01-488-4576
Aircraft Hinge
Used on f-22 raptor. c/o 1 hinge, 1 bushing
01-488-4577
Aircraft Hinge
Used on f-22 raptor. 12.000" overall length 6.000" overall width 3.000" material thickness hinge, assy of dim. are stock material; c/o: -113 hinge & LS3859F6P9 bushing (1) ; m/o: 6al-4v eli titanium beta ann plate
01-488-4578
Structural Component Air Bracket
01-488-4579
Structural Component Air Bracket
Used on f-22 raptor. 5.000" overall length 2.000" overall width 0.063" material thickness bracket opposite -204; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4580
Structural Component Air Bracket
Used on f-22 raptor. 5.000" overall length 2.000" overall width 0.063" material thickness bracket dim. are stock material; opposite -203; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4581
Aircraft Hinge
Used on f-22 raptor. 8.000" overall length 5.000" overall width 3.000" material thickness hinge, assembly of dim. are stock material; c/o: -115 hinge & LS3859F6P7 bushing; m/o: 6al-4v eli titanium beta ann plate
01-488-4582
Structural Component Air Bracket
Used on f-22 raptor. 15.000" overall length 5.000" overall width 0.063" material thickness bracket dim. are stock material; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4583
Structural Component Air Bracket
Used on f-22 raptor. 14.000" overall length 6.000" overall width 0.063" material thickness bracket dim. are stock material; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4584
Structural Component Air Bracket
Used on f-22 raptor. 8.000" overall length 3.000" overall width 0.063" material thickness bracket dim. are stock material; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4585
Structural Component Air Bracket
Used on f-22 raptor. 6.000" overall length 5.000" overall width 0.063" material thickness bracket dim. are stock material; m/o: 6al-4v (ab-1) , ann titanium sheet
01-488-4586
Structural Component Air Bracket
Used on f-22 raptor. 0.100" material thickness bracket dim. is stock material; m/o: 6al-4v (ab-1) ann titanium sheet
01-488-4587
Structural Component Air Bracket
Used on f/a-22 raptor. 7.000" overall length 3.000" overall width 0.100" material thickness bracket alum sheet; heat treat 0
01-488-4588
Structural Aircraft Panel
Used on f/a-22 raptor. panel, tire ann tit. sheet 6al-4v (ab-1)
01-488-4589
Structural Aircraft Panel
Used on f/a-22 raptor. panel, tire ann. titanium sheet, 6al-4v (ab-1)
01-488-4590
Structural Component Air Bracket
Used on f/a-22 raptor. 6.000" overall length 3.000" overall width 0.100" material thickness bracket alum sheet; heat treat 0; c/o urethane (ar)
01-488-4591
Structural Component Air Bracket
Used on f/a-22 raptor. 4.000" overall length 4.000" overall width 0.100" material thickness alum sheet; heat treat 0
01-488-4599
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 3.000" overall width 0.063" material thickness bracket ann tit. 6al-4v (ab-1)
01-488-4621
Structural Component Air Support
Used on f/a-22 raptor. 4.000" overall length 4.000" overall width 4.000" material thickness sprt, assy of c/o 1 (-105) 2 bushing; plate; -111 can be used for all replacements
01-488-4622
Structural Component Air Support
Used on f-22 raptor. 4.000" overall length 4.000" overall width support, assembly of durability critical item; dim. are stock material; c/o: -101 container support & NAS77A6-017 bushing (2) ; m/o: 2124-T8151 aluminum plate
01-488-4624
Structural Component Air Support
Used on f/a-22 raptor. 2.000" overall length 2.000" overall width 2.000" material thickness support 17-4ph soln treated steel bar; form, fit, function
01-488-4625
Bleed Air Duct Assembly
Used on f/a-22 raptor. F119-pw-100 engine
01-488-4628
Structural Component Air Support
Used on f/a-22 raptor. 1.500" overall length 0.025" material thickness support-harness, power distribution center
01-488-4629
Structural Component Air Bracket
01-488-4631
Structural Component Air Support
