01-272-9649
Structural Aircraft Plate
Used on acft model kc-135. 7075-T6 sh clad per qq-a-287 T6 temp; finish SRF2.115; 42.0 in lg, 12.0 in wd, 0.025 in thk; nha 65-2494
01-272-9651
Structural Aircraft Plate
Used on acft model kc-135. 7075-0 sh per qq-a-283, 0 temp; heat treat T6; finish srf 2.30; 43.1 in lg, 26.7 in wd, 0.063 in thk; nha 65-2494
01-272-9653
Structural Aircraft Plate
Used on acft model kc-135. 7075-T6 sh per qq-a-283, T6 temp; finish srf 2.30; 36.9 in lg, 14.6 in wd, 0.063 in thk; nha 65-2494
01-272-9655
Structural Aircraft Plate
Used on C-141.
01-272-9656
Structural Aircraft Plate
Used on C-141.
01-272-9657
Structural Aircraft Plate
Used on C-141.
01-272-9658
Structural Aircraft Plate
Used on C-141.
01-272-9659
Structural Aircraft Plate
Used on F-15.
01-272-9661
Structural Component Air Support
Used on acft model kc-135. steel sheet annealed 4130an per qq-s-685 or 8630 an-s-12; finish f-1.20; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516
01-272-9663
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish srf-2.30; 76.0 in lg, 5.60 in wd, 0.190 in thk; nha 65-2494; opposite -21
01-272-9664
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish srf-2.30; 76.0 in lg, 5.60 in wd, 0.190 in thk; nha 65-2494; opposite -40
01-272-9665
Structural Component Air Support
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; finish SRF2.30; 76.0 in lg, 5.60 in wd, 0.190 in thk; nha 65-2494; opposite -39
01-272-9667
Structural Component Air Support
Used on acft model kc-135. 7075-0 extrusion per qq-a-277, 0 temp; make from bac 1505-10023 by 17.0 ; opposite -3015; heat treat T6; finish srf-2.30; nha 65-2494
01-272-9669
Structural Component Air Support
Used on acft model kc-135. 7075-0 extrusion per qq-a-277, 0 temp; heat treat T6; stock BAC1505-100230 by 17.0; opposite -3035; finish srf-2.30
01-272-9673
Aircraft Former
45.000" overall length 2.000" overall width 0.032" material thickness opp -3118; nha 65-2516
01-272-9674
Aircraft Former
45.000" overall length 2.000" overall width 0.032" material thickness opp -3117; nha 65-2516
01-272-9675
Aircraft Former
Used on KC-135. extrusion; bac 1503-100026 by 7.90 in. lg; nha 65-2494
01-272-9676
Aircraft Former
Used on KC-135. finish SRF2.30; bac 14900-2615 by 8.1 in.; nha 65-2494
01-272-9677
Aircraft Former
Used on C-141. frame
01-272-9678
Aircraft Former
35.000" overall length 5.000" overall width 0.040" material thickness nha 3P21601
01-272-9679
Aircraft Former
8.000" overall length 2.000" overall width 0.071" material thickness
01-272-9680
Aircraft Former
14.000" overall length 2.000" overall width 0.071" material thickness
01-272-9681
Aircraft Former
Used on C-141. frame
01-272-9682
Aircraft Former
Used on C-141. frame
01-272-9683
Aircraft Former
8.000" overall length 2.000" overall width 0.071" material thickness ht tr T6; nha nha 3P21602 & 3P21601
01-272-9686
Aircraft Skin
Used on f-15 aircraft.
01-272-9687
Aircraft Stringer
01-273-0108
Aircraft Fairing
Used on acft model f/a18a,tf/a18a. 0.060" material thickness
01-273-0112
Airfoil Rib
Used on aircraft,ta-4f. 0.063" material thickness
01-273-0113
Aircraft Skin
Aluminum alloy, qq-a-250/13 7075-T6; 0.032 in. thk
01-273-0114
Aircraft Skin
Aluminum alloy, qq-a-250/13 7075-T6; 0.032 in. thk
01-273-0115
Aircraft Skin
33.830 in. lg; 2.906 in. h; 0.080 in. thk; 121 holes 0.097 in. min, 0.102 in. max dia
01-273-0116
Aircraft Skin
44.832 in. lg; 2.606 in. w; 3.490 in. h; u shaped; two hundred
01-273-0128
Thermal Special Purpo Insulation
01-273-1742
Structural Component Air Support
Aluminum alloy, qq-a-250/11 6061-T6; 0.020 in. thk; color white no. 17875 fed std 595
01-273-1743
Structural Component Air Support
01-273-1745
Airfoil Rib
0.040" material thickness primer epoxy-polyamide surface treated
01-273-1746
Airfoil Rib
Used on f-14a tomcat airplane. 0.063" material thickness anodize surface treated
01-273-1747
Airfoil Rib
Used on f-14a tomcat airplane. 0.032" material thickness anodize surface treated
01-273-1760
Thermal Special Purpo Insulation
Tape two edges on both sides
01-273-1761
Thermal Special Purpo Insulation
Tape pads both sides
01-273-1762
Thermal Special Purpo Insulation
01-273-1949
Structural Aircraft Plate
2.750" overall length 1.400" overall width 0.190" material thickness E4130 stl
01-273-1950
Structural Aircraft Plate
Used on F-15.
01-273-1951
Structural Aircraft Plate
Used on F-15.
01-273-1952
Aircraft Fairing
01-273-1953
Structural Component Air Support
Nha 35-35400
01-273-1958
Longeron
Used on F-15. nha 68A332000; lower
01-273-1960
Aircraft Skin
Used on f-15 aircraft. skin-aircraft, lwr ml keel longeron fs 552.000 to fs 565.330; nha 68A324000
01-273-1961
Aircraft Skin
Used on acft model kc-135. clad 2024-0 sh per qq-a-362, 0 temper; heat treat T4; finish srf-2.130; 38.0 in lg, 22.0 in wd, 0.040 in thk; nha 65-31682
