01-458-9345
Structural Aircraft Plate
22.750" overall length 22.000" overall width 0.140" material thickness doubler
01-458-9346
Structural Component Air Support
22.000" overall length 1.920" overall width 1.620" material thickness angle
01-458-9348
Structural Aircraft Plate
15.480" overall length 2.900" overall width 0.100" material thickness
01-458-9349
Structural Component Air Support
1.600" overall length 1.500" overall width 1.000" material thickness angle
01-458-9351
Structural Aircraft Plate
3.550" overall length 1.600" overall width 0.063" material thickness
01-458-9353
Structural Component Air Support
9.700" overall length 2.600" overall width 0.750" material thickness angle
01-458-9354
Structural Component Air Support
Used on b-2 aircraft/pacer special. aft deck assembly manufacturer suggested name: mod instl - aft deck replacement, ca, rh;
01-458-9357
Structural Component Air Support
Used on b-2 aircraft/pacer special. aft deck assy manufacturer suggested name: mod instl - aft deck replacement, ca; c/o: mod instl-rh (DAA3123M278-002) & mod kit-rh (DAA3123M289-002)
01-458-9943
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -016
01-458-9945
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; opp -015
01-458-9946
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -021
01-458-9948
Structural Component Air Support
3.190" overall length 2.250" overall width h-clip
01-458-9950
Structural Component Air Support
37.030" overall length angle heat treatment per stp 54-101; p/N3W31746-101 is the opposite configuration
01-458-9952
Aircraft Stiffener
18.020" overall length 2.060" overall width 1.500" material thickness
01-458-9960
Structural Component Air Support
3.450" overall length 2.250" overall width h-clip
01-458-9961
Structural Component Air Support
37.030" overall length angle heat treatment per stp 54-101; p/N3W31746-102 is the opposite configuration
01-458-9962
Structural Component Air Support
9.630" overall length 0.700" overall width angle
01-458-9964
Structural Aircraft Plate
8.500" overall length 1.000" overall width 0.112" material thickness filler
01-458-9966
Structural Component Air Support
23.100" overall length 3.750" overall width 1.320" material thickness angle cadmium surface treated
01-458-9968
Structural Component Air Support
27.250" overall length 2.518" overall width 1.320" material thickness angle cadmium surface treated
01-458-9969
Aircraft Channel
15.000" overall length 2.000" overall width
01-458-9970
Structural Component Air Support
10.000" overall length 2.000" overall width 0.500" material thickness angle
01-458-9971
Structural Component Air Support
24.000" overall length 4.000" overall width angle part of repair installation, inner wing, lower, p/n 3W29098-105 for panel 4 repair; material:ti-6al-4v sta
01-458-9972
Structural Aircraft Plate
7.250" overall length 1.000" overall width 0.112" material thickness filler
01-458-9973
Structural Component Air Support
28.000" overall length 4.000" overall width angle part of repair installation, inner wing, lower, p/n 3W29098-104 for panel 3 repair; material:ti-6al-4v sta
01-458-9974
Structural Component Air Support
24.000" overall length 4.000" overall width angle part of repair installation, inner wing, lower, p/n 3W29098-106 for panel 4 repair; material:ti-6al-4v sta
01-458-9975
Structural Component Air Support
28.000" overall length 3.750" overall width 1.320" material thickness angle
01-459-0092
Bleed Air Duct Assembly
Used on aircraft c-17a.
01-459-0116
Structural Component Air Support
01-459-0317
Structural Component Air Support
41.380" overall length angle p/n 3W31747-102 is the opposite configuration
01-459-0318
Structural Component Air Support
39.120" overall length 2.250" overall width 1.700" material thickness angle
01-459-0319
Structural Component Air Support
40.250" overall length angle p/n 3W31754-102 is the opposite configuration
01-459-0320
Structural Component Air Support
40.250" overall length 4.030" overall width 1.700" material thickness angle
01-459-0322
Structural Component Air Support
23.820" overall length 3.750" overall width 1.320" material thickness angle
01-459-0323
Structural Component Air Support
40.150" overall length 1.900" overall width 1.700" material thickness angle
01-459-0324
Structural Component Air Support
40.120" overall length 2.620" overall width 1.700" material thickness angle
01-459-0325
Structural Component Air Support
39.120" overall length 2.250" overall width 1.700" material thickness angle
01-459-0326
Structural Component Air Support
41.380" overall length angle p/n 3W31747-101 is the opposite configuration
01-459-0327
Structural Component Air Support
40.250" overall length 1.900" overall width 1.700" material thickness angle
01-459-0328
Structural Component Air Support
40.150" overall length 1.900" overall width 1.700" material thickness angle
01-459-0329
Structural Aircraft Plate
9.000" overall length 2.000" overall width 0.112" material thickness filler part of repair installation, inner wing, lower, p/ns 3W29098-105/-106 for panel 4 replacement
01-459-0330
Structural Component Air Support
40.250" overall length 4.030" overall width 1.700" material thickness angle
01-459-0333
Structural Component Air Support
23.820" overall length 3.750" overall width 1.320" material thickness angle
01-459-0335
Structural Aircraft Plate
9.700" overall length 2.150" overall width 0.080" material thickness
01-459-0336
Structural Aircraft Plate
3.300" overall length 1.600" overall width 0.063" material thickness filler
01-459-0337
Structural Component Air Support
40.250" overall length 1.900" overall width 1.700" material thickness angle
01-459-0340
Structural Component Air Support
40.250" overall length angle p/n 3W31754-101 is the opposite configuration
01-459-0343
Structural Aircraft Plate
45.000" overall length 22.180" overall width 0.125" material thickness doubler
01-459-0713
Structural Component Air Support
28.000" overall length 3.750" overall width 1.320" material thickness angle cadmium surface treated
01-459-0714
Structural Aircraft Plate
22.350" overall length 19.620" overall width 0.140" material thickness doubler
