01-430-0414
Structural Aircraft Plate
1.000" overall length 1.000" overall width 0.081" material thickness requested name-clip
01-430-0415
Structural Component Air Bracket
2.090" overall length 1.110" overall width requested name-clip; material-LS6362 x 3
01-430-0419
Structural Component Air Bracket
3.840" overall length 2.080" overall width requested name-clip; p/n 3W29099-126 opposite configuration; material-LS7042 x 3
01-430-0420
Structural Component Air Bracket
3.560" overall length 1.640" overall width requested name-clip; p/n 3W29099-136 opposite configuration; material-LS7042 x 3
01-430-0421
Structural Component Air Bracket
3.710" overall length 2.080" overall width requested name-clip; p/n 3W29099-163 opposite configuration; material-LS7042 x 2
01-430-0422
Structural Component Air Bracket
2.090" overall length 1.110" overall width requested name-clip; material-LS6362 x 2
01-430-0423
Aircraft Channel
14.100" overall length 1.250" overall width 0.250" material thickness matl stainless steel 17-4ph sst, cond H1025; cadmium plate per qq-p-416 ORLAC0491; u/o: repair instl, rib, wing sta 77.7, multi panel replacement
01-430-0424
Structural Component Air Bracket
0.850" overall width requested name-splice angle; p/n 3W29101-116 opposite configuration; material-LS30011-1 x 5
01-430-0425
Structural Aircraft Plate
5.700" overall length 0.750" overall width 0.063" material thickness
01-430-0426
Structural Component Air Bracket
5.380" overall length 1.000" overall width
01-430-0427
Structural Component Air Fitting
2.380" overall length 2.600" overall width
01-430-0428
Structural Component Air Fitting
2.380" overall length 2.600" overall width material:made from 3W21132-992 casting, A360 al alloy; p/n 3W21132-102 opposite configuration
01-430-0429
Structural Aircraft Plate
16.770" overall length 2.750" overall width 0.190" material thickness
01-430-0448
Structural Aircraft Panel
Used on pacer special. smoothness critical item; c/o:plate (-013) , panel, filler, edges, shims, sleevebolts, washers, nuts, valve, pins, retaining ring, sealant, foam & adhesive
01-430-0457
Structural Component Air Bracket
3.750" overall length 2.080" overall width requested name-clip
01-430-0458
Structural Aircraft Plate
28.280" overall length 2.400" overall width 0.400" material thickness
01-430-0459
Structural Component Air Support
23.820" overall length 3.750" overall width 1.320" material thickness
01-430-0460
Structural Component Air Support
27.250" overall length 3.750" overall width 1.320" material thickness
01-430-0461
Structural Aircraft Plate
6.960" overall length 2.680" overall width 0.112" material thickness requested name-spacer
01-430-0464
Structural Aircraft Plate
28.280" overall length 2.400" overall width 0.400" material thickness
01-430-0470
Structural Aircraft Plate
24.000" overall length 4.000" overall width 2.750" material thickness upper bulkhead cap
01-430-0475
Structural Aircraft Plate
3.870" overall length 1.980" overall width 0.071" material thickness requested name-splice plate
01-430-1125
Structural Aircraft Panel
Used on c-130h aircraft.
01-430-1126
Structural Aircraft Panel
Used on c-130h aircraft.
01-430-1127
Structural Aircraft Panel
Used on c-130h aircraft.
01-430-1132
Structural Aircraft Panel
Used on c-130h aircraft.
01-430-1134
Access Aircraft Door
01-430-1135
Access Aircraft Door
Used on c-17a aircraft.
01-430-1138
Access Aircraft Door
Used on c-17a aircraft.
01-430-1139
Access Aircraft Door
01-430-1140
Access Aircraft Door
01-430-2132
Structural Component Air Fitting
C/o 1 fitting, 2 bearing, 2 BUSHING1 die forging; nha L3004500
01-430-2148
Structural Component Air Support
23.100" overall length 1.320" overall width requested name-angle; p/n 3W29098-162 opposite configuration; material:17-4ph sst; heat treat to 155-190 ksi per STP54-013, condition H1025 or mil-h-6875
01-430-2150
Structural Component Air Support
28.000" overall length 1.320" overall width requested name-angle; p/n 3W29098-160 opposite configuration; material:17-4ph sst; heat treat to 155-190 ksi per STP54-013, condition H1025 or mil-h-6875
01-430-2151
Structural Component Air Bracket
1.640" overall length 1.130" overall width requested name-extrusion; material-LS31241 x 2
01-430-2152
Structural Component Air Support
23.820" overall length 1.320" overall width requested name-angle; p/n 3W29098-157 opposite configuration; material:17-4ph sst; heat treat to 155-190 ksi per STP54-013, condition H1025 or mil-h-6875
01-430-2576
Structural Component Air Fitting
C/o:-005 ftg, bearing & bushing; make from -007 die forging, LB0160-180 steel aly HP9-4-20; u/a:fitting, hinge & actuator; n/a: L3004500; u/o acft 1 & subq
01-430-2580
Structural Aircraft Plate
16.850" overall length 2.790" overall width 0.112" material thickness
01-430-2581
Structural Aircraft Plate
34.000" overall length 1.820" overall width 0.080" material thickness requested name-splice strap
01-430-2582
Structural Aircraft Plate
34.000" overall length 1.700" overall width 0.063" material thickness requested name-splice strap
01-430-2583
Structural Component Air Support
20.000" overall length 1.950" overall width 1.850" material thickness requested name-splice angle
01-430-2584
Structural Component Air Support
15.450" overall length 1.250" overall width requested name-splice zee; p/n 3W29100-109 opposite configuration; material-LS3919 x 16
01-430-2585
Structural Aircraft Plate
16.770" overall length 2.750" overall width 0.240" material thickness
01-430-2587
Longeron Repair Kit
Used on f-5f aircraft. c/o: aircraft parts & expendable tools to replace lh
01-430-2589
Windshield Parts Kit
Used on f-5b aircraft. c/o: components & hardware reqd to install composite bird-impact resistant windshield assembly
01-430-2590
Windshield Parts Kit
Used on f-5b/f aircraft. c/o: expendable hardware reqd to install the composite bird-impact resistant windshield assy
01-430-2591
Windshield Parts Kit
Used on f-5f aircraft. c/o: components & hardware reqd to install composite bird-impact resistant windshield assembly
01-430-2842
Aircraft Fairing
Used on f-18c/d hornet aircraft. 0.011" material thickness
01-430-2844
Aircraft Fairing
Used on f-18c/d hornet aircraft. 0.011" material thickness
01-430-2848
Airfoil Rib
Used on f/a-18c/d hornet aircraft. 12.292" overall length
