Thank you for taking interest in Northrop Grumman Systems Corporation part number 900141-69, which is listed with the NSN 5990-00-813-5085 and a product description of “Synchro Transmitter.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5990-00-813-5085 Item PartTypeName: SYNCHRO,TRANSMITTER | 5990 | 008135085 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
900141-69 | C | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
ABHP | OVERALL LENGTH | 2.2910 INCHES MAXIMUM |
ABKK | FLANGE DIAMETER | 1.0670 INCHES MAXIMUM |
ABKU | FLANGE THICKNESS | 0.0880 INCHES MINIMUM AND 0.0980 INCHES MAXIMUM |
ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
AJST | ROTOR INPUT CURRENT RATING | 280.0 MILLIAMPERES MAXIMUM |
AJTG | ZRO IMPEDANCE MAGNITUDE IN OHMS | 18.10 NOMINAL |
AJTH | ZRO IMPEDANCE ANGLE IN DEG | 79.50 NOMINAL |
AJTS | ROTOR DC RESISTANCE IN OHMS | 9.00 NOMINAL |
AJTT | STATOR DC RESISTANCE IN OHMS | 3.00 NOMINAL |
AJVF | PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT MAXIMUM |
AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 26.00 |
AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -5.0 TO 5.0 |
AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 16.0 CENTIMETER-GRAMS MAXIMUM |
AJVW | ALIGNMENT HOLE QUANTITY | 4 |
AJWG | SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
AJWQ | PILOT LENGTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7820 INCHES MAXIMUM |
CQRG | BODY MATERIAL | STEEL CORROSION RESISTING |
CQZS | SHAFT SLOT DEPTH | 0.0250 INCHES MINIMUM AND 0.0370 INCHES MAXIMUM SINGLE SHAFT |
CRHN | SHAFT SLOT WIDTH | 0.0200 INCHES MINIMUM AND 0.0370 INCHES MAXIMUM SINGLE SHAFT |
CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
CWYF | SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
TTQY | TERMINAL TYPE AND QUANTITY | 5 SCREW |
AAQL | BODY STYLE | STANDARD ROUND B |
AAVH | SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
ABPC | UNDERCUT WIDTH | 0.0450 INCHES MINIMUM AND 0.0550 INCHES MAXIMUM |
ABXF | SHAFT LENGTH | 0.4380 INCHES MINIMUM AND 0.4420 INCHES MAXIMUM SINGLE SHAFT |
AJSL | BODY SIZE | 11 |
AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 1.11 WATTS NOMINAL |
AJTJ | ZSO IMPEDANCE MAGNITUDE IN OHMS | 107.00 NOMINAL |
AJTK | ZSO IMPEDANCE ANGLE IN DEG | 81.70 NOMINAL |
AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
AJWH | SHAFT END PLAY | 0.0005 INCHES MINIMUM AND 0.0030 INCHES MAXIMUM |
AJWR | SHOULDER LENGTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
AJXB | SHAFT MAXIMUM RUNOUT | 0.0008 INCHES |
CQTM | TERMINAL LOCATION | REAR |
CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
CRSY | ALIGNMENT HOLE DEPTH | 0.1200 INCHES MINIMUM AND 0.1300 INCHES MAXIMUM |
CSJY | TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
CWXK | SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
TEST | TEST DATA DOCUMENT | 06481-900141-69 DRAWING (THIS IS THE BASIC GOVERNING DRAWING,SUCH AS A CONTRACTOR DRAWING,ORIGINAL EQUIPMENT MANUFACTURER DRAWING,ETC.; EXCLUDES ANY SPECIFICATION,STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DR |
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