6615PL2198890: ACCELEROMETER,ELECTRICAL,LINEAR.
ACCELEROMETER,ELECTRICAL,LINEAR. Key specifications include OVERALL WIDTH: 3.500 INCHES NOMINAL IN, OVERALL HEIGHT: 4.000 INCHES NOMINAL IN, OVERALL LENGTH: 3.500 INCHES NOMINAL IN, GRAVITY UNIT RANGE: -1.0 TO 1.0, MOUNTING CONFIGURATION: 4 MOUNTING HOLES ON BASE, END ITEM IDENTIFICATION: C130H AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 6615-01-043-2763, 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.
| OVERALL WIDTH | 3.500 INCHES NOMINAL IN |
| OVERALL HEIGHT | 4.000 INCHES NOMINAL IN |
| OVERALL LENGTH | 3.500 INCHES NOMINAL IN |
| GRAVITY UNIT RANGE | -1.0 TO 1.0 |
| MOUNTING CONFIGURATION | 4 MOUNTING HOLES ON BASE |
| END ITEM IDENTIFICATION | C130H AIRCRAFT |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| NSN | 6615-01-043-2763 |
| OVERALL HEIGHT | 4.000 INCHES NOMINAL IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| OVERALL LENGTH | 3.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.500 INCHES NOMINAL IN |
| GRAVITY UNIT RANGE | -1.0 TO 1.0 |
| SPECIAL FEATURES | ELECTROSTATIC SENSITIVE DEVICE; INPUT POWER REQUIREMENTS 26VAC 400HZ SINGLE PHASE; MFG NAME SCCELERATION SENSOR; CASE MATERIAL ALUMINUM; UNIT PROVIDES ACCELERATION SIGNALS TO FLIGHT DIRECTOR AND AUTOPILOT SYSTEMS. IT SENSES A CHANGE IN NORMAL FLIGHT ACCELERATION AND GENERATES A PROPORTIONAL SIGNAL. ALSO PROVIDES A MONITOR SIGNAL WHICH INDICATES RELIABLE OPERATION OF THE UNIT. AIR FORCE TECH ORDER 5A22-2-6-3 VAC |
| MOUNTING CONFIGURATION | 4 MOUNTING HOLES ON BASE |
| END ITEM IDENTIFICATION | C130H AIRCRAFT |