01-222-1818
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.350 in. lg, 2.000 in. w, 0.050 in. thk
01-222-1819
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.350 in. lg, 2.000 in. w, 0.050 in. thk
01-222-1820
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 2.000 in. lg, 1.500 in. w, 0.040 in. thk
01-222-1821
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.200 in. lg, 3.300 in. w, 0.045 in. thk
01-222-1822
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e, 4.200 in. lg, 3.300 in. w, 0.045 in. thk
01-222-1823
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 3.500 in. lg, 1.500 in. w, 0.045 in. thk
01-222-1828
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 7.800 in. lg, 3.6000 in. w, 0.050 in. thk
01-222-1829
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 5.000 in. lg, 2.500 in. w, 0.045 in. thk
01-222-1830
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
01-222-1879
Aircraft Door
Used on 1560-00-074-3201 and 1560-00-874-7338. 6.000" overall length 4.000" overall width
01-222-2785
Structural Aircraft Plate
Used on 1560-00-074-3201 and 1560-00-874-7338. 5.391" overall length 5.391" overall width 0.050" material thickness doubler door assy, drag chute; f-4e/gy
01-222-2786
Structural Aircraft Plate
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5 matl 0.050 in. thk by 5.391 in. w by 5.391 in. lg
01-222-2787
Structural Aircraft Plate
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 2024-0 qq-a-250/15 matl 0.040 in. thk by 3.797 in. w by 4.297 in. lg
01-222-2789
Structural Component Air Support
01-222-2790
Structural Component Air Support
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 5052 qq-a-250/8 matl 0.063 in. thk by 5.391 in. w by 5.391 in. lg
01-222-2791
Structural Component Air Support
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 5052 qq-a-250/8 matl 0.063 in. thk by 5.391 in. w by 5.391 in. lg
01-222-2792
Structural Component Air Support
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5 matl 0.040 in. thk by 14.203 in. w by 19.000 in. lg
01-222-2793
Structural Component Air Support
Used on 1560-00-074-3201 and 1560-00-874-7338. type/model designation:f-4e/gy/ aluminum alloy 2024-0 qq-a-250/5 matl 0.071 in. thk by 3.000 in. w by 2.203 in. lg
01-222-2794
Structural Component Air Support
01-222-2798
Aircraft Former
01-222-2896
Access Aircraft Door
Used on acft model 1f-111.
01-222-2953
Structural Component Air Bracket
01-222-2954
Aircraft Scoop
C/o 2 duct half, flange
01-222-2965
Structural Aircraft Plate
8.650" overall length 1.750" overall width 1.500" material thickness
01-222-2966
Structural Aircraft Plate
7.450" overall length 2.000" overall width 1.500" material thickness
01-222-2967
Structural Aircraft Plate
8.500" overall length titanium 6al-4v ams 4935 annealed, stock 1MT300A01-10002
01-222-2968
Structural Aircraft Plate
6.800" overall length 4.500" overall width 0.125" material thickness material per mms 1203 6al-6v-2sn
01-222-2969
Structural Aircraft Plate
6.800" overall length 4.500" overall width 0.125" material thickness material per mms 1203 6al-6v-2sn
01-222-2970
Structural Aircraft Plate
6.800" overall length 2.600" overall width 0.125" material thickness material per mms-1203 6al-6v-2sn
01-222-2971
Structural Aircraft Plate
18.150" overall length 2.200" overall width 0.025" material thickness
01-222-2972
Structural Aircraft Plate
4.600" overall length 4.600" overall width 0.080" material thickness
01-222-2973
Structural Aircraft Plate
2.600" overall length 2.000" overall width 0.050" material thickness
01-222-2974
Structural Aircraft Plate
6.500" overall length titanium per 1MT300A01-10004
01-222-2975
Structural Aircraft Plate
6.500" overall length titanium per 1MT300A01-10004
01-222-2976
Structural Aircraft Plate
4.188" overall length 1.500" overall width 0.375" material thickness
01-222-2977
Structural Aircraft Plate
3.000" overall length 1.000" overall width 0.063" material thickness
01-222-2978
Structural Aircraft Plate
Used on f-15 acft.
01-222-2979
Structural Component Air Support
Used on acft model f-4a. 7075-T6 per qq-a-277, cond T6; IM2458 by 13.70; opposite p/n -12; nha 32-19416; located at bl 59.560
01-222-2980
Structural Component Air Support
Used on acft model b-1b. c/o 1 bracket, 4 nutplates, rivets as required; located yf 299 to yf 308; nha L5305134-101; opposite -002
01-222-2981
Structural Component Air Bracket
Used as utility light bracket; c/o: 1 bracket, 4 nutplates, rivets a/r; opposite -001; nha L5305134-102
01-222-2982
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition e anl, 4.500 in. lg, 2.700 in. w, 0.045 in. thk
01-222-2983
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 7.000 in. lg, 9.250 in. w, 0.028 in. thk
01-222-2984
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 7.000 in. lg, 9.250 in. w, 0.028 in. thk
01-222-2985
Structural Component Air Support
Used on f-15 acft. steel per mil-s-5059 composition 301 1/4 h, 4.000 in. lg, 3.500 in. w, 0.050 in. thk
01-222-2986
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 2.000 in. lg, 1.500 in. w, 0.040 in. thk
01-222-2987
Structural Component Air Support
Used on f-15 acft. steel per mil-s-5059 composition 301 1/4 h, 4.000 in. lg, 3.500 in. w, 0.050 in. thk
01-222-2988
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 1.950 in. lg, 1.260 in. w, 0.040 in. thk
01-222-2989
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 4.500 in. lg, 3.500 in. w, 0.050 in. thk
01-222-2990
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 4.500 in. lg, 3.500 in. w, 0.050 in. thk
01-222-2991
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 4.500 in. lg, 3.500 in. w, 0.050 in. thk
