Synchros and Resolvers: 1951145-1, 195581-1, 1983005
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1951145-1 19511451 | 5990-01-129-7701 | Stator, Synchro | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) | ||
| 195581 | 5990-00-440-0335 | Synchro | Raytheon Company (37695) | ||
| 195581-1 1955811 | 5990-00-440-0335 | Synchro | Raytheon Company (37695) | ||
| 1957581-1 19575811 | 5990-01-045-2129 | Synchro, Transmitter | Frequency in Hertz: 400.0 nominal Body Size: 10 Overall Length: 1.6000 inches nominal | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 1957638-1 19576381 | 5990-00-424-8872 | Synchro, Transmitter | Terminal Type and Quantity: 6 wire lead Frequency in Hertz: 400.0 nominal Body Size: 8 | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 1957639-1 19576391 | 5990-01-283-7062 | Transolver, Electrical | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) | ||
| 195926 | 5990-01-138-7984 | Synchro, Transmitter | Terminal Type and Quantity: 5 wire lead Frequency in Hertz: 60.0 nominal Body Size: 23 | Scientific Atlanta Inc. (10110) | |
| 196462-1 1964621 | 5990-01-249-2058 | Retainer, Synchro | ITT Corporation (24930) | ||
| 196463-1 1964631 | 5990-01-249-2059 | Retainer, Synchro | ITT Corporation (24930) | ||
| 196466-1 1964661 | 5990-01-249-2060 | Retainer, Synchro | ITT Corporation (24930) | ||
| 1967520-1 19675201 | 5990-00-482-2536 | Motor, Torque | Special Features: Frameless dc permanent magnet type per MIL-E-5272, rotor and stator assy in accordance W/spec requirements sheets 1 thru 7 technical data drwg 1967520-19315, 1.125 in. max od, 0.567 in. max lg, 0.1905 in. max dia bore, four mtg holes | Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | |
| 1976194-2 19761942 | 5990-01-042-7963 | Synchro, Torque Reci | General Characteristics Item Description: Electrical- design requiremens asfollows-input power 0.8 watts maximum, input current 0.19 amps maximum, impedance zso at 90 degrees 15 ohms maximum, brush contact 2.0 ohms maximum, torque gradient(mg-mm/deg) 2800 minimum, nullvoltages-total (mv.) 50 maximum, phase shift 8.0 degrees maximum, transformation ratio 0.454 plus or minus 3 percentsynchronization 4 seconds maximum. themechanical design requirements are in thousandths of an inch tolerance with normal excitation voltage being 26V AT400 hertz.qualification tests shall berun on six units for vibration and forshock with half being tested for radionoise, humidity, high-low temperature | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) | |
| 1977232-1 19772321 | 5990-01-338-2102 | Synchro, Transmitter | Northrop Grumman Systems Corporation (03956) | ||
| 1977616 ITEM 27 1977616ITEM27 | 5990-01-315-3754 | Synchro, Transmitter | Northrop Grumman Systems Corporation (03956) | ||
| 1978347 | 5990-01-334-8634 | Synchro, Receiver | Northrop Grumman Systems Corporation (03956) | ||
| 1978867-1 19788671 | 5990-01-314-0228 | Synchro, Transmitter | III End Item Identification: Depth sounding equipment, doppler speed log | Northrop Grumman Systems Corporation (03956) | |
| 1979009 | 5990-01-411-5930 | Synchro, Transmitter | III End Item Identification: Video processor | Northrop Grumman Systems Corporation (03956) | |
| 1981154-1 19811541 | 5990-00-566-5987 | Synchro, Differential Receiver | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) Honeywell Intl Inc. Defense Avionics (19315) | ||
| 1981154-3 19811543 | 5990-01-105-4952 | Synchro, Differential Receiver | Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) | ||
| 1983005 | 5990-01-490-4341 | Synchro Assembly | Northrop Grumman Systems Corporation (03956) |