01-554-8804
Structural Component Air Bracket
01-554-8807
Aircraft Skin
01-554-8816
Structural Component Air Support
01-554-8820
Structural Component Air Bracket
01-554-8831
Structural Component Air Support
01-554-8866
Structural Component Air Support
01-554-8871
Structural Component Air Support
01-554-8877
Aircraft Hinge
01-554-8880
Structural Component Air Support
01-554-9132
Aircraft Pylon
01-554-9137
Structural Component Air Bracket
Used on f-22 raptor. 3.000" overall length 3.000" overall width 0.063" material thickness c/o 1 (-223 bracket) , misc. hardware; T3 sheet
01-554-9140
Structural Aircraft Panel
01-554-9141
Structural Aircraft Panel
01-554-9142
Structural Aircraft Panel
01-554-9143
Structural Aircraft Panel
01-554-9179
Aircraft Stiffener
24.000" overall length chord upper aft alter BAC1514-1391X24.0 2024-T4 extr qq-a-267 T4 temp finish f-2.30
01-554-9181
Stiffener Aircraft Rib
8.000" overall length 2.900" overall width 0.080" material thickness doubler finish f-2.115 clad 7075-T6 sh qq-a-287 T6 temper
01-554-9187
Aircraft Hinge
01-554-9192
Structural Aircraft Plate
01-554-9197
Aircraft Stiffener
3.300" overall length stiffener bac-1503-100134X3.3 2024-T4 extr qq-a-267 T4 temp finish f-2.30
01-554-9200
Structural Aircraft Plate
01-554-9204
Aircraft Fairing
01-554-9235
Aircraft Spar
Used on F-16. 63.000" overall length 6.500" overall width 1.750" material thickness spar c/o 1 -15 spar, dim. are stock matl., plate alum
01-554-9242
Aircraft Spar
Used on F-16. 77.000" overall length 6.500" overall width 1.750" material thickness spar dim.are stocksize
01-554-9267
Aircraft Spar
Used on F-16. 88.500" overall length 6.000" overall width 1.750" material thickness spar dim. are stock matl; c/o -34 spar.
01-554-9281
Aircraft Spar
Used on F-16. 63.000" overall length 6.500" overall width 1.750" material thickness spar dim. are stocksize; c/o 1 (-24 spar) , plate
01-554-9290
Aircraft Spar
Used on F-16. 63.000" overall length 6.500" overall width 1.750" material thickness spar c/o 1 (-21 spar) , plate; dim. are stock matl.
01-554-9304
Structural Aircraft Plate
Used on A-10. 2.200" overall length 1.200" overall width 0.050" material thickness seal dim. are stock matl.; alcd sh/ used on -3
01-554-9338
Structural Aircraft Plate
Used on A-10. 2.200" overall length 1.200" overall width 0.050" material thickness seal alcd sh-T6; dim. are stocksize matl; used on -4
01-554-9351
Aircraft Spar
Used on F-16. 88.500" overall length 6.000" overall width 1.750" material thickness spar c/o 1 (-48 spar) , plate; dim. are stock size matl.
01-554-9594
Aircraft Spar
Used on F-16. 29.000" overall length 7.000" overall width 1.750" material thickness spar c/o 1 (-15 spar) , plate; dim. are stocksize; -16 opposite; -15/16 maybe used for all replacements of -9/-10; fnsh A427; T7351
01-554-9597
Aircraft Spar
Used on F-16. 77.000" overall length 6.500" overall width 1.750" material thickness spar c/o 1 -28 spar, plate; dim. are stocksize matl
01-554-9629
Structural Component Air Bracket
Angle
01-554-9631
Structural Component Air Bracket
Angle
01-554-9635
Structural Component Air Support
01-554-9637
Aircraft Fairing
01-554-9641
Aircraft Hinge
01-554-9642
Structural Aircraft Plate
01-554-9648
Aircraft Skin
01-554-9668
Aircraft Spar
Used on F-16. 117.000" overall length 5.000" overall width 1.750" material thickness spar c/o 1 (-27 spar) , plate; dim. are stocksize; T7351
01-554-9680
Aircraft Spar
Used on F-16. 117.000" overall length 5.000" overall width 1.750" material thickness spar dim are stock matl; c/o 1 spar, 1 plate; fnsh A427
01-554-9941
Structural Component Air Bracket
2.630" overall length 8.440" overall width weight mount opposite -6 301 cres SH1/2 hard per ams 5528 f-12, 37 plus f-12
01-554-9970
Structural Component Air Bracket
14.900" overall length 0.125" material thickness angle dim. are stock material
01-554-9972
Structural Component Air Bracket
14.900" overall length 0.125" material thickness angle dim. are stock material
01-554-9976
Structural Component Air Bracket
14.800" overall length 0.125" material thickness angle dim. are stock material
01-554-9982
Structural Component Air Bracket
14.900" overall length 0.156" material thickness angle dim. are stock material
01-554-9991
Aircraft Spar
Used on F-16. 109.000" overall length 6.000" overall width 1.750" material thickness spar c/o 1 (-14 spar) , plate; dim. are stock matl, T7351; fnsh A427
01-555-0002
Structural Component Air Support
14.800" overall length 1.246" overall width
01-555-0008
Structural Component Air Support
14.450" overall length 1.276" overall width m/f AND10134-1405
