01-507-5204
Structural Aircraft Plate
1.800" overall length 1.000" overall width 0.125" material thickness radius block heat treat T6; dimensions are stocksize
01-507-5279
Structural Component Air Support
Used on c130 hercules. 0.040" material thickness brackets-seal installation crew door frame stock size 0.040X5X6 in.
01-507-5632
Structural Aircraft Plate
1.800" overall length 1.000" overall width 0.125" material thickness radius block heat treat T6; dimensions are stocksize
01-507-5639
Structural Component Air Support
14.000" overall length 1.500" overall width 0.050" material thickness angle heat treat 0; dimensions are stocksize
01-507-5649
Structural Component Air Support
14.000" overall length 1.500" overall width 0.050" material thickness angle heat treat 0; dimensions are stocksize
01-507-5662
Structural Component Air Support
5.000" overall length 3.300" overall width 2.800" material thickness block dim are stock matl; foam matl shall be polymide foam ac-406
01-507-5663
Structural Component Air Support
7.900" overall length 5.000" overall width 4.000" material thickness block next higher assy, 68A324905, u/o f-15e cum 4
01-507-5664
Structural Component Air Support
5.000" overall length 4.000" overall width 2.800" material thickness block dim are stock matl; foam matl shall be polymide foam ac-406
01-507-5667
Structural Component Air Support
5.000" overall length 2.900" overall width 2.800" material thickness block dim are stock matl; foam matl shall be polymide foam ac-406
01-507-5685
Aircraft Fairing
Used on f/a-22 raptor. fairing
01-507-5686
Aircraft Fairing
Used on f/a-22 raptor. fairing
01-507-5687
Aircraft Fairing
Used on f-22 raptor. fairing wind swept surface critical item; carbon/bmi composite material
01-507-5886
Structural Aircraft Plate
Used on f-18 hornet combat aircraft. plate
01-507-5887
Structural Component Air Support
Used on ef/18 a combat aircraft.
01-507-5892
Structural Component Air Bracket
Used on ef-18 hornet combat aircraft. bracket
01-507-5895
Structural Aircraft Plate
Used on ef-18 hornet combat aircraft. plate
01-507-5897
Aircraft Stiffener
Used on harrier ii. stiffner
01-507-5899
Structural Aircraft Plate
Used on ef-18 a hornet combat aircraft. plate
01-507-5900
Structural Aircraft Plate
Used on ef-18 hornet combat aircraft. plate
01-507-5906
Movable Canopy
Used on f15 aircraft. canopy, moveable, pilot
01-507-6040
Aircraft Fairing
Used on f/a-22 raptor.
01-507-6041
Aircraft Fairing
Used on f/a-22 raptor. fairing, hinge 4-rudder
01-507-6043
Aircraft Fairing
Used on f/a-22 raptor. c/o 1 label, 10 carbon/epoxy
01-507-6045
Aircraft Fairing
Used on f/a-22 raptor. fairing
01-507-6046
Aircraft Fairing
Used on f-22 raptor. fairing, outobard, lower-rudder
01-507-6047
Bleed Air Duct Assembly
Ecs duct
01-507-6048
Access Aircraft Door
Used on f/a-22 raptor. door-access, anti-ice valve, ebay access to anti-ice valve at the bottom of the engine
01-507-6050
Structural Component Air Support
10.600" overall length 5.650" overall width 1.500" material thickness block next higher assy, 68A324910, u/o f-15a, b blk 17
01-507-6051
Structural Component Air Support
6.940" overall length 6.430" overall width 1.500" material thickness block nha, 68A324910, u/o f-15c cum 254
01-507-6052
Structural Component Air Support
9.190" overall length 6.830" overall width 1.500" material thickness block nha 68A324910, u/o f-15c CUM254
01-507-6053
Structural Component Air Support
6.780" overall length 6.430" overall width 1.500" material thickness block nha 68A324910, u/o f-15c cum 254
01-507-6054
Structural Component Air Support
6.940" overall length 6.430" overall width 1.500" material thickness block nha, 68A324910, u/o f-15c CUM254-up, f-15d CUM42-up, f-15dj CUM11-up, f-15e, i, s CUM1-up, fmf-15c CUM10-up, fmf-15d CUM7-up, 8-9
01-507-6055
Structural Component Air Support
8.850" overall length 6.750" overall width 1.500" material thickness block NHA68A324905, u/o f-15e cum 1-up; dim are stock matl, honeycomb core per mil-c-81986, cell size 3/16 in, density 2.0 lb/cu ft fully cured, thickness 1.50porm .03
01-507-6056
Structural Component Air Support
8.820" overall length 6.650" overall width 1.500" material thickness block nha 68A324905, u/o f-15e cum 1 andup; dim are stock matl
01-507-6057
Winglet
Winglet assy, complete same as -501 except ecn chg; composite material; NHA17N6W0636; effectivity 17A071-999
01-507-6058
Aircraft Fairing
Fairing assy-lwr pylon nha 17P6W5360; c/o 1 panel -507; effectivity 17A107-17A999; composite material
01-507-6059
Aircraft Fairing
Lower pylon-fairing assy nha 17P6W5360; c/o 1 panel -508; effectivity 17A107-17A999; composite material
01-507-7009
Aircraft Channel
3.700" overall length 5.500" overall width 0.050" material thickness side cowl panel assy - engine nacelle u/o p/ns 204-70045-1, -401, -447, -460
01-507-7058
Structural Component Air Fitting
01-507-7102
Aircraft Skin
Used on harrier.
01-507-7121
Structural Aircraft Plate
6.400" overall length 1.700" overall width 0.050" material thickness side cowl panel assy - engine nacelle commerically pure titanium, type i comp b
01-507-7242
Aircraft Fairing
Used on f/a-22 raptor. fairing, inboard, lower-rudder
01-507-7243
Structural Aircraft Panel
Used on f-22 raptor. panel, assembly of wind swept surface critical item; c/o: -127 panel, gasket (1) ; m/o: carbon/bmi & glass/bmi composite materials
01-507-7507
Aircraft Channel
12.000" overall length 2.800" overall width 0.050" material thickness side cowl panel assy - engine nacelle u/o p/ns 204-70045-1, -402, -447, -460; A286 cres sheet aisi 660 per ams 5525, condition s.t. (annealed)
01-507-7644
Structural Aircraft Plate
Used on f/a-22 raptor. louver-forward, inlet bypass make from 1 5HP41509-107 louver
01-507-7646
Structural Component Air Support
10.880" overall length 6.950" overall width 5.000" material thickness block NHA68A324966 u/o f-15e, i, s cum 1
01-507-8156
Structural Component Air Fitting
Used on c-130 transport aircraft. fitting, structual nha fitting, lower
01-507-8569
Structural Component Air Support
12.300" overall length 5.600" overall width 1.500" material thickness block nha 68A324905 u/o f-15e cum 1 andup; dim are stock matl; honeycomb core per mil-c-81986, cell size 3/16 in density 2.0 lb/cu ft fully cured, thickness 1.50 porm .03
01-507-8693
Structural Aircraft Plate
3.900" overall length 3.300" overall width 0.090" material thickness side cowl panel assy - engine nacelle c/o p/ns 204-70045-1, -401, -447, -460; A286 cres sheet aisi 660 per ams 5525 condition s.t. (annealed)
01-507-8866
Rudder Balance Weight
Used on nha bracket,fold hinge balance- rotary wing head. company name is balance weight