Used on f/a-22 raptor. 2.000" overall length 2.000" overall width 1.750" material thickness support 17-4ph soln treated steel bar
01-488-4635
Access Aircraft Cover
Used on f/a-22 raptor. cover consists of: 1 5HB49126-103 cover; 18 CA2210-08r rings
01-488-4638
Structural Component Air Bracket
Used on f-22 raptor. 2.000" overall length 4.570" overall width 1.000" material thickness bracket dim. are stock material; m/f: 2024-T851 aluminum plate
01-488-4640
Structural Component Air Bracket
Used on f/a-22 raptor. 1.000" overall length 3.000" overall width 0.050" material thickness bracket alum sht; heat treat T81
01-488-4644
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 2.000" overall width 1.250" material thickness bracket heat treat T851; plate; dim. are stocksize
01-488-4647
Structural Component Air Bracket
Used on f-22 raptor. bracket-coolant loop, main weapons bay
01-488-4648
Structural Component Air Support
Used on f/a-22 raptor. support, assy of c/o 2 rivet, 1 bracket assy, 1 block, 1 (1 oz. sealant)
01-488-4650
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 2.000" overall width 0.080" material thickness bracket heat treat 0; alum sht
01-488-4651
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 2.000" overall width 0.063" material thickness bracket alum. sheet; heat treat 0
01-488-4652
Structural Component Air Support
Used on f/a-22 raptor. 4.000" overall length 3.000" overall width 2.500" material thickness support heat treat T851; alum plate
01-488-4653
Structural Aircraft Plate
Used on f/a-22 raptor. 3.000" overall length 1.000" overall width 0.250" material thickness strap alum plate; heat treat T851
01-488-4654
Structural Component Air Support
Used on f/a-22 raptor. 3.000" overall length 2.000" overall width 0.090" material thickness bracket alum sht; heat treat 0
01-488-4655
Structural Component Air Bracket
Used on f/a-22 raptor. 4.000" overall length 4.000" overall width 0.100" material thickness bracket assy of c/o 1 (-203 bracket) , 1 nut, 2 rivet; heat treat 0; alum sht
01-488-4656
Structural Component Air Support
Used on f/a-22 raptor. 3.000" overall length 3.000" overall width 2.000" material thickness support heat treat T851; alum plate
01-488-4657
Structural Component Air Bracket
Used on f/a-22 raptor. 4.000" overall length 3.000" overall width 0.063" material thickness bracket alum sht; heat treat 0
01-488-4658
Structural Component Air Bracket
Used on f/a-22 raptor. bracket, assy of c/o 1 (block) , 1 (sealant) ; alum sheet
01-488-4660
Structural Aircraft Panel
Used on C130J. nha is part number 3355200-5, panel assy, headset arwo console
01-488-4661
Structural Component Air Bracket
Used on f-22 raptor. 3.000" overall length 3.000" overall width bracket dim. are stock material; m/o: 2124-T851 aluminum plate
01-488-4663
Structural Component Air Bracket
Used on f/a-22 raptor. 4.000" overall length 2.000" overall width 0.080" material thickness bracket alum. sht; heat treat 0
01-488-4664
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 3.000" overall width 0.050" material thickness bracket ann titanium sheet
01-488-4665
Structural Component Air Bracket
Used on f/a-22 raptor. 10.000" overall length 2.000" overall width 0.750" material thickness bracket heat treat T851; alum plate
01-488-4670
Structural Component Air Bracket
Used on f/a-22 raptor. 3.000" overall length 2.000" overall width 0.063" material thickness bracket 6al-4v (ab-1) ann. titanium sheet
01-488-4671
Structural Component Air Bracket
Used on f/a-22 raptor. bracket - duct support, esc
01-488-4680
Aircraft Fairing
Used on c-130j aircraft. panel assy, vertical stabilizer, leading edge to dorsal
01-488-4897
Structural Aircraft Plate
0.090" material thickness plate-side, carriage, aft cargo door, ctr, assy of nha 4F61106
01-488-5002
Structural Component Air Fitting
Fitting-upper aft fuselage longeron
01-488-5016
Structural Component Air Fitting
Fitting-upper aft fuselage longeron
