01-517-2637
Structural Aircraft Plate
Used on f-22 raptor. blade seal made from 1 5HW84783-108 bonded assembly
01-517-2638
Structural Aircraft Plate
Used on f-22 raptor. insert-bonded part, upper aileron seal opposite -114
01-517-2640
Aircraft Hinge
Used on f-22 raptor. hinge
01-517-2642
Structural Aircraft Panel
Used on f-22 raptor. insert wind swept surface critical item; opposite -124; m/o: carbon/bmi composite material
01-517-2644
Structural Aircraft Panel
Used on f-22 raptor. 21.000" overall length 43.000" overall width forward skin panel wind swept surface critical item; opposite -108; dim. are stock material; m/o: carbon/bmi & glass/bmi composite material
01-517-2645
Structural Aircraft Panel
Used on f-22 raptor. 16.000" overall length 9.000" overall width lower panel wind swept surface critical item; opposite -110; c/o: 5HW84753-113 lower panel; m/o: carbon/bmi, glass/bmi, bmi composite material; dim. are stock size
01-517-2647
Structural Aircraft Panel
Used on f-22 raptor. 16.000" overall length 9.000" overall width lower panel wind swept surface critical item; dim. are stock material; opposite -109; c/o: 5HW84753-114 lower panel; m/o: carbon/bmi, glass/bmi, bmi composite material
01-517-2648
Structural Aircraft Panel
Used on f/a-22 raptor. slin panels-bond part, lower opposite -107
01-517-2651
Structural Aircraft Panel
Used on f/a-22 raptor. 10.000" overall length 16.000" overall width skin panel-forward part of skin panels-bond part, lower
01-517-2653
Structural Aircraft Panel
Used on f-22 raptor. insert wind swept surface critical item; opposite -112; m/o: carbon/bmi composite material
01-517-2654
Structural Aircraft Plate
Used on f-22 raptor. insert-bonded part, ukpper aileron seal opposite -113
01-517-2655
Aircraft Skin
Used on f-22 raptor. skin panel, fwd, bond part opposite 5HW84822-109
01-517-2660
Structural Aircraft Plate
Used on f-22 raptor. insert-bonded part lower aileron seal opposite -123
01-517-2662
Aircraft Fairing
Used on f-22 raptor. blade seal wind swept surface critical item; opposite -122; m/f: -119 bonded assy; m/o: carbon/bmi composite material
01-517-2664
Aircraft Fairing
Used on f-22 raptor. blade seal wind swept surface critical item; opposite -121; m/f: -120 bonded assy; m/o: carbon/bmi composite material
01-517-2667
Structural Aircraft Panel
Used on f/a-22 raptor. skin panels-aft bond part, lower
01-517-2668
Structural Aircraft Panel
Used on f-22 raptor. 21.000" overall length 43.000" overall width aft skin panel wind swept surface critical item; opposite -209; dim. are stock material; m/o: carbon/bmi & glass/bmi composite material
01-517-2670
Structural Component Air Fitting
Used on f-22 raptor. 4.000" overall length 6.000" overall width fitting-actuator no. 1, leading edge-wing box consists of 1 5HW82511-147 fitting; 4 4591-001 bushings
01-517-2671
Structural Component Air Fitting
Used on f-22 raptor. 4.000" overall length 6.000" overall width fitting-actuator no. 1, leading edge-wing box consists of 1 5HW82511-148 fitting; 4 4591-001 bushings
01-517-2672
Structural Component Air Support
Used on f-22 raptor. gang channel
01-517-2679
Structural Aircraft Panel
Used on f-22 raptor. panel-bonded, inboard, lower, leading edge, fixed; panel, skin
01-517-2680
Structural Aircraft Panel
Used on f-22 raptor. panel, skin 105 opposite
01-517-2681
Structural Aircraft Panel
