01-395-3926
Structural Component Air Bracket
Used on cp140 aurora, lockheed corp, georgia co. div.
01-395-4102
Structural Component Air Support
01-395-4103
Structural Aircraft Panel
01-395-4108
Aircraft Window Panel
Used on c-130 aircraft.
01-395-4867
Structural Aircraft Panel
01-395-4875
Thermal Special Purpo Insulation
01-395-4917
Structural Component Air Bracket
Used on pacer special. smoothness critical item; nha-002; used as a clip
01-395-5187
Structural Aircraft Panel
01-395-5188
Aircraft Channel
Used on c-130h aircraft. used on glareshield, cockpit windshield
01-395-5190
Structural Component Air Bracket
01-395-5191
Structural Component Air Bracket
01-395-5192
Structural Aircraft Panel
01-395-5193
Structural Component Air Bracket
01-395-5231
Aircraft Skin
Skin assy, top center section; mxu-777a/a;
01-395-5341
Aircraft Frame
Used on pacer special.
01-395-5342
Access Aircraft Cover
Used on b-2 pacer special. nha DAA3121B009-155, -156, -273, -274, DAA3121B134-001, -002, -179, -180; used on i.s. fuel cell access door assembly
01-395-5343
Aircraft Floor
Matl: alum-balsa; c/o: 1 panel, 10 spacer plugs, 20 spacer sleeves, 40 spacers; nha: 204-30543, 204-31283,
01-395-5344
Structural Aircraft Panel
Nha 204-30560; finish f-2.10; BMS4-10 type i, grade 3
01-395-5345
Aircraft Spar
231.000" overall length BAC1506-986; finish f.2.22
01-395-5346
Aircraft Spar
231.000" overall length opposite -8; BAC1506-986; finish f-2.22
01-395-5347
Aircraft Spar
231.000" overall length opp -010; matl per bac 1506-985; T6 temper; fin: f-2.22 & f-2.30 shown shown on drawing & allow no primer on surfaces calling for f-2.22
01-395-5348
Aircraft Beam
20.100" overall length opposite -71; make from BAC1517-1098
01-395-5349
Structural Component Aircraf Web
134.500" overall length 7.500" overall width 0.051" material thickness u/a a reinforcing web; T6 temper; finish f-2.115
01-395-5350
Aircraft Spar
135.000" overall length heat treat T42; finish f-2.30; bac 1514-1107; used as aft chord
01-395-5351
Aircraft Spar
135.000" overall length used as fwd chord; heat treat T42; finish f-2.30; BAC1514-1106
01-395-5352
Aircraft Beam
23.000" overall length make from AND10140-4003; heat treat T6; finish f-2.30
01-395-5909
Structural Aircraft Plate
Used on c-130h aircraft.
01-395-5910
Structural Component Air Support
01-395-5911
Aircraft Strut
01-395-5912
Aircraft Strut
01-395-5915
Structural Aircraft Panel
01-395-5919
Thermal Insulation Pipe Covering
Used on c-130 hercules aircraft. polycarbonate; cover-cooling duct, lpcr-130-1 radar
01-395-6192
Aircraft Beam
20.100" overall length u/a:zee beam; T6 temper; matl bac 1517-1098; fin f-2.30
01-395-6193
Aircraft Beam
204.000" overall length 42.500" overall width u/a:bulkhead beam; T6 temper; FINF2.30; matl bac 1518
01-395-6196
Aircraft Beam
Matl:alter bac 1818-196
01-395-6198
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp -021; u/o acft 6 & subq
01-395-6220
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp-021; u/o acft 16 & subq
01-395-6221
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp -011; u/o acft 6 & subq
01-395-6222
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp -012; u/o acft 6 & subq
01-395-6223
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp -022; u/o acft 6 & subq
01-395-6224
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp-021; u/o acft 9 & subq
01-395-6225
Aircraft Floor
35.000" overall length 8.200" overall width opp -3039
01-395-6226
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp-012; u/o acft 1 only
01-395-6612
Aircraft Stiffener
01-395-6741
Structural Aircraft Plate
01-395-6742
Structural Aircraft Plate
01-395-6745
Access Aircraft Door
Used on b-2 aircraft-pacer special. manufacturer suggested name: door assy; u/o: duct instl-is, egw, X167, Y392; c/o: bond assy, rivets, sealant, seal strips, & retainers
01-395-6746
Access Hole Aircraft Frame
Part of closeout assy-is Y408.76-X181.88; make from -016; next higher assy DAA3121B062-002; pacer special
01-395-6747
Structural Aircraft Plate
Nuclear hardness critical item; u/a:ram shroud; c/o:honeycomb cores, inner & outer face sh, closeouts & foam absorbers; opp -022; u/o acft 9 & subq
01-395-6753
Aircraft Floor
79.000" overall length 45.400" overall width c/o:-5 panel, sleeve-spacers, andplug spacers; matl:alum face shts
