Part Number : HTC-8-ST-1
Alternate P/N : HTC8ST1
NSN : 5990-00-160-1072 (5990001601072)
Item Name : Synchro Control Transformer
Manufacturer : Moog Inc
CAGE Code : 99932
NIIN : 001601072
ASAP Aviation Unlimited offers an unmatched one-stop-shop procurement solution to our clients within the aerospace and defense industries. We are an ASAP Semiconductor company with more than 10 million National Stock Numbers (NSN) in our inventory. ASAP Semiconductor is an AS9120B, ISO 9001:2015, and FAA AC 0056B accreditation, and the only distributor with a NO CHINA SOURCING pledge. We believe that high quality verifiable parts at competitive prices should be an industry norm, not the outlier. At ASAP, we are committed to providing an optimized purchasing experience - that’s why we’ve established a supply-chain network of over 20 locations in the US and abroad with a 95% on time delivery record.
The National Stock Number or NATO Stock Number (NSN) identifies that an item is procured, stocked, and issued through the federal supply system. Part Number HTC-8-ST-1 falls under NSN 5990001601072 and FSC is 5990 Synchros and Resolvers. The NSN is recognized by the United States Department of Defense and the North Atlantic Treaty Organization (NATO). The NSNs are administered by the Defense Logistics Agency (DLA).
Would you like more information on NSN 5990001601072 or part number HTC-8-ST-1? Please call us on our toll-free number +1-714-705-4780 or email us at sales@asapaviationunlimited.com. If you’re ready to submit a Bill of Materials (BOM), simply attach the excel format file to your email and a dedicated representative will contact you shortly.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-160-1072 Item Description: Synchro Control Transformer | 5990 | 001601072 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Htc-8-St-1 | C | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAQL | BODY STYLE | STANDARD ROUND A |
| AAVL | PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| ABXF | SHAFT LENGTH | 0.4570 INCHES NOMINAL SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSP | STATOR INPUT CURRENT RATING | 87.0 MILLIAMPERES NOMINAL |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 210.0 MILLIWATTS NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 210.00 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 143.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS MAXIMUM |
| AJWQ | PILOT LENGTH | 0.0380 INCHES MINIMUM AND 0.0480 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CRGZ | PLUS J ZSO REACTANCE IN OHMS | 114.00 NOMINAL |
| CRSJ | SHAFT TYPE | ROUND SINGLE SHAFT |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| AAFZ | BODY MATERIAL | STEEL, CORROSION RESISTING |
| ABHP | OVERALL LENGTH | 1.7460 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| ABPA | UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.0895 INCHES MINIMUM SINGLE SHAFT AND 0.0900 INCHES MAXIMUM SINGLE SHAFT |
| AJSL | BODY SIZE | 8 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSY | ZSO RESISTANCE IN OHMS | 28.00 NOMINAL |
| AJTA | ZRS RESISTANCE IN OHMS | 250.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 9.000 INPUT TO OUTPUT NOMINAL |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 690.00 NOMINAL |
| CRKL | PLUS J ZRS REACTANCE IN OHMS | 73.00 NOMINAL |
| CSJY | TRANSFORMATION RATIO | 2.303 ROTOR TO STATOR NOMINAL |
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