01-221-3908
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 4.600 in. lg, 1.800 in. w, 0.050 in. thk
01-221-3909
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 4.600 in. lg, 1.800 in. w, 0.050 in. thk
01-221-3910
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 2.800 in. lg, 1.200 in. w, 0.050 in. thk
01-221-3911
Structural Component Air Support
Used on f-15 aircraft. titanium per mil-t-9046 type 3 composition c anl, 3.000 in. lg, 1.800 in. w, 0.050 in. thk
01-221-3912
Structural Component Air Support
Used on f-15 acft.
01-221-3913
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 42.820 in. lg, 3.440 in. w, 0.071 in. thk
01-221-3916
Aircraft Former
9.100" overall length 7.250" overall width 0.063" material thickness material per mms 1203 6al-6v-2sn
01-221-3917
Aircraft Former
01-221-3918
Aircraft Former
Stock 68A332169-2001
01-221-3919
Aircraft Former
Stock 68A332169-2001
01-221-3920
Aircraft Skin
Used on F-15. 36.000" overall length stock IMT363A01-10003
01-221-3921
Aircraft Skin
Used on F-15. 3.250" overall length 1.450" overall width type 3 composition c annealed
01-221-5368
Structural Aircraft Plate
Used on acft model c/kc-135. nha 65-41416-1
01-221-6338
Structural Component Air Support
01-221-6355
Retractable Aircra Step Assembly
01-221-6502
Access Aircraft Door
Used on av-80b aircraft.
01-221-6503
Access Aircraft Door
Used on av-8b aircraft.
01-221-6504
Access Aircraft Door
Used on 1560-00-894-4186,aft doubler assy,nose landing gear.
01-221-6591
Structural Component Air Support
Aluminum qq-a-250/12 7075-T6; 0.040 in. thk; 1.40 in. wide; 1.90 in. lg; 2 holes 0.1645 in. min 0.1675 in. max dia; 1 hole 0.195 in. min 0.202 in. max dia; 2 holes 0.1645 in. min 0.1675 in. max dia
01-221-6604
Structural Component Air Support
Aluminum alloy, qq-a-250/13, 7075-0; 0.040 in. thk, 2.031 in. wd, 5.078 in. lg; aperature 1.000 in. dia; 2 mtg holes, 1 0.190-0.193 in. dia, 1 0.250-0.253 in. dia
01-221-6605
Structural Component Air Support
Aluminum alloy, qq-a-250/13, 7075-0; 0.040 in. thk, 1.969 in. wd, 4.953 in. lg; aperature 1.000 in. dia; 2 mtg holes, 1 0.190-0.193 in. dia, 1 0.250-0.253 in. dia
01-221-6609
Structural Component Air Support
Aluminum, qq-a-250/12, 7075-T6, 0.050 in. thk, 2.219 in. wd, 8.180 in. long; 8 holes along length, 2 holes 0.250-0.253 in. dia, 5 holes 0.190-0.193 in. dia, 1 hole 0.250-0.253 in. dia
01-221-6610
Structural Component Air Support
Titanium alloy, mil-t-9046, ty 3, comp c, 6al-4v; 0.063 in. thk, 3.641 in. wd, 3.781 in. lg; 3 holes along upper edge 0.250-0.253 in. dia; 2 holes along bottom edge, opposite corners, 0.190-0.193 in. dia; 4 holes along bottom edge, between other two, 0.164-0.167 in. dia
01-221-6611
Structural Component Air Support
Aluminum alloy, qq-a-250/12, 7075-T6; 0.040 in. thk, 2.210 in. wd, 7.391 in. lg; 4 holes along length 0.164-0.167 in. dia
01-221-6612
Structural Component Air Support
Aluminum alloy, qq-a-250/13, 7075-0; 0.040 in. thk, 2.031 in. wd, 5.078in. lg; aperature 1.000 in. dia; 2 mtg holes, 1 0.190-0.193 in. dia, 1 0.250-0.253 in. dia
01-221-6628
Structural Aircraft Plate
Type/model designation:f-4e/gy/ nickel-chromium alloy mil-n-7786 matt 0.032 in. thk by 1.500 in. w by 5.750 in. lg
01-221-6629
Structural Aircraft Plate
Used on 1560-01-089-4445. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/15, T6; matl 0.016 in. thk by 5.906 in. w by 21.797 in. lg
01-221-6632
Structural Aircraft Plate
Type/model designation:6M62-7-114 aluminum alloy 2024 qq-a-250/5 matl 0.050 in. thk by 13.795 in. w by 17.516 in. lg
01-221-6637
Structural Aircraft Plate
Type/model designation:f-4e/gy/ stainless steel 301 mil-s-5059 1/2 hard comp, matl 0.125 in. thk by 3.250 in. w by 4.500 in. lg
01-221-6638
Structural Aircraft Plate
Used on mfr pl75a871500-2019/-2029,panel,electrical. type/model designation:GRMK5 steel uns S30100 mil-s-5059 comp 301 1/2h; matl 0.080 in. thk by 1.516 in. w by 6.656 in. lg; mtg hole 0.290 in. min
01-221-6639
Structural Component Air Support
Used on 1560-00-238-4438. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-200/11, T6; made from mfr std 1M7634; 5.000 in.lg; right appl; channel cross sect.
