Part Details | SLEEVE BUSHING
3120-01-478-8323 A tubular shaped unthreaded item with or without a flange at one end designed to be inserted into a hole to reduce the inside diameter of the hole and to protect the surrounding body structure from damage resulting from stress, strain, and/or vibration. The overall length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body. Includes items which are divided into two or more segments which includes 180 degrees (3.141 radians) or less of the bearing periphery. For items made of rubber, see BUSHING, NONMETALLIC. See also BEARING, SLEEVE; BUSHING, TAPERED; SPACER, SLEEVE; INSULATOR, BUSHING; and BUSHING, ELECTRICAL CONDUCTOR. Excludes BUSHING, DRILL, JIG.
Alternate Parts: NAS777017, NAS77-7-017, NAS777017, NAS77-7-017, NAS777017, NAS77-7-017, NAS777017, NAS77-7-017, NAS777017, NAS77-7-017, 3120-01-478-8323, 01-478-8323, 3120014788323, 014788323
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 31 | SEP 28, 2000 | 01-478-8323 | 13206 ( BUSHING, SLEEVE ) |
REFERENCE DRAWINGS & PICTURES
SOLID, EXTERNAL FLANGE ONE END
Cross Reference | NSN 3120-01-478-8323
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| NAS77-7-017 | 70265 | ALL-POWER MANUFACTURING CO.INC. |
| NAS77-7-017 | 23294 | AVALON MACHINE PRODUCTS INC |
| NAS77-7-017 | 65910 | MAYDAY MANUFACTURING CO. |
| NAS77-7-017 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| NAS77-7-017 | 59563 | REID PRODUCTS INC.DBA REID PRODUCTS |
Technical Data | NSN 3120-01-478-8323
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | SOLID, EXTERNAL FLANGE ONE END |
| OVERALL LENGTH | 0.1650 INCHES MINIMUM AND 0.1750 INCHES MAXIMUM |
| BODY OUTSIDE DIAMETER | 0.5631 INCHES MINIMUM AND 0.5638 INCHES MAXIMUM |
| BODY INSIDE DIAMETER | 0.4375 INCHES MINIMUM AND 0.4390 INCHES MAXIMUM |
| FLANGE OUTSIDE DIAMETER | 0.6770 INCHES MINIMUM AND 0.6970 INCHES MAXIMUM |
| FLANGE WIDTH | 0.0770 INCHES MINIMUM AND 0.0820 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F/A-18E/F LEADING EDGE FLAP |