Thank you for taking an interest in our selection of 5990-01-210-9788 parts here on Boost AOG. You are currently on the RFQ form for part number TTH11ES40, a Moog Inc product listed with the Synchro Control Transformer If part number TTH11ES40 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5990-01-210-9788 Item PartTypeName: SYNCHRO,CONTROL TRANSFORMER | 5990 | 012109788 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
TTH-11-ES-40/R2194 | 5 | 1 | C | 9 |
MRC | Criteria | Characteristic |
---|---|---|
AAFZ | BODY MATERIAL | STEEL,CORROSION RESISTING |
AAQL | BODY STYLE | STANDARD ROUND C |
AAVH | SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
AAVL | PILOT DIAMETER | 0.6250 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 1.9750 INCHES NOMINAL |
ABKK | FLANGE DIAMETER | 1.0620 INCHES NOMINAL |
ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
ABPA | UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
ABPC | UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
ABWV | SHAFT DIAMETER | 0.1200 INCHES NOMINAL SINGLE SHAFT |
ABXF | SHAFT LENGTH | 0.3750 INCHES NOMINAL SINGLE SHAFT |
AGAV | END ITEM IDENTIFICATION | AIRCRAFT,PROWLER EA-6B; AIRCRAFT,INTRUDER A-6E; AIRCRAFT,C-2A (REPROCURED); AIRCRAFT,HAWKEYE E-2C |
AJSL | BODY SIZE | 11 |
AJWQ | PILOT LENGTH | 0.0620 INCHES NOMINAL |
AJWR | SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES NOMINAL |
CQTM | TERMINAL LOCATION | REAR |
CQZS | SHAFT SLOT DEPTH | 0.0320 INCHES NOMINAL SINGLE SHAFT |
CRHN | SHAFT SLOT WIDTH | 0.0320 INCHES NOMINAL SINGLE SHAFT |
CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
TTQY | TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
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