01-240-9839
Structural Aircraft Plate
01-240-9899
Aircraft Former
01-241-0169
Structural Component Air Support
Used on sentry f22 aircraft. adapter
01-241-0170
Structural Component Air Support
01-241-0172
Structural Aircraft Panel
01-241-0870
Aircraft Former
Used on aircraft f-18. 4.810" overall width p/o 25 mm gun pak
01-241-0998
Structural Aircraft Plate
01-241-0999
Structural Component Air Support
25.840" overall length 4.150" overall width 0.750" material thickness plastic polyurethane surface treated
01-241-1000
Structural Component Air Support
26.625" overall length 0.438" overall width 0.051" material thickness
01-241-1001
Structural Component Air Support
01-241-1002
Structural Component Air Support
01-241-1003
Aircraft Skin
Used on ch-53 helicopter.... heat treat per T3
01-241-1004
Fuselage Stringer
Aluminum alloy, qq-a-362 2024-T42; 0.032 in.thk;
01-241-1015
Thermal Special Purpo Insulation
01-241-1043
Aircraft Tip
Used on av8b attack aircraft. tip, wing
01-241-1656
Aircraft Fairing
01-241-1657
Aircraft Fairing
6.800" overall length 5.800" overall width 0.020" material thickness
01-241-1658
Structural Component Air Support
8.050" overall length
01-241-1661
Structural Aircraft Panel
Used on acft model p-3c. polycarbonate spec c-22-1115, ty 2; 30.800 in. lg; 12.530 in. w; 0.080 in. thk; 3 holes 0.250 in. min, 0.263 in. max; cutout along lg 0.500 in w; 0.470 in. dp; chamfered ends
01-241-1673
Aircraft Skin
Used on f-14 tomcat airplane.... anodize coating, mil-a-8625, TY2, CL1, epoxy polyamide primer GP111V1
01-241-1674
Aircraft Skin
01-241-1763
Structural Component Air Support
Used on B1-B. stop assembly; aluminum alloy; 3.54 in. nom o/a lg, 1.18 in. nom o/a h, 0.12 in. nom o/a thk, 2 mtg holes, 0.218 in. min, 0.229 in. max
01-241-2230
Structural Component Air Support
Used on c-130 acft. stiffener; p/o center fuselage lower structure, interior
01-241-2231
Structural Component Air Support
Used on c-130 acft. stiffener; p/o center fuselage lower structure, interior
01-241-2232
Structural Component Air Support
Used on c-130 acft. stiffener: p/o center fuselage lower structure, interior
01-241-2233
Structural Component Air Support
Used on c-130 acft. stiffener; p/o center fuselage lower structure, interior
01-241-2234
Structural Component Air Support
Used on c-130 acft. stiffener; p/o center fuselage lower structure, exterior
01-241-2235
Structural Component Air Support
Used on f-15 acft. bracket, u/o engine air inlet variable capture ramps
01-241-3017
Access Aircraft Door
Used on acft model e-3a. 1 ply dacron cloth BMS8-16-4 type ii
01-241-3043
Aircraft Fairing
Used on A-10.
01-241-3045
Structural Component Air Support
Used on acft model b-52. 4340 steel per bac mil-s-5000 forge per mil-f-7190 grade a; heat treat to 180, 000-200, 000 p.s.i; finish f-161; nha 25-524-0
01-241-3046
Structural Component Air Support
0.050" material thickness anodize surface treated
01-241-3047
Structural Component Air Support
Used on f-14a model aircraft. 0.050" material thickness primer epoxy-polyamide surface treated
01-241-3048
Structural Component Air Support
Used on f-14a model aircraft; aircraft, tomcat f-14. 0.050" material thickness primer epoxy-polyamide surface treated
01-241-3049
Structural Component Air Support
Used on f-14a model aircraft. 0.050" material thickness primer epoxy-polyamide surface treated
01-241-3060
Structural Aircraft Panel
Used on acft model e-3a.
01-241-3061
Structural Aircraft Panel
Used on acft model e-3a.
01-241-3087
Aircraft Former
15.900" overall length 11.600" overall width 0.100" material thickness
01-241-3088
Aircraft Former
01-241-3089
Aircraft Former
01-241-3090
Aircraft Former
01-241-3091
Aircraft Former
01-241-3092
Aircraft Former
Nuclear hardness criticial item
01-241-3099
Longeron
Used on acft model kc-135.
01-241-3103
Airfoil Rib
9.700" overall length 5.500" overall width 0.080" material thickness heat treat T4; finish srf-2.119; nha 65-3495
01-241-3104
Airfoil Rib
9.100" overall length 3.300" overall width 0.080" material thickness heat treat T4; finish srf-2.115; nha 65-3495
