01-504-4194
Structural Aircraft Plate
Seal assy - access door instl, engine pylon an interchangeable item, iaw mil-i-8500
01-504-4198
Structural Aircraft Plate
Fence acft p/n 17P2A3935-531 superseded by -603
01-504-4199
Aircraft Floor
01-504-4202
Structural Aircraft Panel
01-504-4222
Structural Aircraft Panel
01-504-4223
Structural Aircraft Panel
01-504-4225
Aircraft Scoop
01-504-4473
Wing Aircraft Spoiler
01-504-4474
Structural Component Air Support
01-504-4475
Structural Component Air Support
01-504-4562
Structural Component Air Bracket
Used on f-22a raptor. 3.000" overall length 3.000" overall width 0.080" material thickness bracket, assembly of dim. are stock material; c/o: -171 bracket, LK213F3 nut,
01-504-4563
Structural Component Air Fitting
Used on f/a-22 raptor. 5.000" overall length 4.000" overall width fitting 1 fitting, 4 nuts, 8 rivets; dimension are stock sized
01-504-4574
Structural Aircraft Panel
Used on f/a-22 raptor. panel
01-504-4867
Aircraft Intercostal
Nha arc-190 hf longwire 816-3233-001
01-504-4869
Aircraft Intercostal
Nha arc-190 hf longwire 816-3233-001
01-504-4988
Structural Aircraft Panel
01-504-5154
Structural Component Air Support
01-504-5251
Structural Component Air Support
8.060" overall length 6.000" overall width 1.460" material thickness 2019 opp -2010; dim are stock; mil-c-81986 superseded by sae-ams-c-81986; nha:-1001 honeycomb liner-inst of, fuel cell; u/o f-15c CUM354 & up, f-15d CUM59 & up, f-15e CUM1 & up
01-504-5252
Structural Component Air Support
11.300" overall length 5.800" overall width 1.430" material thickness fuel cell 2 cnext higher assy, 68A324900, u/o f-15c cum 354
01-504-5253
Structural Component Air Support
14.750" overall length 2.750" overall width 2001 opp -2002; nha 68A324000; u/of-15a CUM1-BLK6, f-15b CUM1-BLK4, f-15a FTA1-STA1
01-504-5254
Structural Component Air Support
8.080" overall length 4.180" overall width 1.390" material thickness fuel cell 2 dnext higher assy, 68A324900, u/o f-15c cum 354
01-504-5255
Structural Component Air Support
8.000" overall length 6.000" overall width 1.460" material thickness fuel cell 2 2007 opp -2008; dim are stock material; mil-c-81986 superseded by sae-ams-c-81986, nha:-1001 honeycomb liner-inst of, fuel cell; u/o f-15c CUM354 & up, f-15d CUM59 & up, f-15e CUM1 & up
01-504-5256
Structural Aircraft Panel
7.000" overall length 4.000" overall width rudder assy-vertical stablizer anodize per PS13201 TYPE2 class 1; heat treat to cond T62 per PG15534
01-504-5257
Structural Component Air Support
8.080" overall length 5.520" overall width 1.390" material thickness fuel cell 2 cnext higher assy, 68A324900, u/o f-15c cum 354
01-504-5474
Wing Aircraft Fairing
Fairing-assembly-wing fold, lwr, flap, le opposite -5
01-504-5503
Structural Component Air Bracket
Cap canted Y365.700; matl 7075-T6 alcad
01-504-5584
Structural Aircraft Panel
Panel assy, stair tread - crew door jc/o 1 guard, stock size .032X4X33; p/n 17P1A4668; 1 panel, stock size 11X33 (make from 9D0059-4a) ; 1 mat (p/n -15) stock size 6X30, deck covering non-skin cloth; 14 insert plugs p/n 9D0057-38400; heat treat T6
01-504-5585
Structural Aircraft Panel
Panel assy, stair tread - crew door c/o 1 guard p/n 17P1A4668-3, 1 panel p/n 17P1A4668-5; 1 mat p/n 17P1A4668-11; 14 insert plugs p/n 9D0057-38400) ; stock size .032 x 4 x 33; heat treat T6
01-504-5592
Trim Aircraft Tab
01-504-5593
Fuselage Parts Kit
