01-555-0019
Structural Component Air Support
14.480" overall length 1.500" overall width
01-555-0030
Structural Component Air Support
14.700" overall length 1.306" overall width m/f AND10134-1206
01-555-0042
Structural Component Air Support
14.700" overall length 1.306" overall width m/f
01-555-0052
Structural Component Air Support
14.680" overall length 1.283" overall width m/f
01-555-0084
Aircraft Spar
01-555-0106
Aircraft Former
3.900" overall length 1.000" overall width 0.032" material thickness filler finish f-2.115 clad 7075-T6 strip spec qq-a-287 T6 temper
01-555-0107
Structural Component Air Bracket
Used on A-10. 14.900" overall length 0.156" material thickness angle alshp-T6511; used on -249; dim. are stock matl
01-555-0119
Structural Component Air Support
Used on A-10. supports T6511
01-555-0122
Structural Component Air Support
Used on A-10. support nha 160D611325; al shp; T6511
01-555-0127
Structural Component Air Support
Used on A-10. support NHA160D611325; al stp; T6511
01-555-0132
Aircraft Spar
Used on F-16. 109.000" overall length 6.000" overall width 1.750" material thickness spar c/o 1 -13 spar, plate; dim. are stocksize matl; fnsh A427; T7351
01-555-0134
Structural Component Air Bracket
7.700" overall length splice angle bac-1490-2541X7.7 clad 7075-T6 qq-a-287 T6 temp finish f-2.115
01-555-0139
Aircraft Skin
26.000" overall length 4.400" overall width nose skin-outed finish f-2.130 T6 strip spec qq-a-287 T6 temper
01-555-0144
Aircraft Spar
Used on F-16. 119.000" overall length 4.000" overall width 1.750" material thickness spar dim are stocksize matl; c/o 1 (-15 spar) , plate; T7351
01-555-0146
Aircraft Former
75.000" overall length 1.140" overall width 0.081" material thickness filler finish f-2.115 clad 7075-T6 strip spec qq-a-287 T6 temper
01-555-0151
Structural Aircraft Plate
3.000" overall length 1.000" overall width 0.063" material thickness plate aisi 301 steel sh spec mil-s-5059 comp 301 sur cond 2b 1/2 hard f-12.35 finish after assembly f-1.10 finish f-12.46 on installation
01-555-0156
Aircraft Skin
33.100" overall length 5.900" overall width nose skin-inbd fwd clad 7075-T6 sh qq-a-287 T6 temp finish f-2.130
01-555-0163
Aircraft Spar
Used on F-16. 109.000" overall length 6.000" overall width 1.750" material thickness spar T7351; dim. are stock matl.; fnsh A427
01-555-0255
Aircraft Spar
Used on F-16. 115.000" overall length 5.000" overall width 1.750" material thickness spar dim. are stock matl; T7351; fnsh A427; c/o 1 (-16 spar) , 1 plate
01-555-0269
Structural Component Air Bracket
6.900" overall length attach angle bac-1503-100130 T4 extr qq-a-267 T4 temp finish f-2.30
01-555-0270
Aircraft Spar
Used on F-16. 115.000" overall length 5.000" overall width 1.750" material thickness spar fnsh A427; dim. are stock matl; T7351; c/o 1 (-24 spar) , 1 plate
01-555-0328
Structural Component Aircraf Web
Bonded web assy of finish f-2.31 bonded web assy bac 5425 optional to bac 5462
01-555-0330
Structural Component Aircraf Web
Bonded web assy of finish f-2.31 bonded web assy bac 5425 optional to bac 5462
01-555-0352
Structural Component Aircraf Web
01-555-0390
Structural Aircraft Plate
01-555-0392
Aircraft Spar
01-555-0408
Aircraft Spar
01-555-0433
Aircraft Skin
01-555-0439
Airfoil Rib
6.000" overall length 3.000" overall width 0.071" material thickness rib matl al aly qq-a-250/4 - T62; dim are stock matl
01-555-0440
Structural Component Air Bracket
Used on A-10. 14.900" overall length 0.125" material thickness angle dim. are stock matl; used on -249;
01-555-0443
Structural Component Air Bracket
Used on A-10. 14.800" overall length 0.125" material thickness angle dim. are stocksize matl; used on -249
01-555-0463
Aircraft Spar
Spar matl FM3-3004-T7351; nha 16W1049
01-555-0465
Aircraft Beam
01-555-0472
Aircraft Spar
Spar matl FM3-3004-T7351; nha 16W1049
01-555-0474
Aircraft Spar
Spar matl FM3-3004-T7351; nha 16W1049
01-555-0478
Structural Aircraft Panel
01-555-0480
Structural Aircraft Panel
01-555-0487
Structural Aircraft Plate
01-555-0489
Structural Aircraft Panel
01-555-0495
Structural Component Aircr Patch
01-555-0498
Airfoil Rib
16.000" overall length 12.500" overall width rib matl al aly 7075 sheet qq-a-283; dim are stock matl
01-555-0503
Structural Component Aircraf Web
01-555-0565
Cowling
Used on ch-149 helicopter.
01-555-0566
Cowling
Used on ch-149 helicopter.
01-555-0823
Aircraft Spar
