01-222-3419
Aircraft Fairing
Used on aircraft,model a-4.
01-222-3799
Structural Component Air Bracket
C/o 2 doubler, vane assy, sealant, adhesive, rivets
01-222-3808
Structural Component Air Support
01-222-3811
Structural Component Air Support
Used on f-15 aircraft. titanium per mil-t-9046 type 3 composition c anl, 7.000 in. lg, 9.250 in. w, 0.050 in. thk
01-222-3812
Structural Component Air Support
Used on f-15 aircraft. titanium per mil-t-9046 type 3 composition c anl, 1.350 in. lg, 2.750 in. w, 0.050 in. thk
01-222-3813
Structural Component Air Support
Used on f-15 aircraft. titanium per mil-t-9046 type 3 composition a anl, 4.250 in. lg, 2.250 in. w, 1.250 in. thk
01-222-3815
Structural Aircraft Panel
Used on acft model e-3a. c/o preimpregnated glass fabric, semi-rigid vinyl, decorative laminate, protective facing, 1 insert; nha 204-40165
01-222-3816
Structural Aircraft Panel
Used on acft model e-3a. c/o preimpregnated glass fabric, semi-rigid vinyl, decorative laminate, protective facing, 2 inserts; nha 204-40135
01-222-3820
Aircraft Skin
Used on FB-111. 82.000" overall length 60.000" overall width
01-222-3821
Aircraft Skin
Used on FB-111. 82.000" overall length 60.000" overall width
01-222-4098
Longeron
Used on aircraft,model ta7c trainer. 16 holes 0.188 in. dia; 8 holes 0.250 in dia; 5 holes 0.312 in. dia; 187 holes 0.156 in. dia
01-222-4136
Structural Aircraft Plate
52.000" overall length 17.300" overall width 0.063" material thickness
01-222-4137
Structural Aircraft Plate
52.000" overall length 17.300" overall width 0.063" material thickness
01-222-4138
Structural Aircraft Plate
34.000" overall length 24.600" overall width 0.056" material thickness
01-222-4139
Structural Aircraft Plate
1.200" overall length 0.560" overall width 0.125" material thickness
01-222-4140
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.200 in. lg, 2.600 in. w, 0.100 in. thk
01-222-4141
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 11.000 in. lg, 1.300 in. w, 0.032 in. thk
01-222-4142
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 24.440 in. lg, 1.780 in. w, 0.040 in. thk
01-222-4143
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 10.650 in. lg, 2.620 in. w, 0.040 in. thk
01-222-4144
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 2.330 in. lg, 1.360 in. w, 0.032 in. thk
01-222-4145
Structural Component Air Support
Used on f-15 acft. titanium alloy per per mil-t-9046type 3 composition c anl, 1.950 in. lg, 1.560 in. w, 0.040 in. thk
01-222-4146
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 2.680 in. lg, 1.300 in. w, 0.063 in. thk
01-222-4147
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 19.000 in. lg, 3.800 in. w, 0.050 in. thk
01-222-4148
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 7.800 in. lg, 3.600 in. w, 0.050 in. thk
01-222-4149
Aircraft Former
26.100" overall length 8.220" overall width 0.056" material thickness
01-222-4150
Aircraft Former
10.850" overall length 8.840" overall width 0.071" material thickness material per mms-1203 6al-6v-2sn
01-222-4151
Aircraft Former
25.300" overall length 8.860" overall width 0.071" material thickness material per mms-1203 6al-6v-2sn
01-222-4152
Aircraft Former
24.900" overall length 8.150" overall width 0.063" material thickness material per mms-1203 6al-6v-2sn
01-222-4153
Aircraft Former
8.750" overall length 7.800" overall width 0.045" material thickness
01-222-4154
Aircraft Former
20.100" overall length 5.750" overall width 0.056" material thickness
01-222-4155
Aircraft Former
25.600" overall length 7.800" overall width 0.045" material thickness
01-222-4156
Aircraft Former
8.900" overall length 7.250" overall width 0.063" material thickness material per mms 1203 6al-6v-2sn
01-222-4157
Aircraft Former
20.100" overall length 5.900" overall width 0.045" material thickness
01-222-4158
Aircraft Former
20.100" overall length 5.800" overall width 0.045" material thickness
01-222-4159
Aircraft Stringer
51.500" overall length 2.800" overall width 0.071" material thickness
01-222-4325
Structural Component Air Support
01-222-5090
Access Aircraft Door
Used on c-2a and e-2c aircraft. anodize surface treated
01-222-5458
Aircraft Wing Assembly
01-222-5470
Structural Component Air Support
01-222-5471
Structural Component Air Support
Type/model designation:GRMK5 aluminum alloy 2024-0 qq-a-250/5 matl 0.063 in. thk by 1.359 in. w by 1.766 in. lg
01-222-5472
Structural Component Air Support
Type/model designation:GRMK5 aluminum alloy 2024-0 qq-a-250/5 matl 0.063 in. thk by 1.359 in. w by 1.766 in. lg
01-222-5477
Structural Aircraft Panel
01-222-5478
Structural Aircraft Panel
01-222-5479
Structural Aircraft Panel
Used on av-8b acft.
01-222-5632
Access Aircraft Cover
01-222-5714
Structural Aircraft Plate
3.500" overall length 1.500" overall width 0.045" material thickness
01-222-5715
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 5.100 in. lg, 2.500 in. w, 0.045 in. thk
01-222-5716
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 5.000 in. lg, 4.500 in. w, 0.045 in. thk
01-222-5717
Structural Component Air Support
Used on f-15 acft.