Used on E-3. kit-100% replacement item lower lobe refurbishment replacement kit for e-3 lower lobe referbishment effort; p/n 20021167-20 is applicable to eff codes T001, T003 thru T0025 iaw usaf drwg 20021167; kit consists of but is not limited to; panel assys; blanket insul assys; hose assys; cable markers; retainer ring insul; wire bundles; decals; clamps; flex ducts; spacers
01-504-5594
Trim Aircraft Tab
01-504-5595
Fuselage Parts Kit
Used on E-3. kit-100% replacement item lower lobe refurbishment replacement kit for e-3 lower lobe refurbishment effort; p/n 20021167-10is applicable to effectivity codes T0001, T0003 thru T0034 iaw usaf drwg 20021167; kit consist of but not limited topanel assys; blanket insul assys; wire bundles; duct assys; hose assy oil
01-504-5596
Fuselage Parts Kit
Used on E-3. kit-100% replacement item lower lobe refurbishment replacement kit for e-3 lower lobe refurbishment effort; p/n 20021167-30is applicable to effectivity codes T0026 thru T0034 iaw usaf drwg 20021167; kit consists of but not limited to, panel assys; placards; duct assys; hose assys; blanket assys insul; wire bundels; gaskets; cable markers; retainer ring insul; spacers; decals; clamps
01-504-5705
Structural Component Air Support
Used on encapsulated harpoon certification and training vehicle (ehctv). fitting assembly used on tank assy, p/n 72A356475-1001/1003
01-504-5768
Structural Component Air Support
01-504-5884
Stiffener Aircraft Rib
01-504-5889
Structural Component Air Support
01-504-5891
Fuselage Section
01-504-6061
Structural Aircraft Plate
11.500" overall length 2.500" overall width 0.050" material thickness angle seal/eng.pylon bulkhead heat treat 0; alcd sh
01-504-6062
Aircraft Former
4.440" overall length 4.060" overall width 0.040" material thickness formers-rudder closure nha 68A240001; heat treat to 2024-T62 per 15534
01-504-6065
Aircraft Former
4.000" overall length 3.750" overall width 0.040" material thickness formers-rudder closure nha 68A240001; heat treat to 2024-T62 per 15534
01-504-6066
Structural Aircraft Plate
11.500" overall length 2.500" overall width 0.050" material thickness angle seal/eng.pylon, bukhead heat treat 0, alcd sh
01-504-6067
Structural Aircraft Plate
6.100" overall length 1.300" overall width 0.016" material thickness housing instl - engine pylon c/o p/n 160D412025-1 (housing instl) , 1/4 hard
01-504-6068
Structural Aircraft Plate
6.100" overall length 1.300" overall width 0.016" material thickness housing instl - engine pylon c/o p/n 160D412025-1 (housing instl)
01-504-6070
Structural Aircraft Panel
Panel assy, stair tread - crew door c/o 1 guard, stock size .032X4X33; 1 panel p/n 17P1A4668-9, 1 mat (-13) stock size 6X30, deck covering non-skin cloth, 14 insert plugs p/n 9D0057-38400; heat treat T6
01-504-6072
Structural Aircraft Panel
Panel assy, stair tread - crew door c/o 1 guard, .032X4X33; 1 panel (make from 9D0059-4a) ; 1 mat, 8X24; deck covering non-skid cloth; 16 insert plugs, heat treat T6
01-504-6197
Structural Aircraft Panel
01-504-6201
Structural Component Air Support
01-504-6359
Structural Component Air Support
8.080" overall length 5.460" overall width 1.390" material thickness 2003 opp -2004; dim are stock; material spec mil-c-81986 superseded bysae-ams-c-81986; nha: -1001 honeycomb liner-inst of, fuel cell; u/o f-15c CUM354 & up, f-15d cum & up, f-15e CUM1 &up
01-504-6360
Structural Component Air Support
5.350" overall length 3.000" overall width 1.440" material thickness fuel cell 2 2009 opp -2010; dim are stock material; mil-c-81986 superseded by sae-ams-c-81986; nha:-1001 honeycomb liner-inst of, fuel cell; u/o f-15c CUM354 & up, f-15d CUM59 & up; f-15e CUM1 & up
