft Fairing
10.100" overall length 7.200" overall width 0.040" material thickness opp -6
01-147-8376
Aircraft Fairing
Opposite -511
01-147-8377
Aircraft Fairing
Opposite -4
01-147-8378
Aircraft Fairing
Opposite -3
01-147-8379
Aircraft Fairing
10.100" overall length 7.200" overall width 0.040" material thickness opposite -5
01-147-8380
Aircraft Fairing
01-147-8381
Aircraft Fairing
10.000" overall length 7.600" overall width 0.050" material thickness opposite -614
01-147-8382
Aircraft Fairing
10.000" overall length 7.600" overall width 0.050" material thickness opposite -613
01-147-8383
Aircraft Fairing
10.200" overall length 7.700" overall width 0.050" material thickness
01-147-8384
Aircraft Fairing
10.200" overall length 7.700" overall width 0.050" material thickness
01-147-8386
Structural Component Air Support
Used on c-141a/c aircraft. used on frame installation lower center, fuselage station 379.55, 386.75, 404.00; matl-2024-T3 clad qq-a-362 temper-T3; dim-3.00 in. lg, 2.00 in w, 0.050 in. thk
01-147-8387
Structural Component Air Support
Used on f-15 acft. function-support aileron bell crank; location-xw-173.192-yw 260.215
01-147-8393
Aircraft Former
Used on B-52. extruded
01-147-8394
Aircraft Former
Used on B-52. extruded
01-147-8395
Aircraft Former
25.000" overall length made from GA3065, alcoa 9802, or 67580
01-147-8396
Aircraft Former
25.000" overall length made from GA3065, alcoa 9802, or 67580
01-147-8397
Aircraft Former
25.000" overall length made from GA3065, alcoa 9802, or 67580
01-147-8398
Aircraft Former
10.000" overall length 2.620" overall width with radius 83.21
01-147-9027
Aircraft Pylon
01-147-9074
Aircraft Fairing
0.080" material thickness
01-147-9093
Aircraft Former
17.500" overall length 1.600" overall width 0.050" material thickness
01-147-9094
Aircraft Former
17.500" overall length 1.600" overall width 0.050" material thickness
01-147-9095
Aircraft Former
10.000" overall length 1.400" overall width 0.050" material thickness
01-147-9096
Airfoil Rib
17.500" overall length 10.000" overall width 0.050" material thickness
01-147-9097
Airfoil Rib
17.500" overall length 10.000" overall width 0.050" material thickness
01-147-9098
Airfoil Rib
17.500" overall length 10.000" overall width 0.050" material thickness
01-147-9099
Airfoil Rib
17.500" overall length 10.000" overall width 0.050" material thickness
01-147-9100
Airfoil Rib
17.500" overall length 10.000" overall width 0.050" material thickness
01-147-9101
Airfoil Rib
13.500" overall length 10.000" overall width 0.050" material thickness
01-148-0359
Access Aircraft Door
01-148-0443
Structural Component Air Bracket
3.000" overall length 1.300" overall width 0.050" material thickness c/o nutplates
01-148-0460
Aircraft Spar
01-148-0461
Aircraft Spar
01-148-0462
Aircraft Spar
01-148-0463
Aircraft Spar
01-148-0509
Structural Aircraft Plate
7.500" overall length 6.000" overall width 0.060" material thickness cres aisi 302
01-148-0510
Structural Aircraft Plate
3.000" overall length stock bac 1511-161
01-148-0511
Structural Aircraft Plate
4.500" overall length 2.300" overall width 0.080" material thickness
01-148-0512
Structural Aircraft Plate
16.000" overall length 10.000" overall width 0.050" material thickness
01-148-0513
Structural Aircraft Plate
5.500" overall length 1.250" overall width 0.063" material thickness
01-148-0515
Structural Aircraft Plate
0.060" material thickness 0.875 in od
01-148-0516
Structural Aircraft Plate
Location-rib NR2 installation outboard strut
01-148-0517
Structural Aircraft Plate
15.000" overall length 5.000" overall width 0.080" material thickness
01-148-0518
Structural Aircraft Plate
2.900" overall length 0.500" overall width 0.030" material thickness
