1650-01-119-7368
Find complete technical information, availability, and procurement data for: 1650-01-119-7368
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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) functional description, feat criticality code justification, transducer assembly, dual, linear, ilca part name assigned by controlling agency, mission reliability: each transducer shall have no less than .99999 probability of completing a 1 hour mission without incurring a mission failure special test features, critical application item special features
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Criticality Code Justification
- feat
- Part Name Assigned By Controlling Agency
- transducer assembly, dual, linear, ilca
- 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)
- 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
- 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
Related Parts
This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:
| Part Number | Name |
|---|---|
| 145HS287 | Dual Transducer |
| 145HS287-2 | Dual Transducer |
| 220K140-2 | Dual Transducer |
| Q2403 | Dual Transducer |
| SM220K140-2 | Dual Transducer |
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