01-543-2652
Structural Aircraft Panel
01-543-2836
Structural Aircraft Panel
Cover
01-543-2872
Structural Aircraft Plate
Used on KC-135. 4.100" overall length 2.400" overall width 0.040" material thickness doubler es code (sw) ; sh clad; o temp; heat treat T4; finish f-2.115; dim. are stocksize matl.
01-543-2875
Structural Aircraft Plate
Used on KC-135. 2.500" overall length 1.900" overall width 0.040" material thickness doubler es code (sw) ; 0 temp; heat treat T4; finish f-2.115; dim. are stocksize matl.
01-543-2898
Structural Aircraft Plate
Used on KC-135. 3.500" overall length 1.500" overall width 0.040" material thickness doubler -2 opposite; temp 0; sh clad; heat treat T4; finish f-2.115; dimensions are stocksize
01-543-2942
Stiffener Aircraft Rib
3.100" overall length 2.100" overall width 0.040" material thickness nose rib heat treat T4
01-543-2957
Stiffener Aircraft Rib
3.100" overall length 2.100" overall width 0.040" material thickness nose rib - partial, outboard aileron heat treat T4; opposite -1
01-543-3041
Structural Component Air Fitting
Used on f-22a raptor. 3.000" overall length 3.000" overall width 0.500 " material thickness fitting dim. are stock material; m/f: 2024-T851 alum plate
01-543-3053
Structural Component Air Fitting
Used on f-22 raptor. 23.000" overall length 12.000" overall width 2.250 " material thickness al plate; nha 5HP41793-111; dim.are stocksize matl.
01-543-3064
Structural Aircraft Panel
Used on fighter aircraft-first (f18 e/f). panel, aircraft, mate
01-543-3082
Structural Aircraft Panel
Used on fighter aircraft-first (f18 e/f). panel, aircraft, mate nha: 015431584 baffle, fuel tank, ai
01-543-3142
Structural Component Air Fitting
Used on C-130. wing joint fitting heat treat T6
01-543-3149
Stiffener Aircraft Rib
Used on KC-135. 3.600" overall length 2.300" overall width 0.040" material thickness nose rib - partial, outboard aileron heat treat T4; opposite -1; used on 5-88190
01-543-3158
Structural Aircraft Plate
Used on KC-135. 4.500" overall length 2.300" overall width 0.040" material thickness splice plate heat treat T3; opposite -2
01-543-3166
Structural Aircraft Plate
Used on KC-135. 4.500" overall length 2.300" overall width 0.040" material thickness splice plate opposite -1; heat treat T3
01-543-3186
Aileron Balance Weight
Used on KC-135. 1.060" overall width stocksize matl .44X1.06X7.02
01-543-3230
Airfoil Rib
Used on KC-135. 3.100" overall length 2.100" overall width 0.040" material thickness nose rib used on 5-88190
01-543-3257
Cable Aircraft Mounted Cutter
01-543-3267
Structural Component Air Support
Used on model 101000 180 hp engine.
01-543-3268
Structural Component Air Bracket
Used on model 101000 180 hp engine.
01-543-3269
Structural Component Air Bracket
Used on model 101000 180 hp engine.
01-543-3649
Aircraft Fairing
Used on A-10A. 8.700" overall length 5.200" overall width 0.040" material thickness heat treat T6; nha 160D712100
01-543-3665
Aircraft Fairing
Used on A-10A. 8.700" overall length 5.000" overall width 0.040" material thickness lower fair rem heat treat T6; nha 160D712100
01-543-3868
Aircraft Door
01-543-3931
Structural Component Air Bracket
01-543-3939
Airfoil Rib
17.400" overall length 7.000" overall width rib matl al clad 2024.0 sheet, qq-a-250/50 temp; dim are stock matl
01-543-3948
Structural Aircraft Plate
01-543-3966
Structural Component Air Support
9.000" overall length 3.600" overall width brace lwr matl al 7075-0 sheet; qq-a-250/12 0 temp; dim are stock matl
01-543-3997
Aircraft Skin
Used on A-10. 93.000" overall length 8.500" overall width used on -1, -3, -5, -9, -7, -201, -203; nha 160D712100; alcd sh; t 76
01-543-4010
Aircraft Fairing
Used on A-10. 28.800" overall length 5.300" overall width 0.040" material thickness upper fairing alcd sh; T6; dim. are stocksize; used on -2, -4, -8, -202, -204, -9
01-543-4017
Aileron Balance Weight
01-543-4042
Structural Aircraft Plate
01-543-4056
Structural Aircraft Plate
01-543-4063
Aileron Balance Weight
Used on kc135 aircraft. antimony lead, l-16 (6% antimony) , finish is 2 coats of zinc chromate primer per mil-p-8585; 1.060" wide; 0.440" high tapering to 0.340" high; located on outboard nose of aileron
01-543-4079
Structural Component Air Support
9.000" overall length 3.600" overall width 0.063" material thickness brace upper matl al 7075 sheet, qq-a-250/12 0 temp; dim are stock matl
01-543-4080
Aileron Balance Weight
01-543-4090
Structural Component Air Support
2.600" overall length 1.600" overall width 0.063" material thickness strap matl al 7075 sheet, qq-a-250/12 T6 temp; dim are stock matl
01-543-4093
Structural Component Air Bracket
01-543-4113
Structural Component Air Support
01-543-4115
Structural Component Air Support
01-543-4134
Structural Aircraft Plate
01-543-4405
Structural Aircraft Panel
Used on f-22 raptor. panel, lower aileron-bonded part c/o 1 panel, lower (5HU84753-11) ; 1 panel, lower (5HU84753-116) ; 1 panel, lower (5HU84753-118; ref smoothness; ref mds index; ref loft; ref symbols, surace; ref inishes, ident, marking, marking parts, wind swept part, temp protection, 2 labels, bkm carbon/bmi, bkm glass/bmi, 3 bkm bmi, ar primer, ar epoxy
01-543-4407
Structural Aircraft Panel
Used on f-22 raptor. skin panel -bonded part, lower
01-543-4408
Aircraft Arresting Hook Arm
Used on f-22 raptor. hook assy - fwd uplock, arresting gear c/o 1 hook; 2 bushing; 1 bearing; ar sealant
