01-325-1601
Metal Bar
Used on AH-64A.
01-327-9524
Metal Bar
100 pct macro etc hed both ends
01-328-2107
Metal Bar
Used on steam catapults.
01-328-2108
Metal Bar
Used on steam catapults.
01-332-6413
Metal Bar
Used on s70b-2 seahawk helicopter.
01-336-3327
Metal Bar
0.500 in. flange
01-338-3068
Metal Bar
4340 mil-s-5000 annealed; pickled, or sandblasted
01-345-0475
Metal Bar
Corrosion resistant; limited to spot welding
01-345-5669
Metal Bar
Mercury exclusion clause
01-352-1235
Metal Bar
Used on c-5b acft.
01-352-1707
Metal Bar
Round; aircraft quality; hardness; rockwell c-50; grain sz: no.5 or finer; cold drawn; annealed; dia 4"; intended for highly stressed aircraft parts requiring high hardenability
01-354-3815
Metal Bar
Used on b-1b acft.
01-354-3816
Metal Bar
Used on b-1b acft.
01-354-4304
Metal Bar
Used on b-1b acft.
01-354-6964
Metal Bar
Corrosion resistant; condition a; elongation 40; tensile strenght 25, 000psi, yield strenght 70, 000psi
01-354-6965
Metal Bar
Corrosion resistant; condition a; elongation 40; tensile strenght 25, 000psi; yield strenght 70, 000psi
01-354-6967
Metal Bar
Corrosion resistant; condition a; elongation 35; tensile strenght 30, 000psi, yield strenght 75, 000psi
01-362-3880
Metal Bar
Corrosion resisting; condition a; tensile strength: 70, 000 psi; yield strength: 30, 000 psi; elongation: 65 percent
01-362-4558
Metal Bar
Used on f-15e acft common bulk item.
01-362-4559
Metal Bar
Used on f-15e acft common bulk item. matl uns K66286, a-286 or iron alloy 660
01-362-4562
Metal Bar
Used on f-15e acft common bulk item.
01-362-8640
Metal Bar
Etensile strength: psi: 125, 000 min.; yield strength: psi: 100, 000 min.; aircraft quality; condition: f; rockwell hardness: c-21; elongation: 17 percent; for use in manufactoring parts
01-362-8641
Metal Bar
Corrosion resistant; length; random; tensile strength: 130, 000 psi; yield strength: 85, 000 psi; elongation: 15 percent; hardness rating: 248-341 hb
01-362-8642
Metal Bar
Ltensile strength: psi: 150, 000 min.; yield strength: psi: 130, 000 min.; rockwell hardness: C22; elongation: 14 percent; for use in the manufacturing of highly stressed aircraft parts requiring high hardenability
