NSN 4730-00-825-2087
Part Details | TUBE COUPLING NUT
4730-00-825-2087 An internally threaded nut which has either an internal seat or shoulder and/or is designed to be used with a ferrule, to mate with the seat of an externally threaded tube fitting to form a leakproof connection. Excludes NUT (1), TUBE COUPLING, REDUCING; and NUT (1), UNION.
Alternate Parts: MS219213S, MS21921-3S, MS219213S, MS21921-3S, MS219213S, MS21921-3S, MS219213R, MS21921-3R, AS219213S, AS21921-3S, AS219213R, AS21921-3R, AS21921, 4730-00-825-2087, 00-825-2087, 4730008252087, 008252087
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | JAN 01, 1962 | 00-825-2087 | 03859 ( NUT, TUBE COUPLING ) |
REFERENCE DRAWINGS & PICTURES
TUBE COUPLING
Cross Reference | NSN 4730-00-825-2087
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| MS21921-3S | 01276 | EATON-AEROQUIP INCDIV FLUID CONNECTORS PRODUCTS |
| MS21921-3S | 00624 | EATON-AEROQUIP LLC.DBA AEROSPACE GROUP |
| MS21921-3S | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS21921-3R | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS21921-3S | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS21921-3R | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS21921 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 4730-00-825-2087
| Characteristic | Specifications |
|---|---|
| THREAD SERIES | UNF |
| NOMINAL THREAD SIZE | 0.375 INCHES |
| THREAD QUANTITY PER INCH | 24 |
| THREAD CLASS | 3B |
| THREAD DIRECTION | RIGHT-HAND |
| NUT STYLE | TUBE COUPLING |
| NUT HEIGHT | 0.570 INCHES MINIMUM AND 0.590 INCHES MAXIMUM |
| WIDTH ACROSS FLATS | 0.438 INCHES NOMINAL |
| LENGTH TO SHOULDER | 0.419 INCHES MINIMUM AND 0.439 INCHES MAXIMUM |
| SMALLEST INSIDE DIAMETER | 0.232 INCHES MINIMUM AND 0.237 INCHES MAXIMUM |
| SEAT ANGLE | 45.00 DEGREES NOMINAL |
| FABRICATION METHOD | |
| NOMINAL TUBE OUTSIDE DIAMETER | 0.188 INCHES |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| SPECIFICATION/STANDARD DATA | 96906-MS21921 GOVERNMENT STANDARD |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | AIRCRAFT, F-16 |