01-497-4608
Airfoil Rib
15.250" overall length 8.700" overall width 0.063" material thickness next higher assy, 1-1008 u/o f-15e cum 1-163; manf suggested name-rib
01-497-4610
Aircraft Former
16.900" overall length 5.780" overall width 0.063" material thickness dim. are stock material; nha -1005, -1009, -1011; u/o f-15c 1-390, f-15d 1andup
01-497-4612
Structural Component Air Support
33.000" overall length next higher assy, 68A321450, u/o f-15c cum 1
01-497-4613
Structural Component Air Support
11.000" overall length manf suggested name tee, next higher assy, 1-1002 u/o f-15c blk 22
01-497-4614
Structural Aircraft Panel
27.000" overall length 15.400" overall width liner dim. are stock material; nha 68A321380-1001, -1003; u/o f-15c CUM1&up, f-15d CUM1&up, f-15e CUM1-2
01-497-4615
Structural Aircraft Plate
6.350" overall length 6.120" overall width 0.063" material thickness doubler dim. are stock material; nha 68A321000-1005, -1009, -1011; u/o f-15c CUM107-303, f-15d CUM18-49
01-497-4616
Structural Aircraft Plate
4.880" overall length 4.320" overall width 0.063" material thickness doubler dim. are stock material; nha 68A321000-1001, -1003, -1005, -1009, -1011; u/o f-15c CUM1-303, f-15d CUM1-49
01-497-4617
Structural Aircraft Panel
33.000" overall length 7.000" overall width liner dim. are stock material; nha 68A321380-1001, -1003; u/o f-15c CUM1&up, f-15d CUM1&up, f-15e CUM1-2
01-497-4621
Aircraft Stiffener
15.000" overall length dim. is stock material; nha -1004, -1008; u/o f-15c CUM186-390, f-15d CUM28&up
01-497-4622
Longeron
85.000" overall length material 1MT10044B01, dim. is stock material; nha 68A331000; u/o f-15e CUM210&up, f-15i CUM1&up, f-15s CUM1&up
01-497-4623
Canopy Transparency
01-497-5066
Structural Aircraft Plate
Used on f/a-22 raptor. louver made from 1 5HP41503-111 lover; stock size 15" wide
01-497-5076
Structural Component Air Support
Manufacturer suggested name "doubler, flange
01-497-5078
Canopy Transparency
01-497-5366
Structural Aircraft Panel
01-497-5368
Aircraft Stiffener
01-497-5369
Structural Aircraft Panel
01-497-5431
Bleed Air Duct Assembly
01-497-5718
Aircraft Hinge
Used on f-22 raptor. hinge-mid inlet bypass consists of 1 5HP41802-111 hinge assembly; 23 CB7514CR5-1p nut plates
01-497-5719
Aircraft Hinge
Used on f/a-22 raptor. hinge-forward, inlet bypass consists of: (1) 5HP41801-112 hinge assembly; (23) CB7514CR5-1p nutplate; (16) (oz) 226817002 shim; (12) (oz) 920082003 epoxy
01-497-5829
Structural Component Air Support
01-497-5944
Door Aircraft Hinge
Used on f-22 raptor. hinge assembly
01-497-5950
Structural Component Air Support
Angle material 0.063 2024-0 alclad
01-497-5952
Structural Component Air Support
2.750" overall length 2.000" overall width 1.500" material thickness splice fitting next higher assy 68A321016; u/o f-15c blk 24
01-497-5953
Structural Component Air Support
7.950" overall length stock material thickness 0.025; nha 68A328002; u/o f-15a, b BLK13&up, f-15c, d, j CUM1&up
01-497-5954
Fuselage Section
Mid nose assy includes antenna mounts; sealing compound mil-s-8802 type ii, class b; doubler .090 thick
01-497-5956
Canopy Transparency
01-497-5959
Canopy Transparency
01-497-6583
Structural Aircraft Plate
01-497-6584
Aircraft Drain-vent
01-497-6586
Structural Component Air Support
14.430" overall length 12.920" overall width 0.050" material thickness liner dim are stock material
01-497-6589
Aircraft Stiffener
15.000" overall length dim are stock matl, 1MA10502-D01; next higher assy, 1-1007, u/o f-15c cum 188-390, f-15d cum 30
01-497-6590
Aircraft Stiffener
15.000" overall length dim are stock material, 1MA163D01-10043
01-497-6592
Aircraft Stiffener
15.000" overall length dim are stock material, 1MA163D01-10043
01-497-6599
Canopy Transparency
01-497-6600
Canopy Transparency
01-497-6603
Aircraft Trailing Edge
U/0 no. 1-58; c/o 1 spar assy, 1 core, adhesive; heat treat 0
01-497-6768
Airfoil Rib
Stock size 5.00 x 5.62 x 25.00
01-497-6965
Structural Component Air Bracket
01-497-7117
Aircraft Thrust Reverser Section
01-497-7119
Aircraft Thrust Reverser Section
01-497-7121
Aircraft Thrust Reverser Section
01-497-7122
Aircraft Thrust Reverser Section
01-497-7123
Aircraft Thrust Reverser Section
01-497-7125
Aircraft Thrust Reverser Section
01-497-7126
Aircraft Thrust Reverser Section
01-497-7127
Aircraft Thrust Reverser Section
01-497-7156
Structural Component Air Support
Used on f/a-22 raptor. 10.000" overall length 2.000" overall width 1.000" material thickness support consists of 1 5HH46113-109 support; 2 LK204F3 nuts; 4 LK207F3 nuts; 8 MS20426AD3-4 rivets
01-497-7174
Canopy Transparency
01-497-7192
Structural Component Air Support
