01-215-9025
Aircraft Skin
01-215-9026
Aircraft Skin
01-215-9027
Aircraft Door
01-215-9080
Structural Aircraft Plate
01-215-9081
Structural Aircraft Plate
01-215-9082
Structural Aircraft Plate
01-215-9083
Structural Aircraft Plate
01-215-9084
Structural Aircraft Plate
01-215-9085
Structural Aircraft Plate
01-215-9086
Structural Aircraft Plate
Used on mcdonnell p/n 32-33091-301 support assy. type/model designation:f-4e/gy/ steel uns S17700 mil-s-25043 17-7ph annealed; matl 0.063 in. thk by 1.000 in. w by 1.500 in. lg
01-215-9087
Structural Aircraft Plate
01-215-9089
Structural Aircraft Plate
01-215-9090
Structural Aircraft Plate
01-215-9091
Structural Component Air Support
Used on 1560-00-871-7700. type/model designation:f-4e/gy/ steel uns S17700 mil-s-25043 17-7ph annealed; matl 0.063 in. thk by 2.500 in. w by 14.797 in. lg; l cross section; right appl
01-215-9092
Structural Component Air Support
Used on 1560-00-871-7701. type/model designation:f-4e/gy/ steel uns S17700 mil-s-25043 17-7ph annealed; matl 0.063 in. thk by 2.500 in. w by 14.797 in. lg; l cross section; left appl
01-215-9093
Structural Component Air Support
Used on mcdonnell p/n 32-33091-301 support assy. type/model designation:f-4e/gy/ steel uns S17700 mil-s-25043 17-7ph annealed; matl 0.063 in. thk by 2.250 in. w by 5.109 in. lg; right appl; l cross section
01-215-9094
Structural Component Air Support
Used on mcdonnell p/n 32-33091-301 support assy. type/model designation:f-4e/gy/ steel uns S17700 mil-s-25043 17-7ph annealed; math 0.063 in. thk by 2.250 in. w by 5.109 in. lg; left appl; l cross section
01-215-9097
Structural Aircraft Panel
Used on acft model c-5b. consists of 1 inner skin, 4 edging, 6 doubler, 1 core, 1 outer skin; nha 4F75412; located at fus sta 1208.00 to 1231.051
01-215-9098
Structural Aircraft Panel
Used on acft model c-5b. consist of 8 angle, 3 block, 4 seal, 2 splice strip, 2 panel, 1 fairlead, 6 pad, 1 edge member, 20 insert, misc hardware; located at fus sta 684.00 bl 24.00l
01-215-9100
Aircraft Skin
01-215-9101
Aircraft Skin
01-215-9102
Aircraft Skin
01-215-9103
Aircraft Skin
01-215-9104
Aircraft Door
01-215-9105
Aircraft Door
Used on 1560-00-780-7698 door assy. 10.797" overall length 7.203" overall width
01-215-9106
Aircraft Door
Used on 1560-00-780-7968 door assy. 21.000" overall length 7.984" overall width includes holes
01-216-0490
Structural Component Air Support
01-216-0611
Structural Aircraft Plate
81.000" overall length 19.000" overall width 0.750" material thickness nha 68A112127
01-216-0612
Structural Aircraft Plate
01-216-0613
Structural Aircraft Plate
01-216-0614
Structural Aircraft Plate
01-216-0615
Structural Aircraft Plate
01-216-0616
Structural Aircraft Plate
01-216-0617
Structural Aircraft Plate
01-216-0618
Structural Aircraft Plate
01-216-0619
Structural Aircraft Plate
01-216-0621
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2124-T851; supports actuator-foward ramp
01-216-0622
Structural Component Air Support
Used on c-5 aircraft. support-duct, fus sta 330.50 to 335.50; matl 2024-0 clad per qq-a-250/5; heat treat T42; size .032X6.0X7.0; opposite -102a; nha 4C22225
01-216-0623
Structural Component Air Support
Used on f-15 acft.
01-216-0630
Structural Aircraft Panel
Used on c-5 aircraft. 10.000" overall length 7.000" overall width part of -101a trim panel instl-flt sta
01-216-0631
Structural Aircraft Panel
Used on c-5 aircraft. matl LS32738g; part of -521c panel assembly; used on floor assembly-flight station
01-216-0635
Aircraft Former
10.600" overall length 2.000" overall width 0.020" material thickness matl sheet hastelloy x per ams 5536; part of -1, -503, -505 former installation-canted
