623B: DAMPENER,FLUID PRESSURE.
The DAMPENER,FLUID PRESSURE is a the manufacturer industrial component. Key specifications include overall_width: 19.000 INCHES NOMINAL IN, overall_height: 8.750 INCHES NOMINAL IN, special_features: 14.500 IN. DEEP; C/O 6 IDENTICAL MONITORING CHANNELS IN, functional_description: MONITORS & ANALYZES TURBOJET, TURBOPROP AND TURBOFAN ENGINE VIBRATION, end_item_identification: T-21 AIRCRAFT ENGINE TEST STAND, functional_classification: AA-8.13.
This part is cataloged in the U.S. Government catalog under NSN 6635-01-321-1668, 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 | 19.000 INCHES NOMINAL IN |
| overall_height | 8.750 INCHES NOMINAL IN |
| special_features | 14.500 IN. DEEP; C/O 6 IDENTICAL MONITORING CHANNELS IN |
| functional_description | MONITORS & ANALYZES TURBOJET, TURBOPROP AND TURBOFAN ENGINE VIBRATION |
| end_item_identification | T-21 AIRCRAFT ENGINE TEST STAND |
| functional_classification | AA-8.13 |
| NSN | 6635-01-321-1668 |
| OVERALL HEIGHT | 8.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 19.000 INCHES NOMINAL IN |
| FUNCTIONAL CLASSIFICATION | AA-8.13 |
| SPECIAL FEATURES | 14.500 IN. DEEP; C/O 6 IDENTICAL MONITORING CHANNELS IN |
| FUNCTIONAL DESCRIPTION | MONITORS & ANALYZES TURBOJET, TURBOPROP AND TURBOFAN ENGINE VIBRATION |
| END ITEM IDENTIFICATION | T-21 AIRCRAFT ENGINE TEST STAND |