NSN 4730-01-383-5621
Part Details | FLUID PASSAGE BOLT
4730-01-383-5621 A boltlike item having a concentric hole along the longitudinal centerline which may extend a part or the full length of the item. It has a hole(s) perpendicular to the axis, joining or passing through the concentric hole along the longitudinal centerline. The item is designed to distribute fluid, air, or lubricant through its body to a mating item, such as a CONNECTOR, MULTIPLE, FLUID PRESSURE LINE, bearing(s), bushing(s), or the like. The item must be capable of attaching to a block fitting and/or a tubing line or be designed to accommodate a FITTING, LUBRICATION. Excludes BOLT, INTERNALLY RELIEVED BODY; BLEEDER VALVE, HYDRAULIC SYSTEM; and BUSHING, MACHINE THREAD. See also PIN, VEHICULAR LEAF SPRING SHACKLE.
Alternate Parts: 17P6W824717, 17P6W8247-17, 17P6W8247, 4730-01-383-5621, 01-383-5621, 4730013835621, 013835621
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | NOV 25, 1993 | 01-383-5621 | 18683 ( BOLT, FLUID PASSAGE ) |
REFERENCE DRAWINGS & PICTURES
SHOULDER
GASKET SEAL COMPRESSION
PLAIN
GASKET SEAL COMPRESSION
PLAIN
HEXAGON
Cross Reference | NSN 4730-01-383-5621
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17P6W8247-17 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 17P6W8247 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 4730-01-383-5621
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| SURFACE TREATMENT | CHROMATE |
| BODY STYLE | SHOULDER |
| CONCENTRIC HOLE DEPTH | 2.153 INCHES MINIMUM AND 2.163 INCHES MAXIMUM |
| CONCENTRIC HOLE DIAMETER | 0.107 INCHES MINIMUM AND 0.114 INCHES MAXIMUM |
| OVERALL LENGTH | 4.867 INCHES MINIMUM AND 4.912 INCHES MAXIMUM |
| FIRST DIAMETER FROM WRENCHING FEATURE | 1.212 INCHES MINIMUM AND 1.242 INCHES MAXIMUM |
| SECOND DIAMETER FROM WRENCHING FEATURE | 0.893 INCHES MINIMUM AND 0.944 INCHES MAXIMUM |
| LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO END OF FIRST DIAMETER | 2.898 INCHES MINIMUM AND 2.908 INCHES MAXIMUM |
| LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO END OF SECOND DIAMETER | 3.134 INCHES MINIMUM AND 3.159 INCHES MAXIMUM |
| FIRST RADIAL FLUID HOLE DIAMETER | 0.107 INCHES MINIMUM AND 0.114 INCHES MAXIMUM |
| DISTANCE FROM FIRST RADIAL HOLE CENTER TO END OF BOLT | 2.089 INCHES MINIMUM AND 2.109 INCHES MAXIMUM |
| LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO BOLT END | 4.242 INCHES MINIMUM AND 4.272 INCHES MAXIMUM |
| WRENCHING FEATURE HEIGHT | 0.625 INCHES MINIMUM AND 0.640 INCHES MAXIMUM |
| FIRST END CONNECTION TYPE | THREADED EXTERNAL TUBE |
| FIRST END STYLE DESIGNATOR | PLAIN |
| FIRST END THREAD SERIES DESIGNATOR | UNJF |
| FIRST END NOMINAL THREAD SIZE | 1.000 INCHES |
| FIRST END THREAD CLASS | 3A |
| FIRST END THREAD DIRECTION | RIGHT-HAND |
| FIRST END THREAD LENGTH | 1.108 INCHES MINIMUM AND 1.113 INCHES MAXIMUM |
| SECOND END CONNECTION TYPE | THREADED INTERNAL TUBE |
| SECOND END STYLE DESIGNATOR | 4 GASKET SEAL COMPRESSION |
| SECOND END SEAT RADIUS | 0.015 INCHES NOMINAL |
| SECOND END THREAD SERIES DESIGNATOR | UNF |
| SECOND END NOMINAL THREAD SIZE | 0.250 INCHES |
| SECOND END THREAD CLASS | 3B |
| SECOND END THREAD DIRECTION | RIGHT-HAND |
| SECOND END THREAD LENGTH | 0.250 INCHES NOMINAL |
| WRENCHING FEATURE STYLE | HEXAGON |
| WIDTH ACROSS FLATS | 1.801 INCHES MINIMUM AND 1.815 INCHES MAXIMUM |
| SPECIAL FEATURES | FURNISHED WITH A LUBICATION FITTING LOCATED ON SECOND END |
| END ITEM IDENTIFICATION | C-17A AIRCRAFT |