01-530-2583
Aircraft Door
Used on v22 aircraft. essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-530-2593
Structural Aircraft Panel
Used on v22 aircraft. essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-530-2599
Structural Component Air Bracket
Used on v-22 lrip 1 e-nsn isil. (navy) bracket assembly, ai essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-530-2759
Structural Component Air Fitting
Used on c-130 acft. fitting - floor to ring bhd nha 35625h; u/o c-130 acft; make from 356183-3
01-530-2770
Structural Aircraft Plate
6.920" overall length 4.019" overall width 1.011" material thickness doubler u/o acft 83-0065 thru 86-0140; nha L1600042
01-530-2774
Structural Aircraft Plate
5.470" overall length 4.802" overall width 1.849" material thickness doubler u/o acft 83-0065 thru 86-0140; nha L1600042
01-530-2778
Structural Aircraft Plate
5.680" overall length 5.100" overall width doubler u/o acft 83-0065 thru 86-0140; nha L1600042
01-530-2787
Structural Component Air Support
27.100" overall length 6.900" overall width 0.050" material thickness frame matl al 2024-0 clad sheet, qq-a-462 temp-0; dim are stock matl
01-530-2803
Access Aircraft Door
Used on inlet barrier, uh-60 blackhawk helicopter. door-bypass rh
01-530-2804
Structural Component Air Support
27.100" overall length 7.100" overall width 0.063" material thickness frame matl al 2024-0, clad sheet, qq-a-462 0 temp; dim are stock matl
01-530-2808
Access Aircraft Door
Used on inlet barrier, uh-60 blackhawk helicopter. door - bypass lh
01-530-2812
Aircraft Fairing
Used on inlet barrier, uh-60 blackhawk helicopter. assy-module, filter lh
01-530-2816
Aircraft Fairing
Used on inlet barrier, uh-60 blackhawk helicopter. assy-module, filter rh
01-530-2819
Structural Component Air Support
Used on inlet barrier, uh-60 blackhawk helicopter. brace, nacelle, filter, open
01-530-2824
Structural Component Air Support
Used on inlet barrier, uh-60 blackhawk helicopter. strut, upr
01-530-2826
Structural Component Air Support
Used on inlet barrier, uh-60 blackhawk helicopter. strut, lwr
01-530-2924
Fuel Aircraft Cell
Used on kc-135r/t acft. fuel cell bladder no. 1 forward body; nitrile const. modification
01-530-2926
Fuel Aircraft Cell
Used on kc-135r/t acft. fuel cell bladder no. 2 forward body, nitrile const. modification
01-530-2975
Structural Component Air Support
27.100" overall length 7.200" overall width 0.063" material thickness frame matl al 2024-0, clad sheet, qq-a-462, temp 0; dim are stock matl
01-530-2980
Structural Component Air Support
27.100" overall length 7.200" overall width 0.063" material thickness frame matl al 2024-0, clad sheet, qq-a-462, temp-0; dim are stock matl
01-530-2986
Structural Component Air Support
27.100" overall length 7.400" overall width 0.063" material thickness frame matl al 2024-0, clad sheet, qq-a-462, temp 0; dim are stock matl
01-530-3036
Structural Component Air Fitting
Used on b1 acft. 4.250" overall length 2.000" overall width 1.250 " material thickness angle AMS5604, cres plate, alloy 17-4ph, cond H1025
01-530-3072
Structural Component Air Support
T-angle crown structure instl, kit 40 body extension phase 6 ecm
01-530-3092
Structural Component Air Fitting
17.750" overall length 14.000" overall width 4.250 " material thickness fitting, support-no. 1&2 spoiler wing panel, assy of ams 5604, cres plate, ALLOY17-4ph, cond H1025
01-530-3146
Structural Component Air Fitting
Used on b1 acft. fitting, support no. 1&2 spoiler, wing panel, assy of ams 5604, cres plate, ALLOY17-4ph cond H1025
01-530-3196
Aircraft Latch Assembly
Trigger lock latch
01-530-3211
Aircraft Latch Assembly
Used on boeing 757 aircraft. latch assembly
01-530-3263
Aircraft Skin
102.000" overall length 67.000" overall width
01-530-3266
Aircraft Skin
146.000" overall length 64.000" overall width
01-530-3394
Structural Component Air Fitting
Used on b-1b lancer. 4.250" overall length 1.000" overall width 0.125 " material thickness strap matl cres steel plate ALLOY17-4ph cond H1025; dim are stock matl
01-530-3437
Structural Aircraft Plate
Used on b-1b aircraft. 6.910" overall length 5.010" overall width 0.530" material thickness alum plate; nha L1600042; effectivity on b-1b 83-0065 thru 86-0140 (acft 2 thru 100) ; heat treat T7351
01-530-3440
Structural Aircraft Plate
Used on b-1b aircraft. 5.730" overall length 4.790" overall width 0.490" material thickness heat treat T7351; nha L1600042; plate/alum; effectivity 83-0065 thru 86-0140 (acft 2 thru 100)
01-530-3441
Structural Aircraft Plate
Used on b-1b aircraft. 7.550" overall length 4.830" overall width 0.878" material thickness heat treat T7351; nha L1600042; effectivity suitable for b-1b acft 2 thru 100, 83-0065 thru 86-0140.
01-530-3529
Aircraft Leading Edge
92.000" overall length passivate surface treated
01-530-3559
Structural Aircraft Plate
35.000" overall length 1.600" overall width 0.040" material thickness retainer dim. are stock material; nha 160D891700
01-530-3655
Structural Component Air Fitting
Used on EA-6B. navy: fitting assembly
01-530-3678
Fuel Aircraft Cell
Used on king air, u-21 and c-12. fuel cell
01-530-3679
Fuel Aircraft Cell
Used on king air, u-21 and c-12. fuel cell velc. hgr
01-530-3689
Aircraft Latch Assembly
Used on b757 boeing aircraft. panel station 740 to 1277.2 equipment
01-530-3781
Structural Component Air Fitting
Used on EA-6B. navy: fitting assembly next higher assembly 1128B40223
01-530-3799
Structural Component Air Fitting
Used on EA-6B. navy: fitting assembly next higher assembly 1128B40223
01-530-3808
Structural Component Air Fitting
01-530-3974
Access Aircraft Door
01-530-3993
Structural Aircraft Panel
Used on f/a-22 raptor.
01-530-3996
Structural Aircraft Panel
Used on f/a-22 raptor.
01-530-4015
Structural Aircraft Panel
Used on f/a-22 raptor. door instl
01-530-4016
Structural Aircraft Panel
Used on f/a-22 raptor. door instl
01-530-4017
Structural Aircraft Panel
Used on f/a-22 raptor. door instl
01-530-4021
Aircraft Skin
160.000" overall length 64.000" overall width skin, upper lobe dengineering order no.2004C0001; matl AL7475-0, STM07-120 cond T761; new part no. for crown skins of -105a (model a)
01-530-4022
Aircraft Skin
138.000" overall length 75.000" overall width replaces-120a; clad (1) side; heat treat T61; dim. are stock matl; ecn 2005C0001; new p/n for crown skins for more corrosion stress resistant
