At NSN Unlimited, we maintain a large database of parts HTC8A4L150, CTH8A4L150, CTH-8-A-4 L150, CM010029C8, 8CT-300-B-1B 15 with NSN 5990-00-067-6791 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Ge Aviation Systems Llc, Moog Inc, Dimo Corp, Api Harowe Inc, Kearfott Corporation. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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| Alternative NSN: 5990-00-067-6791 |
| Item Name: Synchro Control Tra |
| FSG: 59 Electrical and Electronic Equipment Components |
| Federal Supply Class (FSC): 5990 Synchros and Resolvers |
| NIIN: 000676791 |
| NCB Code: USA (00) |
| Manufacturers: Ge Aviation Systems Llc , Moog Inc , Dimo Corp , Api Harowe Inc , Kearfott Corporation , Ametek Technical And Industrial |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| HTC8A4L150 | 5990-00-067-6791 | synchro control tra | ge aviation systems llc | Avl | RFQ |
| HTC8A4L150 | 5990-00-067-6791 | synchro control tra | moog inc | Avl | RFQ |
| HTC8A4L150 | 5990-00-067-6791 | synchro control tra | dimo corp | Avl | RFQ |
| HTC8A4L150 | 5990-00-067-6791 | synchro control tra | api harowe inc | Avl | RFQ |
| CTH8A4L150 | 5990-00-067-6791 | synchro control tra | api harowe inc | Avl | RFQ |
| CTH8A4L150 | 5990-00-067-6791 | synchro control tra | moog inc | Avl | RFQ |
| CTH8A4L150 | 5990-00-067-6791 | synchro control tra | ge aviation systems llc | Avl | RFQ |
| CTH-8-A-4 L150 | 5990-00-067-6791 | synchro control tra | dimo corp | Avl | RFQ |
| CM010029C8 | 5990-00-067-6791 | synchro control tra | api harowe inc | Avl | RFQ |
| CM010029C8 | 5990-00-067-6791 | synchro control tra | dimo corp | Avl | RFQ |
| CM010029C8 | 5990-00-067-6791 | synchro control tra | kearfott corporation | Avl | RFQ |
| CM010029C8 | 5990-00-067-6791 | synchro control tra | ge aviation systems llc | Avl | RFQ |
| 8CT-300-B-1B 15 | 5990-00-067-6791 | synchro control tra | dimo corp | Avl | RFQ |
| 8CT-300-B-1B 15 | 5990-00-067-6791 | synchro control tra | ge aviation systems llc | Avl | RFQ |
| 8CT 300 B 1B 15 | 5990-00-067-6791 | synchro control tra | api harowe inc | Avl | RFQ |
| 137030-01 | 5990-00-067-6791 | synchro control tra | ge aviation systems llc | Avl | RFQ |
| 137030-01 | 5990-00-067-6791 | synchro control tra | dimo corp | Avl | RFQ |
| 137030-01 | 5990-00-067-6791 | synchro control tra | api harowe inc | Avl | RFQ |
| 08CT1402-1 | 5990-00-067-6791 | synchro control tra | ametek technical and industrial | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL, CORROSION RESISTING |
| AAQL | BODY STYLE | STANDARD ROUND A |
| AAVL | PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 1.6310 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| ABPA | UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| ABWV | SHAFT DIAMETER | 0.0900 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.3320 INCHES NOMINAL SINGLE SHAFT |
| AFJN | III FRAGILITY FACTOR | MODERATELY RUGGED |
| AHCG | MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| AJSL | BODY SIZE | 8 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| AJSP | STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES MAXIMUM |
| AJSQ | STATOR INPUT ELECTRICAL POWER RATING | 0.1 WATTS MAXIMUM |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 470.00 NOMINAL |
| AJSY | ZSO RESISTANCE IN OHMS | 81.00 NOMINAL |
| AJTA | ZRS RESISTANCE IN OHMS | 590.00 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT MINIMUM AND 12.000 INPUT TO OUTPUT MAXIMUM |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -16.0/+30.0 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| AJWE | III SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| AJWG | SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| AJWH | III SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| AJWQ | PILOT LENGTH | 0.0430 INCHES NOMINAL |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 1770.00 NOMINAL |
| CRGZ | PLUS J ZSO REACTANCE IN OHMS | 330.00 NOMINAL |
| CRKL | PLUS J ZRS REACTANCE IN OHMS | 190.00 NOMINAL |
| CRSJ | SHAFT TYPE | ROUND SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 2.1465 ROTOR TO STATOR MINIMUM AND 2.2165 ROTOR TO STATOR MAXIMUM |
| CWXK | SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| CWYF | III SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
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