01-083-8938
Structural Component Air Support
Used on acft model f4c. alum alloy per qq-a-200/13 cond T651, stock size 1M9569 by 7.700 in.
01-083-8940
Airfoil Rib
8.700" overall length 4.700" overall width 0.050" material thickness
01-083-8942
Airfoil Rib
8.400" overall length 3.800" overall width 0.025" material thickness
01-083-8943
Airfoil Rib
7.700" overall length 6.900" overall width 0.050" material thickness
01-083-8944
Airfoil Rib
7.500" overall length 2.700" overall width 0.040" material thickness
01-083-8945
Airfoil Rib
7.850" overall length 3.200" overall width 0.050" material thickness
01-083-8946
Airfoil Rib
7.600" overall length 3.000" overall width 0.025" material thickness
01-083-8947
Aircraft Skin
01-084-0258
Structural Aircraft Panel
9.300" overall length 8.800" overall width
01-084-0259
Aircraft Fairing
01-084-0266
Airfoil Rib
10.000" overall length 3.200" overall width 0.080" material thickness
01-084-0267
Airfoil Rib
8.750" overall length 4.600" overall width 0.032" material thickness
01-084-0269
Airfoil Rib
5.700" overall length 2.600" overall width 0.063" material thickness
01-084-0270
Airfoil Rib
14.000" overall length 5.000" overall width 0.063" material thickness
01-084-1418
Radome
Acft b-52
01-084-1419
Aircraft Fairing
01-084-1420
Aircraft Fairing
01-084-1436
Aircraft Skin
Used on c-135 airplane.. panel instl w.b.l.64320 to w.s.360
01-084-2110
Structural Aircraft Plate
Used on acft model 1f4c. alum alloy 7178-T6 per qq-a-250/15 cond T6, 0.100 in.thick, 1.450 in.wide, 3.550 in.length, right hand
01-084-2121
Airfoil Rib
7.400" overall length 3.700" overall width 0.063" material thickness
01-084-2237
Structural Component Air Support
Used on uh-60 blackhawk. tie rod right side-support assembly
01-084-2643
Aircraft Pylon
Used on f-16a/b/c/d usaf aircraft. pylon assy, fuel tank-bl 71.00; c/016D640-3 bracket instl (1) , 16D1915-811 harness instl (1) , 16D1915-807 tape instl (1) , hardware, support assy, skin assy, fairing, longeron, longeron assy, skin, frame, ejector instl, closure, sway brace; eff on-0074-0079, 0084-0085, 0090-0091, 0096, 0097, 0101-0102, 0114-0115, 0130-0131, nha-16S400-825;
01-084-3424
Access Aircraft Cover
01-084-5036
Aircraft Skin
55.000" overall length 17.000" overall width effectivity 0019-on, ecn 61724, nha 16B1932-3; superseded 16B1318-21, i/c code ow
01-084-5453
Access Aircraft Door
Spring loaded self-closing
01-084-6754
Structural Component Air Bracket
01-084-6838
Structural Aircraft Plate
7.640" overall length 0.060" overall width 0.250" material thickness left hand
01-084-7187
Aircraft Skin
Used on c-135 airplane.. installed at w.bl.L64320 to w.s.360
01-084-8393
Radome
Used on F-16. 73.500" overall length nose radome
01-084-8440
Aircraft Skin
Used on F-16.
01-084-8441
Aircraft Skin
Used on F-16.
01-084-9338
Structural Aircraft Panel
01-084-9339
Structural Aircraft Panel
01-084-9437
Aircraft Skin
Used on F-16.
01-084-9438
Aircraft Skin
Used on F-16.
01-084-9720
Structural Aircraft Plate
01-085-0066
Access Aircraft Door
01-085-0067
Access Aircraft Door
01-085-0068
Access Aircraft Door
01-085-0069
Access Aircraft Door
01-085-0333
Structural Component Air Support
Used on aircraft model ov-10d.
01-085-0334
Structural Component Air Support
Used on aircraft model ov-10d.
01-085-0335
Structural Component Air Support
Used on aircraft model ov-10. steel, 8.830 in. lg
01-085-0346
Horizontal Stabilizer
Used on aircraft model e2c.
01-085-1366
Structural Component Air Support
01-085-1370
Structural Aircraft Plate
01-085-1870
Structural Component Air Support
Support assembly, drag link
01-085-1875
Structural Component Air Support
Eff on 0020 & on; nha 16B1270-1; superseded p/n: 16B1270-35 ow per ecn 67695
