01-203-7181
Structural Aircraft Panel
Used on acft model b-1b.
01-203-7182
Structural Aircraft Panel
Used on acft model b-1b.
01-203-7183
Structural Aircraft Panel
Used on acft model b-1b.
01-203-7194
Aircraft Former
01-203-7195
Aircraft Former
17-7ph lac 1-595 cond a
01-203-7196
Aircraft Former
17-7ph lac 1-595 cond a
01-203-7197
Aircraft Former
14.880" overall length 3.245" overall width 1.080" material thickness
01-203-7202
Airfoil Rib
20.700" overall length 7.800" overall width 0.032" material thickness
01-203-7203
Airfoil Rib
20.700" overall length 7.800" overall width 0.032" material thickness
01-203-7204
Airfoil Rib
12.000" overall length 9.000" overall width 0.032" material thickness
01-203-7207
Airfoil Rib
31.800" overall length 8.000" overall width 0.080" material thickness
01-203-7208
Airfoil Rib
31.800" overall length 8.000" overall width 0.080" material thickness
01-203-7209
Airfoil Rib
18.000" overall length 9.000" overall width 0.080" material thickness
01-203-7210
Airfoil Rib
18.000" overall length 9.000" overall width 0.050" material thickness
01-203-7211
Airfoil Rib
15.000" overall length 9.200" overall width 0.071" material thickness
01-203-7212
Airfoil Rib
15.000" overall length 9.200" overall width 0.071" material thickness
01-203-7213
Aircraft Skin
Used on f-5 aircraft.
01-203-7214
Aircraft Skin
94.000" overall length 33.000" overall width c/0 -27 skin; fin A804; nuts, rivets, sealant; superseded -803 ow per ecn 5H040; eff on 6d 0001 999; nha -16B5314-817
01-203-7215
Aircraft Skin
69.000" overall length 23.000" overall width
01-203-7216
Aircraft Skin
80.000" overall length 24.000" overall width
01-203-7218
Aircraft Stringer
76.500" overall length
01-203-7219
Aircraft Stringer
47.000" overall length
01-203-7220
Aircraft Stringer
66.000" overall length
01-203-7321
Bell Crank
Used on acft model b-1b. arms 180 deg; 2.62 lg, 1.25 wide, 1.00 thk; nha L3400134
01-203-8718
Aircraft Engine Build- Parts Kit
01-203-9493
Structural Aircraft Panel
Panel assembly, nose, forward, wheelwell fairing; used on 4F75003-601a, -108a, -110a, and -112a
01-203-9622
Structural Aircraft Plate
Used on c-5b aircraft. c/o: mount plate (1) , strip (2) ; nha 4N12407
01-203-9623
Structural Aircraft Plate
Used on acft model kc-135.
01-203-9624
Structural Aircraft Plate
Used on acft model kc-135. 9.3 in lg, 4.4 in wd, 0.063 in thk; clad 2024-T3 sheet per qq-a-362, T3temper, finish srf 2.115
01-203-9627
Structural Aircraft Plate
12.000" overall length 8.000" overall width 0.020" material thickness
01-203-9628
Structural Component Air Support
Used on t-38 aircraft. located fus sta 388.75; matl S101625 extr al alloy 7075-T6 per qq-a-277; size 42.00in long
01-203-9629
Structural Component Air Support
Used on acft model kc-135. consists of 1 fitting, 2 bushing; opposite p/n -2
01-203-9630
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha 65C18243
01-203-9631
Structural Component Air Support
Used on acft model kc-135. 7075-T73 alum die forging per BMS7-186; finish f-2.47; opposite p/n -1; nha 65C18245; located at sta 204.86
01-203-9632
Structural Component Air Support
Used on acft model c-18a. nha 69-25624-1
01-203-9633
Structural Component Air Support
Used on acft model c-18a. nha 50-7946
01-203-9634
Structural Component Air Support
Used on acft model c-18a. nha 50-8294-5
01-203-9638
Structural Component Air Support
Used on acft model kc-135. consist of 1 fitting, 4 bushing; nha 65C18245; located at nac sta 205.41
01-203-9639
Structural Component Air Support
Used on acft model kc-135. consist of 1 support angle, 1 channel, 2 fairlead, 2 bolt, 2 nutplate, 2 spacer
01-203-9640
Structural Component Air Fitting
Nha 5-84477-3078s
01-203-9645
Bleed Air Duct Assembly
C/o 1 tube, 2 subassy, 1 doubler, 1 bracket
01-203-9660
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -109a & -111a stiffener (1 ea) , -117a lug (1) , -141b web assembly (1) ;
01-203-9661
Structural Aircraft Panel
Used on acft model b-1b. epoxy glass sheet, l-p-509 type iv grade g-11; 71.00 in. long, 29.88 in. wide, 0.063 in. thick; nha L5342229-079
01-203-9662
Structural Aircraft Panel
C/o doubler p/n 12B3803-438, spacer p/n 12B3803-439, skin assembly p/n 12B3803-834
01-203-9663
Structural Aircraft Panel
C/o doubler p/n 12B3803-437, spacer p/n 12B3803-439, skin assembly p/n 12B3803-501
01-203-9671
Aircraft Former
9.140" overall length
01-203-9672
Aircraft Former
9.000" overall length
01-203-9673
Aircraft Former
6.700" overall length
01-203-9674
Aircraft Former
6.100" overall length 6.250" overall width 6.250" material thickness
01-203-9676
Airfoil Rib
20.200" overall length 7.700" overall width 0.032" material thickness
