Part Details | EXTERNALLY THREADED RING
5365-00-897-8925 A cylindrically shaped item with a concentric bore and a peripheral thread over its entire length or over a portion thereof. One face is drilled, slotted, knurled, or has projecting lugs for installation and/or removal purposes. Excludes RETAINER, OPTICAL ELEMENT.
Alternate Parts: 114D20721, 114D2072-1, 114D20721, 114D2072-1, 5365-00-897-8925, 00-897-8925, 5365008978925, 008978925
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1962 | 00-897-8925 | 08417 ( RING, EXTERNALLY THREADED ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5365-00-897-8925
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114D2072-1 | 81205 | THE BOEING COMPANYDBA BOEING |
| 114D2072-1 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5365-00-897-8925
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 4130 |
| OVERALL LENGTH | 0.500 INCHES NOMINAL |
| CASEHARDENING INDICATOR | NOT CASEHARDENED |
| DRIVE TYPE | SLOTTED FACE |
| ACCOMMODATION TYPE AND QUANTITY | 4 SLOTS |
| WIDTH | 0.500 INCHES NOMINAL |
| DEPTH | 0.120 INCHES NOMINAL |
| ANGLE BETWEEN ACCOMMODATIONS IN DEG | 90.0 |
| RADIUS FROM GEOMETRIC AXIS TO ACCOMMODATION | 2.595 INCHES NOMINAL |
| THREAD SIZE | 5.8125 |
| SCREW THREAD SERIES DESIGNATOR | Q ANY ACCEPTABLE |
| THREAD CLASS | 3A |
| THREAD DIRECTION | RIGHT-HAND |
| BEVELED THREAD | INCLUDED |
| THREAD LOCATION | END OPPOSITE DRIVE END |
| BORE SHAPE | STRAIGHT |
| BORE DIAMETER | 5.070 INCHES NOMINAL |
| BORE ANNULAR INTERNAL SERRATION | NOT INCLUDED |
| BORE EDGE PROCESS | CHAMFERED |
| PROCESS END LOCATION | END OPPOSITE DRIVE END |
| CHAMFER ANGLE IN DEG | 45.0 |
| CHAMFER LENGTH | 0.040 INCHES NOMINAL |
| SETSCREW LOCKING NOTCH | NOT INCLUDED |
| FSC APPLICATION DATA | DRIVE MECHANISMS,HELICOPTER |