NSN 4710-00-278-3305
Part Details | METALLIC TUBE
4710-00-278-3305 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: MHC241, FMS1080B, FMS 1080, MILT6845, MIL-T-6845, FMS1080B, AMST6845 TYPE 1, AMS-T-6845 TYPE 1, 304625T, 304-625T, FMS1080B, 4710-00-278-3305, 00-278-3305, 4710002783305, 002783305
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | JAN 01, 1963 | 00-278-3305 | 31979 ( TUBE, METALLIC ) |
REFERENCE DRAWINGS & PICTURES
PLAIN ROUND
PLAIN
PLAIN
Cross Reference | NSN 4710-00-278-3305
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MHC241 | 0VP52 | FINCANTIERI MARINE SYSTEMS NORTHAMERICA, INC. |
| FMS1080B | 85426 | JOHNSON MATTHEY INC |
| FMS 1080 | 81755 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MIL-T-6845 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| FMS1080B | 85577 | PACIFIC TUBE CO |
| AMS-T-6845 TYPE 1 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 304-625T | 78821 | TD MATERIALS INC |
| FMS1080B | 98413 | WALL TUBE AND METAL PRODUCTS COSUB OF PHILLIPS PETROLEUM CO |
Technical Data | NSN 4710-00-278-3305
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 1045 |
| MEASURING METHOD AND LENGTH | RN60.000 INCHES MINIMUM AND RN240.000 INCHES MAXIMUM |
| CROSS-SECTIONAL SHAPE STYLE | PLAIN ROUND |
| WALL THICKNESS | 0.035 INCHES NOMINAL |
| DIAMETER | 0.625 INCHES NOMINAL |
| FIRST END STYLE | PLAIN |
| SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
| CONSTRUCTION | SEAMLESS |
| MAXIMUM OPERATING PRESSURE | 3000.0 POUNDS PER SQUARE INCH |
| MAXIMUM OPERATING TEMP | 800.0 DEG FAHRENHEIT |
| HEAT TREATMENT | COLD DRAWN 1/8 HARD CONDITION |
| SURFACE CONDITION AND LOCATION | OUTSIDE POLISHED |
| SPECIAL FEATURES | AEROSPACE VEHICLE HYDRAULIC SYSTEM |
| SPECIFICATION/STANDARD DATA | 81349-MIL-T-6845 GOVERNMENT SPECIFICATION |
| NONDEFINITIVE SPEC/STD DATA | 1 TYPE |
| END ITEM IDENTIFICATION | GRUMMAN A10 AIRCRAFT |
