NSN 2805-00-625-2444
Part Details | PISTON CONNECTING ROD
2805-00-625-2444 A device used for connecting a piston to a crankshaft or to a master connecting rod of an internal combustion engine, steam reciprocating engine, reciprocating air compressor, or the like. The rod may be connected directly to the piston, or it may transmit the motion through a crosshead.
Alternate Parts: 114C98STD, 114C98, 11498STD, 114-98STD, 11498, 114-98, 1140098, 114-0098, A8909, A8909, 2805-00-625-2444, 00-625-2444, 2805006252444, 006252444
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-625-2444 | 60266 ( CONNECTING ROD, PISTON ) |
REFERENCE DRAWINGS & PICTURES
I-SECTION TYPE
2 BOLT 45 DEGREES
SMALL ENGINE AND AUTOMOTIVE STANDARD
Cross Reference | NSN 2805-00-625-2444
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 114C98STD | 44940 | CUMMINS POWER GENERATION INC. |
| 114C98 | 44940 | CUMMINS POWER GENERATION INC. |
| 114-98STD | 44940 | CUMMINS POWER GENERATION INC. |
| 114-98 | 44940 | CUMMINS POWER GENERATION INC. |
| 114-0098 | 44940 | CUMMINS POWER GENERATION INC. |
| A8909 | 96789 | KING BRAND MUSIC PAPER INC |
| A8909 | 96787 | STEWART AVIONICS INC |
Technical Data | NSN 2805-00-625-2444
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM |
| FABRICATION METHOD | N ANY ACCEPTABLE |
| CENTER TO CENTER EFFECTIVE LENGTH | 5.062 INCHES NOMINAL |
| BODY WIDTH AT PISTON CONNECTING END | 1.031 INCHES NOMINAL |
| BODY WIDTH AT SHAFT CONNECTING END | 1.031 INCHES NOMINAL |
| BODY THICKNESS AT PISTON CONNECTING END | 0.906 INCHES NOMINAL |
| BODY THICKNESS AT SHAFT CONNECTING END | 0.969 INCHES NOMINAL |
| PISTON END CONNECTION STYLE | SMALL ENGINE AND AUTOMOTIVE STANDARD |
| END THICKNESS | 1.125 INCHES NOMINAL |
| EDGE RADIUS | 0.594 INCHES NOMINAL |
| END HOLE INSIDE DIAMETER | 0.750 INCHES NOMINAL |
| PISTON CONNECTING END BEARING | INCLUDED |
| BEARING REPLACEABILITY | NONREPLACEABLE |
| PISTON CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
| PISTON CONNECTING END LUBRICATION METHOD | SPLASH |
| SHAFT CONNECTING END STYLE | 2 BOLT 45 DEGREES |
| SHAFT CONNECTING END HOLE INSIDE DIAMETER | 1.625 INCHES NOMINAL |
| SHAFT CONNECTING END EDGE RADIUS | 1.125 INCHES NOMINAL |
| SHAFT CONNECTING END WIDTH | 2.875 INCHES NOMINAL |
| SHAFT CONNECTING END THICKNESS | 1.125 INCHES NOMINAL |
| SHAFT CONNECTING END BEARING | INCLUDED |
| SHAFT CONNECTING END BEARING REPLACEABILITY | NONREPLACEABLE |
| SHAFT CONNECTING END LUBRICATION DRILL FEATURE | NOT INCLUDED |
| SHAFT CONNECTING END LUBRICATION METHOD | SPLASH |
| CROSS-SECTIONAL SHAPE STYLE | I-SECTION TYPE |
| SPECIAL FEATURES | GRUMMAN AEROSPACE A-10 AIRCRAFT |