NSN 4710-00-289-0398
Part Details | METALLIC TUBE
4710-00-289-0398 A straight, hollow product, welded or seamless, of round, square, or any other cross section and continuous periphery, which does not conform in cross sectional dimensions to recognized pipe standards, or those in Tables 1 through 10, Appendix C, FIIG A004A. It is designed to convey fluids, gasses, and/or semisolids. It may be rolled into coils for ease in handling. For items designed to join a tube or tube fitting to another tube, pipe, or hose or fitting, see ADAPTER (as modified); COUPLING (as modified); or NIPPLE (as modified). Excludes TUBE, BENT (as modified); PIPE, METALLIC; SPACER, SLEEVE; METAL BAR (hollow); and items with fittings, except end protectors.
Alternate Parts: MILT8504, 740633, MILT85040.625ODX0.049WALL, MIL-T-85040.625ODX0.049WALL, MILT8504, MIL-T-8504, AMS5567, MILT8504, 4710-00-289-0398, 00-289-0398, 4710002890398, 002890398
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | JAN 01, 1963 | 00-289-0398 | 31979 ( TUBE, METALLIC ) |
REFERENCE DRAWINGS & PICTURES
PLAIN ROUND
PLAIN
PLAIN
Cross Reference | NSN 4710-00-289-0398
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MILT8504 | 06805 | ALL BORO METAL PRODUCTS CO INC |
| 740633 | 80045 | L-3 COMMUNICATIONS CINCINNATIELECTRONICS CORPORATION |
| MIL-T-85040.625ODX0.049WALL | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-T-8504 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AMS5567 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| MILT8504 | 78821 | TD MATERIALS INC |
Technical Data | NSN 4710-00-289-0398
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-8504 MIL SPEC SINGLE MATERIAL RESPONSE |
| MEASURING METHOD AND LENGTH | RN96.000 INCHES MINIMUM AND RN192.000 INCHES MAXIMUM |
| CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| WALL THICKNESS | 0.049 INCHES NOMINAL |
| DIAMETER | 0.625 INCHES NOMINAL |
| FIRST END STYLE | PLAIN |
| SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| CONSTRUCTION | STRAIGHT SEAMED |
| WELDING METHOD | FURNACE BUTT |
| MAXIMUM OPERATING TEMP | -800.0 DEG FAHRENHEIT |
| HEAT TREATMENT | ANNEALED |
| SPECIAL FEATURES | GRUMMAN,A10 AIRCRAFT |
| SPECIFICATION/STANDARD DATA | 81343-MS5567 PROFESSIONAL/INDUSTRIAL ASSOCIATION SPECIFICATION |
