The PUMP,FUEL,CAM ACTUATED is a the manufacturer industrial component. Key specifications include fuel_filter: NOT INCLUDED, mounting_type: NONSTANDARD, overall_width: 3.875 INCHES NOMINAL IN, priming_lever: NOT INCLUDED, stroke_length: 0.364 INCHES NOMINAL IN, drain_facility: NOT INCLUDED. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2910-00-629-2292, indicating validated use in U.S.
government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| fuel_filter | NOT INCLUDED |
| mounting_type | NONSTANDARD |
| overall_width | 3.875 INCHES NOMINAL IN |
| priming_lever | NOT INCLUDED |
| stroke_length | 0.364 INCHES NOMINAL IN |
| drain_facility | NOT INCLUDED |
| overall_height | 4.626 INCHES NOMINAL IN |
| overall_length | 4.438 INCHES NOMINAL IN |
| vacuum_booster | NOT INCLUDED |
| fording_feature | NOT INCLUDED |
| actuation_method | DIRECT CAM |
| special_features | GRUMMAN A10 AIRCRAFT |
| NSN | 2910-00-629-2292 |
| INLET CONNECTION TYPE/SIZE | FUEL 3/8 IN.-18 THD SIZE IN |
| MAXIMUM STATIC PRESSURE ABOVE OUTLET HEIGHT | 5-3/4 LB AT 16 IN. AT 1800 RPM LBS |
| ACTUATION METHOD | DIRECT CAM |
| OUTLET CONNECTION TYPE/SIZE | FUEL 3/8 IN.-18 THD SIZE IN |
| DISTANCE FROM PUMP MOUNTING FACE TO ACTUATOR CENTER | 2.062 IN. TO CENTER OF CAM ECCENTRICITY IN |
| VACUUM BOOSTER | NOT INCLUDED |
| STROKE LENGTH | 0.364 INCHES NOMINAL IN |
| FUEL FILTER | NOT INCLUDED |
| SPECIAL FEATURES | GRUMMAN A10 AIRCRAFT |
| PRIMING LEVER | NOT INCLUDED |