You are currently exploring our in-stock options for part number 1849B0404 with the NSN 5990005573669. This product is listed with the description “Synchro Control Transformer” and is manufactured by Kollsman Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 1849B0404 is listed alongside the NSN 5990-00-557-3669 and belongs to the FSC 5990 Synchros and Resolvers. Additionally, it is also under the CAGE Code 89944, which is assigned to Kollsman Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 1849B0404 seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5990-00-557-3669 Item PartTypeName: SYNCHRO,CONTROL TRANSFORMER | 5990 | 005573669 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1849B0404 | C | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAFZ | BODY MATERIAL | STEEL,STAINLESS |
AAQL | BODY STYLE | STANDARD ROUND B |
AAVH | SHOULDER DIAMETER | 0.1195 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM |
AAVL | PILOT DIAMETER | 0.5000 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 1.5150 INCHES NOMINAL |
ABKK | FLANGE DIAMETER | 1.3100 INCHES MINIMUM AND 1.3140 INCHES MAXIMUM |
ABKU | FLANGE THICKNESS | 0.0620 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
ABPC | UNDERCUT WIDTH | 0.0750 INCHES MINIMUM AND 0.0780 INCHES MAXIMUM |
ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
ABXF | SHAFT LENGTH | 0.5000 INCHES NOMINAL SINGLE SHAFT |
AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
AJSL | BODY SIZE | 14 |
AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 9.0 NOMINAL |
AJSP | STATOR INPUT CURRENT RATING | 175.0 MILLIAMPERES NOMINAL |
AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 100.0 MILLIWATTS NOMINAL |
AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
AJSW | ZRO RESISTANCE IN OHMS | 6150.00 NOMINAL |
AJSY | ZSO RESISTANCE IN OHMS | 30.00 NOMINAL |
AJTA | ZRS RESISTANCE IN OHMS | 130.00 NOMINAL |
AJTS | ROTOR DC RESISTANCE IN OHMS | 670.00 NOMINAL |
AJTT | STATOR DC RESISTANCE IN OHMS | 41.00 NOMINAL |
AJVF | PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 INPUT |
AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 70.00 |
AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -45.0 TO 45.0 |
AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
AJWQ | PILOT LENGTH | 1.2177 INCHES NOMINAL |
AJWR | SHOULDER LENGTH | 0.0930 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1080 INCHES MINIMUM AND 1.1110 INCHES MAXIMUM |
CQTM | TERMINAL LOCATION | REAR |
CQXQ | PLUS J ZRO REACTANCE IN OHMS | 615.00 NOMINAL |
CRGZ | PLUS J ZSO REACTANCE IN OHMS | 155.00 NOMINAL |
CRKL | PLUS J ZRS REACTANCE IN OHMS | 50.00 NOMINAL |
CRSJ | SHAFT TYPE | ROUND SINGLE SHAFT |
CSJY | TRANSFORMATION RATIO | 0.862 ROTOR TO STATOR NOMINAL |
TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
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