01-205-8445
Aircraft Former
01-205-8446
Aircraft Former
01-205-8447
Aircraft Former
01-205-8448
Aircraft Former
01-205-8449
Aircraft Former
01-205-8450
Aircraft Former
01-205-8451
Aircraft Former
01-205-8452
Aircraft Former
01-205-8453
Aircraft Former
01-205-8454
Aircraft Former
01-205-8455
Aircraft Former
01-205-8456
Aircraft Former
01-205-8457
Aircraft Former
01-205-8458
Aircraft Former
01-205-8459
Aircraft Former
01-205-8460
Aircraft Former
01-205-8461
Aircraft Former
01-205-8471
Aircraft Spar
54.500" overall length 6.800" overall width 0.050" material thickness ht PS15520
01-205-8492
Aircraft Door
01-205-9446
Structural Component Air Support
0.035" material thickness
01-206-0561
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024, T4; right hand tab; 8.000 in. lg by 5.500 in. w; w/o holes
01-206-0562
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024, T4; left hand tab; 8.000 in. lg by 5.500 in. w; w/o holes
01-206-0563
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13; 0.025 in. matl thk by 13.900 in. w by 25.000 in. lg; c shape; l cross section, 16 holes equally spaced to match p/n 204-030-814-45 door; w/o rivet hole
01-206-0564
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d daluminum alloy 2024 qq-a-250/5, to; 0.025 in. thk by 2.000 in. w by 88.000 in. lg; c shape; modified l cross section; 2 c-holes; w/o attaching holes; makes 2 parts; has excess tooling matl each end
01-206-0565
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d rdalgsynthetic repair parts frg program aluminum alloy 7075 qq-a-250/13, to; 0.032 in. thk by 7.000 in. w by 22.000 in. lg; c shape; u cross section; w/o holes
01-206-0566
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.020 in. thk by 2.800 in. w by 18.000 in. lg; ski shape; l cross section; w/o holes; right hand bow
01-206-0567
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.020 in. thk by 2.800 in. w by 18.000 in. lg; ski shape left hand bow, l cross section; w/o holes
01-206-0568
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.020 in. thk by 1.800 in. w by 15.000 in. lg; left hand bow ski shape; l cross section; w/o holes
01-206-0571
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.020 in. thk by 6.000 in. w by 32.000 in. lg; left hand bow ski shape; u cross section; w/o holes
01-206-0572
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.025 in. thk by 5.000 in. w by 11.000 in. lg; l cross section; w/o holes; left hand design
01-206-0573
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.025 in. thk by 5.000 in. w by 11.000 in. lg; l cross section; w/o holes; right hand design
01-206-0574
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.040 in. thk by 8.000 in. w by 14.000 in. lg; triangular cross section w/ flanges; left hand design; w/o holes
01-206-0575
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.040 in. thk by 8.000 in. w by 14.000 in. lg; triangular cross section w/ flanges; right hand design; w/o holes
01-206-0576
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, T4; special shape fscm 97499 std 40-005; 2.700 in. o/a lg; w/o holes
01-206-0577
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, T4; special shape fscm 97499 std 40-005; 3.500 in. lg; w/o holes
01-206-0684
Structural Aircraft Plate
Used on kc-135 aircraft.
01-206-0695
Aircraft Former
01-206-0696
Aircraft Former
01-206-0697
Aircraft Former
01-206-0698
Aircraft Former
01-206-0699
Aircraft Former
01-206-1375
Aircraft Windshield Panel
01-206-1582
Access Aircraft Door
Used on aircraft model sh-60b,lamps mark 3.
01-206-1898
Structural Aircraft Plate
12.000" overall length 8.000" overall width 0.020" material thickness
01-206-1899
Landing Gear Aircraft Fairing
Used on aircraft model sh-60b. cognizant service:navy;
01-206-1902
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d titanium alloy uns R58820 mil-t-9046, class 2 tit; 0.125 in. matl thk by 4.900 in. w by 6.900 in. lg; w/o holes
01-206-1903
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d titanium alloy uns R58820 mil-t-9046, class 2 tit; 0.125 in. matl thk by 5.630 in. w by 5.760 in. lg; left hand appl; w/o holes
01-206-1904
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d titanium alloy uns R58820 mil-t-9046, class 2 tit; 0.125 in. matl thk by 5.630 in. w by 5.760 in. lg; right hand appl; w/o holes
01-206-1921
Structural Aircraft Panel
Part of -103b trim panel instl-floating ceiling, flight sta; c/o: -107a filler (2) , -109a filler (1) , -121b filler (1) , -127b filler (1) , -129a filler (1) , -111b panel (1) , grommet (1)
01-206-1924
Structural Aircraft Panel
Used on c-5b aircraft. part of -128a walkway installation-cargo inspection, aft fus, fs 1884 to fs 1964; c/o: -106b core (1) , -108b face sheet (1) , -110b face sheet (1) , -112a doubler (1) , -132a angle (1)
