01-203-4601
Aircraft Skin
79.000" overall length 28.000" overall width
01-203-4602
Aircraft Skin
30.000" overall length 24.000" overall width
01-203-4603
Aircraft Skin
80.000" overall length 24.000" overall width
01-203-4604
Aircraft Spar
78.000" overall length 9.500" overall width 0.063" material thickness
01-203-4605
Aircraft Stringer
76.000" overall length
01-203-4606
Aircraft Stringer
76.000" overall length
01-203-4607
Aircraft Stringer
76.500" overall length
01-203-4608
Aircraft Stringer
76.500" overall length
01-203-4610
Aircraft Window Panel
01-203-6860
Access Aircraft Cover
Used on F-16. dorsal fairing access
01-203-6861
Access Aircraft Cover
Used on F-16. dorsal fairing access
01-203-6862
Access Aircraft Cover
Used on acft model b-1b. 0.250" hole diameter end radius 7.000 in.; nha L3022127; used as fuselage yf 686.50 to 792.50 fuel tank access door
01-203-6863
Access Aircraft Cover
Used on b-1b aircraft. 0.256" hole diameter nuclear hardness critical item; holes countersunk 0.090 by 0.415 in. dia; nha L3010828; used as fuel tank access door
01-203-7073
Structural Component Air Support
Used on acft model b-1b. made from -005 die forging hp-9-4-30 steel, cond nt; c/o 1 hook, 3 bushings; nha L3400134
01-203-7101
Aircraft Bulkhead
Made 12B9544013
01-203-7127
Structural Aircraft Plate
Used on acft model b-1b. consists of 1 stud, 1 plate
01-203-7128
Structural Aircraft Plate
Used on kc-135 aircraft. stock size .063 (2.9X1.8) ; matl inconel 625 annealed sheet per AMS5599; fin f-4.10; nha 458-52033
01-203-7129
Structural Aircraft Plate
Used on kc-135 aircraft. stock size .063 (3.6X2.7) ; matl inconel 625 annealed sheet per AMS5599; fin f-4.10; nha 458-52033
01-203-7130
Structural Aircraft Plate
Used on kc-135 stratolifter aircraft. 3.600" overall length bracket-fire detector inconel 625 annealed sheet per AMS5599; finish f-4.10 nha 458-52033
01-203-7131
Structural Aircraft Plate
Used on acft model kc-135. molded plastic glass fabric laminate; finish f-6.10; nha 5-86024; consist of 1 bulkhead, 1 grommet; located at sta 1670
01-203-7132
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7990-156; used as cargo door upper forward strip
01-203-7136
Structural Aircraft Plate
10.750" overall length 1.780" overall width 0.620" material thickness
01-203-7137
Aircraft Fairing
C/o 89 bushings, 2 retainer, 2 nuts, 1 lip, 1 skin, 4 angles, rivots a/r; opposite -002; nha L3226900
01-203-7138
Aircraft Fairing
C/o 89 bushings, 2 retainers, 2 nuts, 1 lip, 1 skin, 4 angles, rivots a/r; opp -001; nha L3226900
01-203-7139
Aircraft Elevator
01-203-7144
Structural Component Air Support
Used on c-5b aircraft.
01-203-7145
Structural Component Air Support
Used on c-5b aircraft.
01-203-7146
Structural Component Air Support
Used on t-38 aircraft.
01-203-7147
Structural Component Air Support
01-203-7148
Structural Component Air Support
Used on c-5b aircraft.
01-203-7149
Structural Component Air Support
Used on kc-135 aircraft. stock sz 1.3X1.1X2.2in; matl 15-5ph bar per AMS5659, ht tr 155-170 ksi per BAC5619; fin f-8.07; nha 65C18616
01-203-7150
Structural Component Air Support
Used on kc-135 aircraft. stock 1.5; matl 17-4 ph stainless steel plate per AMS5643; fin f-1.108; nha 458-52033
01-203-7151
Structural Component Air Support
Used on acft model kc-135. consist of 2 rod end, 1 tube, 1 pin, 1 chain; nha 458-52022
01-203-7152
Structural Component Air Support
Used on acft model kc-135. consist of 2 rod end, 1 tube, 1 pin, 1 chain; nha 458-52022
01-203-7153
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel PH13-8M0; stock size 3.05 in. lg, 2.88 in. w, 2.10 in. thk; c/o 1 fitting, 2 bushings; opposite p/n -002; nha L3223450
01-203-7155
Structural Component Air Support
Used on acft model kc-135. consist of 1 bracket, 2 angle, 2 shear plate, 2 collar, 2 lock bolt, 2 rig pin plate; nha 65-12778
01-203-7156
Structural Component Air Support
Used on c-130 acft. p/o firewall assy; steel mil-s-5059 type 301; 27.250 in. lg, 1.100 in. dp, 3.555 in. w
01-203-7157
Structural Component Air Support
Used on c-130 acft. p/o firewall assy-upper; steel mil-s-5059 type 301; 19.690 in. lg; 1.170 in. dp, 2.861 in. w
01-203-7161
Structural Aircraft Panel
01-203-7162
Structural Aircraft Panel
01-203-7169
Structural Aircraft Panel
Used on c-5b aircraft. 20.000" overall length 6.000" overall width nha 4F54200; opposite -112a
01-203-7171
Structural Aircraft Panel
Matl LS33821-1X26; nha 4F54200, eff on 0082 & up
01-203-7172
Structural Aircraft Panel
C/o: insert (4) , splice plate (2) , reinforcement (3) , face sheet (4) , doubler (3) , core (4) , filler block (2) ; opposite -178a; nha 4F20021
01-203-7173
Structural Aircraft Panel
Used on c-5b aircraft. consist of one angle, -105a; one panel, -117a; one safety strip instl; one doubler; opposite -124a
01-203-7174
Structural Aircraft Panel
Used on acft model kc-135. consist of 1 bottom manifold, 1 reservoir sides, 2 bracket, 1 plate, 1 filler metal; nha 458-52022
01-203-7175
Structural Aircraft Panel
Nuclear hardness critical item; consist of 1 outer skin, 1 inner skin, 1 core, 1 closeout, 4 frame, misc hardware
01-203-7176
Structural Aircraft Panel
2.150" overall length 0.620" overall width nha L3400124
01-203-7177
Structural Aircraft Panel
Used on acft model b-1b.
01-203-7178
Structural Aircraft Panel
Used on acft model b-1b.
01-203-7179
Structural Aircraft Panel
Used on acft model b-1b.
