NSN 2530-00-618-4429
Part Details | MASTER HYDRAULIC BRAKE CYLINDER ASSEMBLY
2530-00-618-4429 A device consisting of a reservoir and/or CYLINDER, HYDRAULIC BRAKE, MASTER with other components necessary to displace fluid from a central source for actuating the slave or wheel cylinders of a hydraulic brake system.
Alternate Parts: M9221, 1026, MC9221, 174271, 174-271, 9221, E9221, F9221, FD9221, 5454383, 5450936, 5450396, 5254383, 90FD9221, 5454383, 5450936, 5450396, 5254383, FD9221, MC9221, 2530-00-618-4429, 00-618-4429, 2530006184429, 006184429
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 25 | JAN 01, 1963 | 00-618-4429 | 11007 ( CYLINDER ASSEMBLY, HYDRAULIC BRAKE, MASTER ) |
REFERENCE DRAWINGS & PICTURES
TWO HOLE
Cross Reference | NSN 2530-00-618-4429
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| M9221 | 71425 | AIRTEX PRODUCTSDIV OF UIS INC |
| 1026 | 06840 | BENDIX CORP THE |
| MC9221 | 76761 | C. E. NIEHOFF & CO. |
| 174-271 | 76462 | DELCO MORAINE DIV OF GENERALMOTORS CORP |
| 9221 | 19239 | ECHLIN INC |
| E9221 | 80724 | EIS BRAKE PARTSDIV OF STANDARD MOTOR PRODUCTS INC |
| F9221 | 63477 | FEDERAL MOGUL CORPSUB WAGNER BRAKE |
| FD9221 | 63477 | FEDERAL MOGUL CORPSUB WAGNER BRAKE |
| 5454383 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| 5450936 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| 5450396 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| 5254383 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| 90FD9221 | 16662 | LIFT PARTS MFG CO INCDIV OF ECHLIN MFG CO THE |
| 5454383 | 23862 | MILITARY VEHICLES OPNGENERAL MOTORS TRUCK AND BUS GROUP |
| 5450936 | 23862 | MILITARY VEHICLES OPNGENERAL MOTORS TRUCK AND BUS GROUP |
| 5450396 | 23862 | MILITARY VEHICLES OPNGENERAL MOTORS TRUCK AND BUS GROUP |
| 5254383 | 23862 | MILITARY VEHICLES OPNGENERAL MOTORS TRUCK AND BUS GROUP |
| FD9221 | 98296 | STANDARD MFG CO INC |
| MC9221 | 66614 | TRW INC REPLACEMENT PARTS DIV |
Technical Data | NSN 2530-00-618-4429
| Characteristic | Specifications |
|---|---|
| OVERALL WIDTH | 2.625 INCHES NOMINAL |
| OVERALL HEIGHT | 4.250 INCHES NOMINAL |
| EXTENDED LENGTH | 7.953 INCHES NOMINAL |
| COMPRESSED LENGTH | 6.516 INCHES NOMINAL |
| BODY MATERIAL | ANY ACCEPTABLE |
| FIRST PISTON ROD END STYLE | 7 |
| FIRST END EXTERNAL THREAD LENGTH | 1.938 INCHES |
| FIRST PISTON ROD END THREAD SERIES DESIGNATOR | NF |
| FIRST PISTON ROD END THREAD DIAMETER | 0.375 INCHES |
| FIRST PISTON ROD END THREAD QUANTITY PER INCH | 24 |
| FIRST PISTON ROD END THREAD CLASS | 2A |
| FIRST PISTON ROD END THREAD DIRECTION | AAL |
| STRAIGHT BORE INSIDE DIAMETER | 1.250 INCHES NOMINAL |
| MOUNTING TYPE AND LOCATION | BOSS CENTER SECTION |
| MOUNTING PROVISION | UNTHREADED MOUNTING HOLES |
| MOUNTING PROVISION ARRANGEMENT STYLE | TWO HOLE |
| CENTER TO CENTER DISTANCE BETWEEN MOUNTING PROVISIONS | 2.875 INCHES NOMINAL |
| MOUNTING FACILITY DIAMETER | 0.469 INCHES NOMINAL |
| PORT LOCATION AND QUANTITY | 1 CYLINDER HEAD END |
| PORT STYLE | 5 |
| PORT THREAD SERIES DESIGNATOR | NF |
| PORT THREAD DIAMETER | 0.500 INCHES |
| PORT THREAD QUANTITY PER INCH | 20 |
| PORT THREAD CLASS | 2B |
| RESERVOIR TYPE | INTEGRAL |
| ACTUATION METHOD | DIRECT |
| FEATURES PROVIDED | RUBBER BOOT |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | GRUMMAN A-10 AIRCRAFT |