ASAP Aviation Procurement is pleased to announce that part number 11GLT25RHX BB2 of NSN 5990-00-101-2524 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 11GLT25RHX BB2 is a Synchro Control Transformer manufactured by Moog Inc under CAGE Code 99932. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. 11GLT25RHX BB2 Moog Inc is in stock.
Are you interested in learning more about part number 11GLT25RHX BB2? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-101-2524 Item PartTypeName: SYNCHRO,CONTROL TRANSFORMER | 5990 | 001012524 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 11GLT25RHXB852 | 2 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL,STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND C |
| AAVH | SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 2.1660 INCHES MINIMUM AND 2.1860 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| ABPA | UNDERCUT DIAMETER | 0.9700 INCHES MINIMUM AND 0.9800 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| ABWV | SHAFT DIAMETER | 0.1870 INCHES MINIMUM SINGLE SHAFT AND 0.1873 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.5340 INCHES MINIMUM SINGLE SHAFT AND 0.5600 INCHES MAXIMUM SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSL | BODY SIZE | 11 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJTG | ZRO IMPEDANCE MAGNITUDE IN OHMS | 3160.00 MINIMUM AND 3740.00 MAXIMUM |
| AJTH | ZRO IMPEDANCE ANGLE IN DEG | 78.00 MINIMUM AND 84.00 MAXIMUM |
| AJTJ | ZSO IMPEDANCE MAGNITUDE IN OHMS | 594.00 MINIMUM AND 736.00 MAXIMUM |
| AJTK | ZSO IMPEDANCE ANGLE IN DEG | 79.00 MINIMUM AND 85.00 MAXIMUM |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 415.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 4.800 INPUT TO OUTPUT NOMINAL |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 25.00 OUTPUT |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 35.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -5.5 TO 5.5 |
| AJWQ | PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| AJWR | SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6910 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | SIDE |
| CQZS | SHAFT SLOT DEPTH | 0.0260 INCHES MINIMUM SINGLE SHAFT AND 0.0360 INCHES MAXIMUM SINGLE SHAFT |
| CRHN | SHAFT SLOT WIDTH | 0.0260 INCHES MINIMUM SINGLE SHAFT AND 0.0360 INCHES MAXIMUM SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 1.560 ROTOR TO STATOR NOMINAL |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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