Thank you for taking interest in Lockheed Martin Corporation part number CDN10AS1, which is listed with the NSN 5990-00-904-7315 and a product description of “Synchro Differential 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.
Note : We Will Not Share Your Information To Any Third Parties.
Alongside part number CDN10AS1, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Synchro Differential Transmitter part with the NSN 5990-00-904-7315. For example, you can browse other Lockheed Martin Corporation components that were produced under CAGE Code 56232 or listings that belong to FSC 5990 Synchros and Resolvers with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number CDN10AS1 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-904-7315 Item PartTypeName: SYNCHRO,DIFFERENTIAL TRANSMITTER | 5990 | 009047315 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | U | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CDN10AS1 | 3 | 1 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAQL | BODY STYLE | STANDARD ROUND B |
| AAVH | SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.5000 INCHES MINIMUM AND 0.5005 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 1.6650 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0580 INCHES MINIMUM AND 0.0680 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.0895 INCHES MINIMUM AND 0.0900 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.3370 INCHES NOMINAL SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSL | BODY SIZE | 10 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| AJSP | STATOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 28.90 MINIMUM AND 39.10 MAXIMUM |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 28.80 MINIMUM AND 35.20 MAXIMUM |
| AJTT | STATOR DC RESISTANCE IN OHMS | 22.50 MINIMUM AND 27.50 MAXIMUM |
| AJVF | PHASE SHIFT ANGLE IN DEG | 10.200 OUTPUT TO INPUT MAXIMUM |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 60.00 OUTPUT |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS MAXIMUM |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS MAXIMUM |
| AJWQ | PILOT LENGTH | 0.0350 INCHES MINIMUM AND 0.0450 INCHES MAXIMUM |
| AJWR | SHOULDER LENGTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1900 INCHES MAXIMUM |
| AJXB | SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| CQRG | BODY MATERIAL | STEEL CORROSION RESISTING |
| CQTM | TERMINAL LOCATION | REAR |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 107.10 MINIMUM AND 130.90 MAXIMUM |
| CQZS | SHAFT SLOT DEPTH | 0.1880 INCHES NOMINAL SINGLE SHAFT |
| CRHN | SHAFT SLOT WIDTH | 0.1250 INCHES NOMINAL SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 1.028 ROTOR TO STATOR MINIMUM AND 1.090 ROTOR TO STATOR MAXIMUM |
| TEST | TEST DATA DOCUMENT | 10001-2325877 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 DRAW |
| TTQY | TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
