Part Details | ENGINE POPPET VALVE
2805-00-088-3337 A mushroom or tulip-shaped item having a circular head with a conical face and an extended stem used to regulate the flow of incoming fuel-air mixture or air into the combustion chamber or exhaust gases from the combustion chamber of a reciprocating internal combustion engine.
Alternate Parts: 110881, 110-881, 1100881, 110-0881, 101B881, 101881, 101-881, 1010881, 101-0881, 110B912, 110B881, 110912, 110-912, V2276N, V-2276N, 1998, 110B881, 2805-00-088-3337, 00-088-3337, 2805000883337, 000883337
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JAN 01, 1963 | 00-088-3337 | 15884 ( VALVE, POPPET, ENGINE ) |
REFERENCE DRAWINGS & PICTURES
FLAT
GROOVED
Cross Reference | NSN 2805-00-088-3337
Part Number | Cage Code | Manufacturer |
---|---|---|
110-881 | 44940 | CUMMINS POWER GENERATION INC. |
110-0881 | 44940 | CUMMINS POWER GENERATION INC. |
101B881 | 44940 | CUMMINS POWER GENERATION INC. |
101-881 | 44940 | CUMMINS POWER GENERATION INC. |
101-0881 | 44940 | CUMMINS POWER GENERATION INC. |
110B912 | 44940 | CUMMINS POWER GENERATION INC. |
110B881 | 44940 | CUMMINS POWER GENERATION INC. |
110-912 | 44940 | CUMMINS POWER GENERATION INC. |
V-2276N | 76255 | MCQUAY-NORRIS INCOEM DIV |
1998 | 54509 | NAPASCO INTERNATIONAL INC |
110B881 | 96787 | STEWART AVIONICS INC |
Technical Data | NSN 2805-00-088-3337
Characteristic | Specifications |
---|---|
MATERIAL AND LOCATION | STEEL, FED STD 66, AISI/SAE 4140 OVERALL |
HEAD STYLE | FLAT |
HEAD HEIGHT | 0.1325 INCHES MINIMUM AND 0.1475 INCHES MAXIMUM |
OUTSIDE DIAMETER | 1.3740 INCHES MINIMUM AND 1.3840 INCHES MAXIMUM |
NECK RADIUS | 0.3125 INCHES NOMINAL |
SEAT ANGLE IN DEG | 44.0 |
STEM STYLE | GROOVED |
GROOVE DIAMETER | 0.2980 INCHES MINIMUM AND 0.3040 INCHES MAXIMUM |
CHAMFER LENGTH | 0.0312 INCHES NOMINAL |
GROOVE WIDTH | 0.0950 INCHES MINIMUM AND 0.1050 INCHES MAXIMUM |
STEM LENGTH | 5.3980 INCHES MINIMUM AND 5.4080 INCHES MAXIMUM |
STEM DIAMETER | 0.3425 INCHES MINIMUM AND 0.3430 INCHES MAXIMUM |
DISTANCE FROM GROOVE TO STEM END | 0.5350 INCHES MINIMUM AND 0.5750 INCHES MAXIMUM |
CHAMFER ANGLE IN DEG | 45.0 |
CARBON RELIEF GROOVE | NOT INCLUDED |
SPECIAL FEATURES | GRUMMAN AEROSPAE A-10 AIRCRAFT |
FSC APPLICATION DATA | GASOLINE ENGINE |