01-516-3526
Structural Component Air Support
32.000" overall length 16.000" overall width fitting lh dim stock mattl; make from forging 160D612608f
01-516-3543
Structural Component Air Support
32.000" overall length 16.000" overall width fitting rh dim are stock matl; make from forging 160D612608f
01-516-3544
Structural Component Air Support
32.000" overall length 16.000" overall width dim are stock matl; make from forging 160D612608f
01-516-3636
Access Aircraft Door
01-516-3637
Aircraft Floor
01-516-3649
Door Aircraft Parts Kit
01-516-3654
Structural Component Air Fitting
01-516-3657
Structural Component Air Support
Used on f/a-22 raptor. support-aux pump tubing, assy of
01-516-3658
Structural Component Air Support
Used on f-22 raptor. support support, tubing-utility distribution module 4
01-516-3659
Tubing Aircraft Support
Used on f-22 raptor. 5.000" overall length 1.000" overall width 1.000" material thickness support-auxiliary pump tubing, assembly of consists of 1 5HH41025-147 support; 2 LK216F3 nuts
01-516-3660
Tubing Aircraft Support
Used on f-22 raptor. 4.000" overall length 3.000" overall width 1.000" material thickness support-auxiliary pump tubing, assembly of consists of 1 5HH41025-143 support; 2 LK213F3 nuts
01-516-3662
Structural Component Air Support
Used on f-22 raptor. 15.080" overall length 4.950" overall width 1.000" material thickness support assembly thickness dim. is stock material; c/o: -121 support, LK213F3 nut (4) , LK213F4 nut (4) ; MS20426AD3-5 rivet (8) , MS20605AD3C2 rivet (8) , m/o: 2124-T851 aluminum plate
01-516-3663
Structural Component Air Support
Used on f-22 rator. 2.000" overall length support, assy of 1 nut LK208F3; 2 rivet MS20426AD3-4 & -139 support; 5PTM4G10K10B26 extruded shape; ht per AMS2770; final conditon-T6511
01-516-3664
Structural Component Air Support
Used on f/a-22 raptor. support
01-516-3667
Structural Aircraft Plate
Used on f/a-22 raptor. 8.980" overall length 0.850" overall width 0.078" material thickness plate assembly end item is control unit, generator, main
01-516-3670
Structural Component Air Support
Used on f-22 raptor. 25.000" overall length 9.000" overall width support assembly dim. are stock material; c/o support assy, bushing (2) , lanyard assy (2) , ring (6) , screw (6) ; 5PTM7G08 2124-T8151 aluminum plate
01-516-3673
Tubing Aircraft Support
Used on f-22 raptor. 3.000" overall length 6.000" overall width 0.063" material thickness bracket assembly dimensions are stock items; c/o: -107 bracket; LK204F3 nut (3) ,
01-516-3674
Tubing Aircraft Support
Used on f-22 raptor. 2.030" overall length 3.840" overall width bracket assembly c/o: -143 bracket, nut (1) rivet (1) ; 5PTM4G10K10A51, extruded shape, h/t alum per AMS2770, final condition T8511
01-516-3675
Tubing Aircraft Support
Used on f-22 raptor. bracket assembly c/o: -117 bracket, -121 shim, nutplate (1) ; 5PTM4G10K40A143 extruded shape
01-516-3676
Tubing Aircraft Support
Used on f-22 raptor. 3.000" overall length 6.000" overall width 0.063" material thickness bracket assembly dimension as stock material; c/o: -108 bracket, LK204F3-5 nut (3) ; & MS20426AD3-5 rivet (6) ; m/f: 2024-0 alum sht; ht per AMS2770; final cond T62
01-516-3677
Structural Component Air Bracket
Used on f/a-22 raptor. bracket
01-516-3678
Tubing Aircraft Support
Used on f/a-22 raptor. 1.270" overall width support bracket material final condition T8511; finish 607-646
01-516-3679
Structural Component Air Support
Used on f/a-22 raptor. 2.290" overall length 1.400" overall width bracket, support-fuel line bracket has 14 degree bend at 1.370"
01-516-3680
Structural Component Air Support
Used on f/a-22 raptor. 1.580" overall width 0.800" material thickness bracket, support-fuel line, extrusion, machined
01-516-3683
Bleed Air Duct Assembly
Used on f/a-22 raptor. duct assembly - ram air ecs primary heat exchanger refer to drawing 5HP41047
01-516-3684
Structural Aircraft Plate
Used on f-22a raptor. 8.000" overall length 3.000" overall width 0.500" material thickness seal wind swept surface critical item; dim. are stock material; m/f: 2024-T851 alum plate; c/o: -120 seal, nuts & rivets
01-516-3687
Structural Aircraft Plate
Used on F-22A. 8.000" overall length 3.000" overall width 0.500" material thickness seal assy wind swept surface critical item; m/f: 2024 alum plate; dim. are stock material; c/o: -122 seal, nuts & rivets
01-516-3688
Structural Aircraft Plate
Used on f-22a raptor. 8.000" overall length 3.000" overall width 0.500" material thickness seal, assembly of wind swept surface critical item; dim. are stock material; c/o: -124 seal, LK204F3 nut, & MS20426AD3-4 rivet; m/f: 2024-T851 aluminum plate
01-516-3693
Access Aircraft Door
Used on f-22 raptor. finish assembly durability critical / wind swept surface critical item; m/f: 5HM88110-111
01-516-3707
Structural Aircraft Panel
01-516-3708
Structural Aircraft Panel
01-516-3709
Structural Aircraft Panel
01-516-3710
Structural Aircraft Panel
01-516-3761
Structural Component Air Support
Support-mechanism attach 5 made from -7 rough forging; nha 2-13201
01-516-3799
Structural Component Air Bracket
Used on pantera targeting pod. pod primary structure made from cast aluminium mated with a compact stainless steel roll bearing
01-516-3919
Aircraft Stiffener
01-516-3968
Structural Component Air Support
01-516-4267
Structural Aircraft Panel
Used on mv-22 aircraft. navy panel assembly, aircraft plastic polyvinyl chloride surface treated
01-516-4268
Structural Aircraft Panel
Used on mv-22 osprey tilt-rotor aircraft. mounting tray, aircr contractor supported item for navicp phil consummable, v-22xc low rate initial production (lrip) 1 e-nsn interim support item list (isil)
01-516-4450
Structural Component Air Fitting
20.000" overall length 2.750" overall width 2.750 " material thickness fitting fwd heat treat T7351; plate; additional ws 66.00
01-516-4452
Structural Component Air Fitting
20.000" overall length 2.750" overall width 2.750 " material thickness fitting, fwd heat treat T7351; plate; additional WS66.00
01-516-4525
Structural Component Air Support
Used on 65-22113-94.
01-516-4541
Structural Component Air Bracket
Used on 65-8774-2.
01-516-4545
Structural Component Air Bracket
Used on panel installation,wing body fairing ram air scoop modulation.
01-516-4548
Structural Component Air Bracket
Used on 65-22919-2.
01-516-4556
Structural Component Air Fitting
Used on 65-18103-2.
01-516-4557
Structural Component Air Fitting
Used on 65-18140-2.
01-516-4558
Structural Component Air Fitting
Used on 65-18140-1.
01-516-4569
Structural Component Air Bracket
Used on 65-19001-1.
01-516-4571
Structural Component Air Fitting
Used on door assembly,aft galley.