Used on f-22 raptor. skin panel wind swept surface critical item; m/o: carbon/bmi & glass/bmi composite materials
01-517-2683
Structural Aircraft Panel
Used on f-22 raptor. panel, bonded c/o ref smoothness, mds index, bullnose loft, surface texture, std dod barcode, ident marking, temp protection, raw matl., 2 label, bkm carbon/bmi
01-517-2685
Structural Aircraft Panel
Used on f-22 raptor. panel, bonded c/o refs smoothness, mds index, bullnose loft, surface texture, std dod barcode, ident. marking, temp protection, raw matl., 2 label, bkm carbon/bmi
01-517-2687
Aircraft Hinge
Used on f-22 raptor. 8.000" overall length 7.000" overall width hinge fitting fracture critical catagory 1; opposite -106; dim. are stock material; m/o: 6al-4v eli, titaniium, te cont ba, ma-ti, st-plate
01-517-2688
Structural Aircraft Panel
Used on f-22 raptor. panel, skin opposite -106
01-517-2692
Structural Aircraft Panel
Used on f-22 raptor. panel assy opposite -222; c/o 6 rivets, 4 pin, 3 nut, 4 collar, 1 shim, 2 labels, 1 splice, (ref smoothness, std dod barcode, ident. marking, raw matl) , 1 panel
01-517-2715
Aircraft Spar
Lwr rear spar cap make from 160D611316-11 extr (2024-T3511)
01-517-2802
Airfoil Rib
18.000" overall length 14.000" overall width 0.080" material thickness rib assy, airfoil c/o 1 rib, 1 doubler (7.4 x 6.0 x 0.071) , 1 bracket (7.2 x 2.6 x 0.071) , 1tee (16.0 x .080) , 1 support, 1 radius blk., 1 clip, 1 shim, 2 angles; heat treat 0 & T6; used on -6, -8, -10 rh
01-517-2803
Airfoil Rib
19.000" overall length 14.000" overall width 0.080" material thickness rib assy, airfoil used on -6, -8, -10 rh; c/0 1 rib, 1 doubler (7.4 x 6.0 x 0.071) , 1 bracket (7.2 x 2.6 x 0.071) , 1 tee (16.0 x 0.080) , 1 cover (6.0 x 6.0 x 0.71) , 1 support, 1 radius blk., 1 clip
01-517-2806
Airfoil Rib
19.000" overall length 14.000" overall width 0.080" material thickness rib assy, airfoil used on -5, -7, -9 lh; consist of 1 bracket (7.2 x 2.6 x .071) , 1 tee (16.0 x .080) , 1 support, 1 radius blk., 1 rib (19.0 x 14.0 x .080) , 1 doubler (7.4 x 6.0 x .071)
01-517-2834
Airfoil Rib
Rib, airfoil
01-517-2872
Structural Aircraft Plate
10.300" overall length 4.400" overall width 0.080" material thickness plate used on 160D117101-1, -3, -5 windshield assy; heat treat T6; alcd sheet; dimensions are stocksize
01-517-2873
Airfoil Rib
Rib, airfoil
01-517-2880
Airfoil Rib
Rib, airfoil
01-517-2886
Airfoil Rib
Rib, airfoil
01-517-2889
Airfoil Rib
Rib, airfoil
01-517-2960
Structural Component Air Bracket
1.950" overall length 1.750" overall width
01-517-3002
Structural Component Air Support
Used on boeing 707 aircraft. side cowl panel hinge
01-517-3004
Access Aircraft Door
Used on boeing 707 aircraft.
01-517-3082
Radome
Used on c-130 acft.
01-517-3091
Structural Aircraft Panel
Used on f-22a raptor. access panel wind swept surface critical item; composite material: carbon/epoxy
01-517-3093
Structural Aircraft Panel
Used on f-22 raptor. access panel wind swept surface critical item; carbon/epoxy composite material
01-517-3094
Structural Aircraft Panel
Used on f-22a raptor. 29.516" overall length access panel composite material made from carbon
01-517-3130
Airfoil Rib
58.000" overall length 23.000" overall width 2.500" material thickness rib heat treat T7351; al pl
01-517-3132
Structural Aircraft Panel
01-517-3133
Structural Aircraft Panel
Nha -516
01-517-3493
Access Aircraft Door
Used on UH2A/B.
01-517-3600
Bleed Air Duct Assembly
