01-206-1928
Aircraft Former
01-206-1929
Aircraft Former
01-206-1930
Aircraft Former
01-206-1931
Aircraft Former
Used on aircraft c-18a.
01-206-1937
Aircraft Pylon
Used on aircraft model sh-60b. cognizant service:navy;
01-206-1938
Airfoil Rib
Used on aircraft model a-6.
01-206-1939
Aircraft Skin
Used on 1520-00-859-2670. 60.000" overall length 30.000" overall width with cutout latch
01-206-2274
Structural Component Air Support
0.063" material thickness
01-206-3608
Airfoil Rib
Used on F-15.
01-206-5111
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T4, 0.025 in. matl thk by 5.600 in. w by 39.500 in. lg; z cross section; w/ lightening holes; w/o rivet holes; mates w/ p/n 205-030-135-19a sill assy
01-206-5112
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T4, 0.025 in. matl thk by 4.600 in. w by 29.000 in. lg; z shape; w/o rivet holes
01-206-5113
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, T6; clevis design; 2.940 in. w by 3.51o in. lg; 0.6245 in. min 0.6255 in. max dia pin hole each fork; w/o mtg holes
01-206-5115
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, T6; extruded t shape; top right
01-206-5116
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, T6; extruded t shape; top right
01-206-5118
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, T6; 0.063 in. matl thk; 1.250 in. w both legs; 18.500 in. lg; l cross section; w/o rivet holes
01-206-5119
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, T6; 0.094 in. matl thk; 1.000 in. w both legs; 12.200 in. o/a lg; l cross section; w/o rivet holes
01-206-5120
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11, l cross section; made from p/n 205-030-240-3; w/o rivet holes
01-206-5121
Structural Component Air Support
Used on 1520-01-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5; v cross section; bow design; made from p/n 205-030-213-3; w/o rivet holes
01-206-5122
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to, 0.040 in. matl thk by 2.000 in. w by 39.000 in. lg, u cross section; w/o holes
01-206-5123
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d made from p/n 205-030-161-13 cap assy; component qty 8; w/o rivet holes in leg of t angle p/n 205-030-161-3 cap
01-206-5124
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d made from p/n 205-030-161-15 cap beam; l cross section; 0.125 in. matl thk; w/o rivet holes
01-206-5125
Structural Component Air Support
Used on 1520-00-859-2670. made from p/n 205-030-161-9 cap assy, comp qty 3; l cross section; 62.000 in. o/a lg; w/o rivet holes in leg
01-206-5126
Aircraft Skin
Used on 1520-00-859-2670. 39.500" overall length 5.600" overall width
01-206-5127
Aircraft Skin
Used on 1520-00-859-2670. 26.000" overall length 5.500" overall width
01-206-5129
Fuselage Stringer
Used on 1520-00-859-2670. 86.700" overall length 12.600" overall width 0.050" material thickness bow shape; u cross section; 15 lightening holes; w/o rivet holes
01-206-5131
Fuselage Stringer
Used on 1520-00-859-2670. 92.500" overall length 6.500" overall width 0.032" material thickness l cross section; 15 lightening holes; w/o rivet holes; right hand design
01-206-5132
Fuselage Stringer
Used on 1520-00-859-2670. 23.800" overall length 6.800" overall width 0.050" material thickness bow shape; w/2 lightening holes; w/o rivet holes
01-206-5133
Fuselage Stringer
Used on 1520-00-859-2670. 54.000" overall length 6.000" overall width 0.050" material thickness v cross section; w/o rivet holes; left hand
01-206-5134
Fuselage Stringer
Used on 1520-00-859-2670. 54.000" overall length 6.000" overall width 0.050" material thickness v cross SECTI0n; w/o rivet holes; right hand
01-206-5192
Access Aircraft Door
Used on acft model b-1b. consist of 1 door, 2 seal; nha L3010829; located on yf 442 to 462; used on fuel tank access door assy
01-206-5193
Access Aircraft Door
Used on acft model b-1b. consist of 2 seal, 1 door; opposite p/n -011; nha L3010826; located on yf 432 to 452; used on upper fuel tank access door assy
01-206-5194
Access Aircraft Door
Used on acft model b-1b.
01-206-5263
Structural Component Air Fitting
3.300" overall length 2.700" overall width 0.750 " material thickness nlg fwd door hinge pin assy
01-206-5286
Structural Aircraft Plate
Used on acft model kc-135. al aly sheet 2024-T3 per qq-a-250/4; stock 0.063 thick; yellow chem film per mil-f-14072; nha 82-01020
01-206-5287
Structural Aircraft Plate
26.000" overall length 21.000" overall width 0.160" material thickness nha L3226360
01-206-5288
Structural Component Air Support
Used on f-16c/d usaf aircraft. xmade from -7 forging; material-of forging-7075-T73 per qq-a-367; locationfs 380.79; total length-14.22 in; nha-16B6557-19; eff on-5c 0178, 0180, 0182, 0188, 0190, 0192, 0194, 202, 204, 206, 208, 212, 214, 216, 218, 220, 222, 224, 226, 228, 231, and 233-9999
01-206-5289
Structural Component Air Support
Used on acft model kc-135. consist of 1 guide plate, 1 tee, 1 stiffener, 1 clip, 1 support, 3 bolt, 3 collar; nha 458-52215
01-206-5290
Structural Component Air Support
Used on acft model kc-135. 7075-T73 alum die forging per BMS7-186; finish f-2.47; nha 65C18597
01-206-5291
Structural Component Air Support
Used on acft model kc-135. consist of 1 support plate, 8 nutplate; nha 458-54716
01-206-5292
Structural Component Air Support
Used on acft model kc-135. consist of 1 support, 3 nutplate; nha 39-28101
01-206-5293
Structural Component Air Support
Used on kc-135 aircraft.
01-206-5294
Structural Component Air Support
Used on kc-135 aircraft.
01-206-5295
Structural Component Air Support
Used on kc-135 aircraft.
01-206-5296
Structural Component Air Support
Nha L3226360
01-206-5298
Structural Aircraft Panel
C/o 2 facesheet, 10 honeycomb core; nha L3226780
01-206-5310
Aircraft Former
01-206-5311
Aircraft Former
01-206-5312
Aircraft Former
01-206-5313
Aircraft Former
01-206-5314
Aircraft Former
