Mfg Part Number: 23TR6B
NSN : 5990-00-926-4324
NIIN : 009264324
CAGE Code : 96169
Manufacturer: Electric Boat Corporation
Item Name : Synchro Receiver Tr
Here at Internet For Aviation, we have 23TR6B Synchro Receiver Tr from Electric Boat Corporation, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific 23TR6B to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5990-00-926-4324 Item Description: Synchro Receiver Tr | 5990 | 009264324 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
23TR6B | B | 1 | C | A |
2.012956 | 2277534-0001 | 23M4F1Q | 23TRX6 |
23TRX6A | 23TRX6B | 512291 | 59 000-016 |
5990PL0820496 | 5M7360-980-11 | AS20708 56 | AY2401F12C2 |
M20708 56-01B | SAE-AS20708 56 | TRX23-6N3 |
MRC | Criteria | Characteristic |
---|---|---|
AAFZ | BODY MATERIAL | STEEL, STAINLESS |
AAQL | BODY STYLE | STANDARD ROUND D |
AAZW | SECOND SHOULDER DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
AAZX | SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
ABKU | FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
ABWV | SHAFT DIAMETER | 0.2403 INCHES MINIMUM SINGLE SHAFT AND 0.2405 INCHES MAXIMUM SINGLE SHAFT |
AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
AHCG | MAXIMUM TEMP RISE | 35.0 DEG CELSIUS |
AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 5.6 WATTS MAXIMUM |
AJTN | ZSS IMPEDANCE MAGNITUDE IN OHMS | 110.00 MINIMUM AND 145.00 MAXIMUM |
AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 60.00 OUTPUT |
AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 160.00 |
AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | 8.0/+8.0 |
AJVM | SPLINE TOOTH QUANTITY | 22 SINGLE SHAFT |
AJVN | RECEIVER ERROR ANGULAR RANGE IN MINUTES | 45.0/+45.0 |
AJWQ | PILOT LENGTH | 0.0430 INCHES NOMINAL |
AJWR | SHOULDER LENGTH | 0.2500 INCHES NOMINAL |
AJXA | SPLINE TOOTH DIAMETRAL PITCH | 96 SINGLE SHAFT |
AJYY | SHAFT THREAD SERIES DESIGNATOR | UNF SINGLE SHAFT |
AKAN | SHAFT THREAD CLASS | 2A SINGLE SHAFT |
CQWQ | SHAFT THREAD LENGTH | 0.2900 INCHES NOMINAL SINGLE SHAFT |
CWBH | SHAFT NOMINAL THREAD SIZE | 0.250 INCHES SINGLE SHAFT |
TTQY | TERMINAL TYPE AND QUANTITY | 5 SCREW |
ZZZK | SPECIFICATION/STANDARD DATA | 81349-MIL-S-20708/56 GOVERNMENT SPECIFICATION |
AAVH | SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
AAVL | PILOT DIAMETER | 0.5950 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 4.2990 INCHES NOMINAL |
ABKK | FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
ABPM | BODY DIAMETER | 1.9900 INCHES MAXIMUM |
ABXF | SHAFT LENGTH | 0.7190 INCHES NOMINAL SINGLE SHAFT |
AJSL | BODY SIZE | 23 |
AJSS | FREQUENCY IN HERTZ | 60.0 NOMINAL |
AJST | ROTOR INPUT CURRENT RATING | 210.0 MILLIAMPERES MAXIMUM |
AJTP | ZSS IMPEDANCE ANGLE IN DEG | 10.00 MINIMUM AND 17.00 MAXIMUM |
AJVF | PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
AJVV | TORQUE GRADIENT PER ANGULAR DEG | 0.120 INCH-OUNCES MINIMUM |
AJWV | AFT OF FIRST FLANGE DIAMETER | 1.9400 INCHES MAXIMUM |
AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.5800 INCHES NOMINAL |
AKAF | SHAFT THREAD DIRECTION | RIGHT-HAND SINGLE SHAFT |
CQTM | TERMINAL LOCATION | REAR |
CRSJ | SHAFT TYPE | SPLINE W/THREADS SINGLE SHAFT |
CSJY | TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
TEST | TEST DATA DOCUMENT | 81349-MIL-S-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTI |
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