Part Details | EXTERNALLY THREADED RING
5365-00-526-2485 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: 9603511, 9-60351-1, 960351, 9-60351, 9603511, 9-60351-1, 5365-00-526-2485, 00-526-2485, 5365005262485, 005262485
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-526-2485 | 08417 ( RING, EXTERNALLY THREADED ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5365-00-526-2485
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9-60351-1 | 17765 | BOEING COMPANY, THEDBA BOEING |
| 9-60351 | 81205 | THE BOEING COMPANYDBA BOEING |
| 9-60351-1 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 5365-00-526-2485
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| SURFACE TREATMENT | CADMIUM |
| OVERALL LENGTH | 0.400 INCHES NOMINAL |
| MATERIAL HARDNESS RATING | 34.0 ROCKWELL C MINIMUM AND 38.0 ROCKWELL C MAXIMUM |
| CASEHARDENING INDICATOR | NOT CASEHARDENED |
| DRIVE TYPE | DRILLED FACE |
| ACCOMMODATION TYPE AND QUANTITY | 6 HOLES |
| DIAMETER | 0.1875 INCHES NOMINAL |
| DEPTH | 0.120 INCHES NOMINAL |
| ANGLE BETWEEN ACCOMMODATIONS IN DEG | 60.0 |
| RADIUS FROM GEOMETRIC AXIS TO ACCOMMODATION | 1.875 INCHES NOMINAL |
| THREAD SIZE | 4.250-32 |
| SCREW THREAD SERIES DESIGNATOR | UNS |
| THREAD CLASS | 2A |
| BEVELED THREAD | INCLUDED |
| THREAD LOCATION | BOTH ENDS |
| BORE SHAPE | STRAIGHT |
| BORE DIAMETER | 3.260 INCHES NOMINAL |
| BORE ANNULAR INTERNAL SERRATION | NOT INCLUDED |
| BORE EDGE PROCESS | CHAMFERED |
| PROCESS END LOCATION | BOTH ENDS |
| CHAMFER ANGLE IN DEG | 45.0 |
| CHAMFER LENGTH | 0.060 INCHES NOMINAL |
| SETSCREW LOCKING NOTCH | NOT INCLUDED |
| FSC APPLICATION DATA | STABILIZER,AIRCRAFT |