NSN 4730-00-461-3639
Part Details | TUBE COUPLING NUT
4730-00-461-3639 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: 48F8, 1110X10, 48F8, 1110X10, 41FS58, 41FS5-8, MS391668, MS39166-8, 41FS10, 41FS-10, 21045109445, 210-4510944-5, 21D45109445, 21D4510944-5, 10 010110B, SAE J512 10 010110B, J512, 4730-00-461-3639, 00-461-3639, 4730004613639, 004613639
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | MAY 09, 1969 | 00-461-3639 | 03859 ( NUT, TUBE COUPLING ) |
REFERENCE DRAWINGS & PICTURES
TUBE COUPLING
Cross Reference | NSN 4730-00-461-3639
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 48F8 | 12603 | CLARK EQUIPMENT CO |
| 1110X10 | 79470 | DANA CORPWEATHERHEAD DIV |
| 48F8 | 77237 | DANA OFF HIGHWAY PRODUCTS, LLC |
| 1110X10 | 01276 | EATON-AEROQUIP INCDIV FLUID CONNECTORS PRODUCTS |
| 41FS5-8 | 30327 | IMPERIAL |
| MS39166-8 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| 41FS-10 | 93061 | PARKER-HANNIFIN CORPORATIONDBA FLUID SYSTEM CONNECTORS DIVISION |
| 210-4510944-5 | 51563 | ROHR, INCDBA GOODRICH AEROSTRUCTURES GROUP |
| 21D4510944-5 | 51563 | ROHR, INCDBA GOODRICH AEROSTRUCTURES GROUP |
| 10 010110B | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| SAE J512 10 010110B | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| J512 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 4730-00-461-3639
| Characteristic | Specifications |
|---|---|
| THREAD SERIES | UNF |
| NOMINAL THREAD SIZE | 0.875 INCHES |
| THREAD QUANTITY PER INCH | 14 |
| THREAD CLASS | 2B |
| THREAD DIRECTION | RIGHT-HAND |
| NUT STYLE | TUBE COUPLING |
| NUT HEIGHT | 1.312 INCHES NOMINAL |
| WIDTH ACROSS FLATS | 1.063 INCHES NOMINAL |
| LENGTH TO SHOULDER | 0.750 INCHES NOMINAL |
| SMALLEST INSIDE DIAMETER | 0.630 INCHES MINIMUM AND 0.635 INCHES MAXIMUM |
| SEAT ANGLE | 45.00 DEGREES NOMINAL |
| FABRICATION METHOD | |
| NOMINAL TUBE OUTSIDE DIAMETER | 0.625 INCHES |
| SPECIFICATION/STANDARD DATA | 81343-J512 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| NONDEFINITIVE SPEC/STD DATA | 4 FIGURE |
| END ITEM IDENTIFICATION | 92F SUPPORT EQUIPMENT, F-16 AIRCRAFT |