Part Details | SLEEVE BUSHING
3120-01-213-7055 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: 9131M66P03, 9131M66P03, 9131M66P03, 9131M66P03, 9131M66P03, 3120-01-213-7055, 01-213-7055, 3120012137055, 012137055
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 31 | JUL 29, 1985 | 01-213-7055 | 13206 ( BUSHING, SLEEVE ) |
REFERENCE DRAWINGS & PICTURES
SOLID, EXTERNAL FLANGE ONE END
Cross Reference | NSN 3120-01-213-7055
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9131M66P03 | 58828 | CFM INTERNATIONAL, INC. |
| 9131M66P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9131M66P03 | 07128 | TRELLEBORG SEALING SOLUTIONS ELSEGUNDO, INC. |
| 9131M66P03 | 60402 | TRI-MACK PLASTICS MANUFACTURINGCORP. |
| 9131M66P03 | 28884 | TSS TECHNOLOGIES, INC.DBA TSS MEDICAL |
Technical Data | NSN 3120-01-213-7055
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | SOLID, EXTERNAL FLANGE ONE END |
| OVERALL LENGTH | 0.2770 INCHES MINIMUM AND 0.2990 INCHES MAXIMUM |
| BODY OUTSIDE DIAMETER | 0.6540 INCHES MINIMUM AND 0.6550 INCHES MAXIMUM |
| BODY INSIDE DIAMETER | 0.5760 INCHES MINIMUM AND 0.5770 INCHES MAXIMUM |
| FLANGE OUTSIDE DIAMETER | 0.8150 INCHES MINIMUM AND 0.8250 INCHES MAXIMUM |
| FLANGE WIDTH | 0.0570 INCHES MINIMUM AND 0.0590 INCHES MAXIMUM |
| SPECIAL FEATURES | FLIGHT SAFETY CRITICAL AIRCRAFT PART |
| CRITICALITY CODE JUSTIFICATION | FEAT |