01-221-6640
Structural Component Air Support
Used on 1560-00-231-4683. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-200/11, T6; made from mfr std 1M7634; 5.000 in. lg; left appl; channel cross sect.
01-221-6647
Structural Component Air Support
Used on 1560-00-441-6682 and 1560-00-106-6821 and 1560-00-140-2662. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, cond 0; made from std AND10134-1006; 9.609 in. lg; l cross sect; right appl
01-221-6648
Structural Component Air Support
Used on 1560-00-887-0168 and 1560-00-106-6822 and 1560-00-007-4500. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, cond 0; made from std AND10134-1006; 9.609 in. lg; l cross sect.; left appl
01-221-6649
Structural Component Air Support
Used on 1560-00-441-6682 and 1560-00-887-0166 and 1560-00-106-6821 and 1560-00-140-2662. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, cond 0; made from std AND10134-1006; 9.500 in. lg; l cross sect; right appl
01-221-6650
Structural Component Air Support
Used on 1560-00-887-0168 and 1560-00-106-6822 and 1560-00-007-4500. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, cond 0; made from std AND10134-1006; 9.500 in. lg; l cross sect.; left appl
01-221-6652
Structural Component Air Support
Used on 1560-00-887-0166 and 1560-00-106-6822 and 1560-00-007-4500. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13, cond 0; made from std and/0134-1006; 9.500 in. lg; left appl; l cross sect.
01-221-6653
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 5052-0 ww-t-700/4 matl 1.000 in. thk by 0.281 in. w by 5.703 in. lg
01-221-6654
Structural Component Air Support
Used on 1560-00-762-2849 and 1560-00-254-8653 and 1560-00-445-8570. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-200/13; made from mfr std 1M2378 by 7.797 in. lg; right appl
01-221-6655
Structural Component Air Support
Used on 1560-00-179-9190. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/15; matl 0.040 in. thk by 5.703 in. w by 20.906 in. lg; l cross section; right appl
01-221-6656
Structural Component Air Support
Used on 1560-00-800-2655 and 1560-00-944-5686 and 1560-00-983-4345. type/model designation:f-4e/gy/ plastic phenolic mil-p-15035 type fpg; matl 0.040 in. thk by 1.240 in. w by 1.594 in. lg
01-221-6657
Structural Component Air Support
Used on 1560-00-078-0792 and 1560-00-978-9924. type/model designation:f-4e/gy/ aluinum alloy 7178 qq-a-250/13 matl 0.050 in. thk by 3.234 in. w by 20.078 in. lg
01-221-6658
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy UNSR56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 4.750 in. lg; u cross section; right appl
01-221-6659
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a 8mn; matl 0.020 in. thk by 1.203 in. w by 4.406 in. lg; u cross section; left appl
01-221-6661
Structural Component Air Support
Type/model designation:f-4e/gy/ nickel-chromium alloy mil-n-7786; matl 0.071 in. thk by 0.062 in. w by 2.100 in. lg
01-221-6662
Structural Component Air Support
Used on mfr pl75a871500-2019/-2029,panel,electrical. type/model designation:GRMK5 aluminum alloy 2024 qq-a-250/5, cond 0; matl 0.063 in. thk by 2.156 in. w by 6.797 in. lg; l cross sect.; 3 mtg holes 0.195 in. min
01-221-6663
Structural Component Air Support
Used on mfr pl75a871500-2021,panel,electrical. type/model designation:GRMK5 aluminum alloy 2024 qq-a-250/5, cond 0; matl 0.050 in. thk by 1.391 in. w by 5.609 in. lg; l cross sect; 3 rivet holes
01-221-6664
Structural Component Air Support
Type/model designation:GRMK5 comp qty 72
