145HS287-2: TRANSDUCER,DUAL.
The TRANSDUCER,DUAL is a the manufacturer industrial component. Key specifications include special_features: CRITICAL APPLICATION ITEM, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: TRANSDUCER ASSEMBLY, DUAL, LINEAR, ILCA. This part is cataloged in the U.S.
Government catalog under NSN 1650-01-119-7368, 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.
| special_features | CRITICAL APPLICATION ITEM |
| special_test_features | MISSION RELIABILITY: EACH TRANSDUCER SHALL HAVE NO LESS THAN .99999 PROBABILITY OF COMPLETING A 1 HOUR MISSION WITHOUT INCURRING A MISSION FAILURE |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | TRANSDUCER ASSEMBLY, DUAL, LINEAR, ILCA |
| NSN | 1650-01-119-7368 |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | THE TRANSDUCER ASSEMBLY SHALL BE CAPABLE OF CONTINUOUS OPERATION THROUGHOUT THE AMBIENT TEMPERATURE RANGE OF - 50 DEGREES FAHRENHEIT TO +275 DEGREES FAHRENHEIT; UNIT SHALL BE CAPABLE OF OPERATION FROM SEA LEVEL TO 50,000 FEET ALTITUDE COMBINED WITH TEMPERATURES FROM -50F TO +160F FT |
| SPECIAL TEST FEATURES | MISSION RELIABILITY: EACH TRANSDUCER SHALL HAVE NO LESS THAN .99999 PROBABILITY OF COMPLETING A 1 HOUR MISSION WITHOUT INCURRING A MISSION FAILURE |
| SUPPLEMENTARY FEATURES | CLEANING OF SAND AND DUST: AIRBORNE SAND AND DUST PARTICLES ENCOUNTERED IN DESERT OPERATIONS, PER METHOD 510, PROCEDURE I, OF MIL-STD-810B; SALT SPRAY: ATMOSPHERE CONTAINING SALT LADEN MOISTURE, PER METHOD 509, PROCEDURE I OF MIL-STD-810B |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | CRITICAL APPLICATION ITEM |
| FUNCTIONAL DESCRIPTION | MOISTURE: THE DESIGN CONFIGURATION SHALL BE SUCH THAT MOISTURE CANNOT COLLECT IN DEPRESSIONS OR IRREGULAR SURFACES TO THE EXTENT OF CAUSING MALFUNCTION FROM CORROSION, FREEZING OR OTHER INJURIOUS EFFECTS; VIBRATION AND SHOCK: TRANSDUCER ASSEMBLY SHALL BE DESIGNED TO AVOID THE EFFECTS DUE TO AIRCRAFT EXCITATION FREQUENCIES AS FOLLOWS: SPIRAL BEVEL MESH: 3241 TO 3441 HZ; LOWER PLANETARY 1ST HARMONIC: 1407 TO 1495 HZ; LOWER PLANET 2ND HARMONIC: 2814 TO 2990 HZ; LOWER PLANETARY 3RD HARMONIC: 4222 TO 4483 HZ; MAJOR AUXILIARY POWER UNIT FREQUENCIES: ROTOR SPEED: 1021 - 1123 HZ; OUTPUT SHAFT: 137 TO 140 HZ;SHOCK: THE VALVE ASSEMBLY SHALL BE DESIGNED TO WITHSTAND AND FUNCTION AFTER BEING SUBJECTED TO 12 IMPACTS OF 15 (FORCES OF NEWTONIAN GRAVITY) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TRANSDUCER ASSEMBLY, DUAL, LINEAR, ILCA |