01-523-2315
Structural Aircraft Plate
01-523-2316
Structural Aircraft Plate
3.700" overall length 2.100" overall width 0.080" material thickness access panel doubler dims are stock material; f-2.59; nha is 520-12913 for effectivity L7401-L7402; nha is 520-13301 for effectivity L7401-L7899
01-523-2423
Structural Component Air Support
Wing splice fitting make from forging 160D612608f
01-523-2584
Structural Aircraft Panel
Panel panel inst y 609.500 to Y671.230
01-523-2586
Access Aircraft Door
01-523-2612
Structural Component Air Fitting
16.650" overall length 2.750" overall width 2.660 " material thickness fitting matl AL7050-T7452 forged block per bms 7-214; dim are stock matl
01-523-2613
Structural Aircraft Panel
98.000" overall length 75.000" overall width panel frabric carbon fiber woven b-stage epoxy impergnated; dms 2288 type 2, class 2, grade d; dim are stock matl
01-523-2617
Structural Component Air Support
01-523-2625
Structural Component Air Bracket
01-523-2626
Structural Component Air Fitting
4.377" overall length 1.482" overall width fitting dim are stock matl; -104 opposite
01-523-2627
Structural Component Air Fitting
01-523-2628
Structural Component Air Fitting
4.377" overall length 1.482" overall width fitting dim are stock matl; -103 opposite
01-523-2629
Structural Component Air Fitting
01-523-2630
Structural Component Air Fitting
3.494" overall length 1.321" overall width 0.100 " material thickness 107 opp -108
01-523-2631
Structural Component Air Fitting
01-523-2632
Structural Component Air Fitting
01-523-2633
Structural Component Air Fitting
3.494" overall length 1.321" overall width 0.100 " material thickness 108 opp -107
01-523-2634
Structural Component Air Fitting
01-523-2956
Aircraft Leading Edge
Panel assy nha 17P6P5806-501; xfvs 217.214-369-710
01-523-2963
Structural Aircraft Plate
5.900" overall length 5.700" overall width 0.080" material thickness access panel dims are stock material; f-2.59; nha is 520-12913 for effectivity L7401-L7402; nha is 520-13301 for effectivity L7401-L7899
01-523-2969
Aircraft Leading Edge
50.000" overall length 28.000" overall width 0.100" material thickness dim. are stock material
01-523-2970
Aircraft Leading Edge
60.000" overall length 28.000" overall width 0.100" material thickness dim. are stock material
01-523-2971
Structural Component Air Bracket
01-523-2972
Structural Component Air Fitting
01-523-2973
Structural Component Air Fitting
01-523-3026
Aircraft Skin
Skin panel replacement
01-523-3178
Aircraft Former
Used on f-18 aircraft. 0.071" material thickness former support
01-523-3179
Aircraft Former
Used on f-18 aircraft. 0.071" material thickness former support
01-523-3180
Aircraft Former
Used on f-18 aircraft. 0.071" material thickness former support
01-523-3181
Aircraft Former
Used on f-18 aircraft. 0.071" material thickness former support
01-523-3250
Fuselage Parts Kit
Used on KC-135.
01-523-3346
Structural Component Air Bracket
Used on f-22 raptor. 2.000" overall length 2.500" overall width bracket length dim. is stock material; m/o 6al-4v (ab-1) ann titanium plate
01-523-3347
Structural Aircraft Panel
3.000" overall length 1.560" overall width plate harness support plate, internal; matl AL2024-T3 clad sheet per ams-qq-a-250/5, .080X1.80X3.20; dim are stock matl
01-523-3348
Structural Aircraft Panel
01-523-3350
Structural Component Air Fitting
01-523-3352
Structural Component Air Fitting
01-523-3353
Structural Component Air Fitting
01-523-3621
Aircraft Pylon Section
The -1 consist of 1 gusset p/n 659-12486-10; 1 skin p/n 659-12486-11; 1 web p/n 659-12486-12; 1 angle p/n 659-12486-3; 1 angle p/n 659-12486-4; 2 bulb seal p/n 659-12486-6; 1 gusset p/n 659-12486-8; 1 bulb seal p/n 659-12486-9
01-523-3815
Aircraft Stiffener
Used on f-16 aircraft.
01-523-3816
Aircraft Stiffener
Used on f-16 aircraft.
01-523-3817
Aircraft Stiffener
Used on f-16 aircraft.
01-523-3818
Aircraft Stiffener
Used on f-16 aircraft.
01-523-4064
Structural Aircraft Plate
3.300" overall length 2.200" overall width 0.050" material thickness plate commercially pure titanium sheet, spec mil-t-9046 type i comp b, anneald; dim are stock material
01-523-4087
Structural Component Air Bracket
2.500" overall length 1.300" overall width 0.500" material thickness clip commercially pure titanium sheet spec mil-t-9046 type i comp b anneald; dim are stock material
01-523-4337
Structural Aircraft Plate
01-523-4344
Aircraft Leading Edge
01-523-4352
Tubing Aircraft Support
1.830" overall length 0.250" overall width navy) block, coiled tube support - double line, stacked item is used to seperate primer epoxy surface treated
01-523-4588
Aircraft Door
Used on f/a-22 raptor. door assembly-exhaust, apu made from 1 each 5HR40310-103, -105, -109, -111 shims; 1 5HR40311-109 door; 1 5HR40317-101 hinge assembly; 1 5HR40325-107 plate; 4 EL1382NN6-10pins; 3 EL1382NN6-6 pins; 6 EL1382NN6-7 pins; 1 EL1382NN6-9 pin; 4 ELEL4382NN5-4 pins; 4 EN1132ND5 nuts; 14 EN1132ND6 nuts
01-523-4631
Structural Component Air Support
01-523-4642
Structural Aircraft Plate
3.500" overall length 0.800" overall width 0.500" material thickness clip dim are stock matl; -63 left hand only
