01-530-4023
Aircraft Skin
144.000" overall length 75.000" overall width skin, upper lobe replaces -119a; clad (1) side; dim.are stock matl.; ecn 2005C0001; new p/n for crown skins for more corrosion stress resistant
01-530-4059
Aircraft Door
Used on V-22. door assembly, aircraft essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-530-4068
Structural Component Air Support
01-530-4118
Structural Component Air Fitting
Used on b-1b lancer. 14.000" overall length 13.750" overall width 4.025 " material thickness fitting matl AMS5604 cress plate ALLOY17-4ph cond H1025; dim are stock matl
01-530-4159
Structural Component Air Bracket
Bracket
01-530-4475
Aircraft Skin
86.000" overall length 67.000" overall width skin matl al 7475-0, STM07-120 cond T761; -128a replaces the - 114a skin; dim are stock matl
01-530-4478
Bleed Air Duct Assembly
24.250" overall length 4.500" overall width 0.010" material thickness duct matl duct end AL6061-T6, qq-a-250/11 temp T6
01-530-4479
Bleed Air Duct Assembly
Nha 17P2N9004; u/o 17A001-34, 17T001 acft
01-530-4566
Aircraft Former
01-530-4630
Structural Aircraft Panel
Used on f/a-22 raptor. door instl-inbd pylon
01-530-4631
Structural Aircraft Panel
Used on a/f-22 raptor. door instl-inbd pylon
01-530-4632
Aircraft Skin
167.000" overall length 63.000" overall width skin gmatl al 7475-0 cond-T761, STM07-120; dim are stock material; the -120a replaces -102a; new p/n for replacement skins for c-5a model, new skins are to be more stress corrosion resistant than existing skins
01-530-4633
Aircraft Skin
182.000" overall length 63.000" overall width skin bmatl al 7475-0 cond-T761, STM07-120; dim are stock material; new p/n for replacement skins for c-5a model, new skins to be more stress corrosion resitant than existing skins; the -121a replaces -103a
01-530-4741
Structural Component Air Support
Used on a-10a thunderbolt ii. seal seal assy -3, -4, -5, -7, -9, -10
01-530-4751
Structural Component Air Support
Used on a-10a thunderbolt ii. seal seal assy -3, -4, -5, -7, -9, -10
01-530-4830
Aircraft Bulkhead
01-530-4836
Structural Aircraft Panel
01-530-4837
Structural Component Aircraf Web
27.000" overall length 11.000" overall width 0.090" material thickness dim. are stock material
01-530-5050
Aircraft Skin
01-530-5052
Aircraft Skin
Used on C-5. 174.000" overall length 63.000" overall width heat treat cond-T761; clad; nha 4F42001; dim. are stock matl. size; replaces -104a skin
01-530-5073
Structural Component Air Support
Used on A-10A. seal assembly alcd sh, heat treat T6; c/o -39 retainer, -41 retainer
01-530-5077
Structural Component Air Support
Used on A-10A. seal assembly alcd sh heat treat T6; c/o -39 retainer, -41 retainer
01-530-5121
Structural Aircraft Plate
01-530-5124
Structural Component Air Support
Used on a-10 acft thunderbolt ii. seal seal assy -3, -4, -5, -10
01-530-5270
Structural Component Air Bracket
Used on c-2a; angle, power plant-oilcooler exit flap. 19.000" overall length 7.000" overall width 0.045" material thickness navy: angle assembly alodine before primer, epoxy polymide primer epoxy-polyamide surface treated
01-530-5290
Structural Component Air Bracket
Used on e-2c; channel, cont surf-inbd ruddder. 15.000" overall length 3.000" overall width 0.020" material thickness navy: angle assembly coating, anodize, sulfric acid, non dyed, sealed primer, epoxy, polymide; next higher assembly= 123CS11804 anodize surface treated
01-530-5359
Access Aircraft Door
Used on f/a-22 raptor. access inboard pylon
01-530-5363
Access Aircraft Door
Used on f/a-22 raptor. access outboard pylon
01-530-5364
Access Aircraft Door
Used on f/a-22 raptor. access inboard pylon
01-530-5368
Access Aircraft Door
01-530-5709
Structural Component Air Support
Used on FILLER. 1.200" overall length 1.060" overall width 0.090" material thickness support fairing fwd upper aileron heat treat T3
01-530-5891
Aircraft Skin
Used on a-10a thunderbolt ii. 60.000" overall length skin engineering order 05A1605 adds sheet 5 to to show -7
01-530-5998
Structural Component Air Support
3.200" overall length 3.100" overall width 0.032" material thickness tab matl al 2024-0 ht-T4; -25 opposite; dim are stock matl
01-530-6007
Structural Component Air Support
3.000" overall length 2.800" overall width 0.032" material thickness tab matl al 2024 -0 ht-4; dim are stock matl
01-530-6011
Structural Component Air Support
2.900" overall length 2.800" overall width 0.032" material thickness tab dim are stock matl; opp -27
01-530-6018
Aircraft Fairing
3.900" overall length 2.200" overall width 0.025" material thickness opposite of -514
01-530-6019
Structural Component Air Support
3.200" overall length 3.100" overall width 0.032" material thickness bulkhead opposite -21 1560-01-530-6214
01-530-6026
Structural Component Air Support
2.500" overall length 2.200" overall width 0.032" material thickness tab dim are stock matl; opp -35
01-530-6029
Structural Component Air Support
2.800" overall length 2.500" overall width 0.032" material thickness bulkhead opposite -32 1560-01-530-6047
01-530-6038
Structural Component Air Support
2.600" overall length 2.500" overall width 0.032" material thickness bulkhead dim. are stock material; finnish per f-2.115; opposite of -34 1560-01-530-6183
01-530-6047
Structural Component Air Support
2.600" overall length 2.500" overall width 0.032" material thickness bulkhead opposite -31 1560-01-530-6029
01-530-6053
Structural Component Air Support
3.200" overall length 3.100" overall width 0.032" material thickness bulkhead dim. are stock material; finnish per f-2.115
01-530-6183
Structural Component Air Support
Used on c-135 acft bulkhead. 2.600" overall length 2.500" overall width 0.032" material thickness bulkhead-tab, elevator heat treat 0; clad sheet; opp -33; clip, intercostal; opposite of -33 1560-01-530-6038
01-530-6199
Structural Component Air Support
01-530-6202
Structural Component Air Support
01-530-6207
Structural Component Air Support
01-530-6209
Structural Component Air Support
01-530-6214
Structural Component Air Support
Used on c-135 acft. 3.500" overall length 2.600" overall width 0.032" material thickness bulkhead tab spar, elevator opposite -22 1560-01-530-6019
01-530-6292
Structural Component Air Support
Used on c-135 acft. 2.500" overall length 2.200" overall width 0.032" material thickness bulkhead-tab spar, elevator heat treat 0; clad sheet
01-530-6312
Aircraft Skin
174.000" overall length 63.000" overall width replaces -101a skin; heat treat T761
