NIIN Output Data
NIIN:
NSN:
Item Name:
SYNCHRO , TRANSMITTER
Definition:
A SYNCHRO CONSISTING OF A STATOR AND ROTOR INDUCTIVELY COUPLED. THE ELECTRICAL OUTPUT OF THE STATOR INTO A RECEIVER SYNCHRO, A CONTROL TRANSFORMER OR DIFFERENTIAL SYNCHRO IS DEPENDENT UPON THE POSITION OF ITS ROTOR. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| AY201S25T | 96774 | A | C | 1 | 5 | ZZ | 9X | |
| 103778-02 | 35351 | A | 5 | 2 | X | XX | ||
| S215CT20B2 | 96762 | H | 5 | 9 | X | XX | ||
| AY2015-25 | 19315 | A | 5 | 9 | 6 | TX | ||
| AY201S25T | 55972 | A | 5 | 9 | 3 | TX | ||
| CTH-15-DS-1/B112 | 99932 | A | 5 | 2 | 3 | TX | ||
| 405253-1 | 96214 | A | 3 | 2 | 1 | TX | ||
| 737097-2 | 56232 | A | 5 | 9 | 6 | TX |
CAGE Information
| Code | Company |
|---|---|
| 19315 | HONEYWELL INTL INC DEFENSE AVIONICS |
| 96774 | HONEYWELL INTERNATIONAL INC. DBA HON |
| 35351 | GE AVIATION SYSTEMS LLC |
| 96762 | ELECTRONIC RESEARCH ASSOCIATES INC T |
| 55972 | HONEYWELL INTL INC DEFENSE AVIONICS |
| 99932 | MOOG INC. DBA MOOG COMPONENTS GROUP |
| 96214 | RAYTHEON COMPANY |
| 56232 | LOCKHEED MARTIN CORPORATION DBA LOCK |
Federal Supply Class
Title
SYNCHROS AND RESOLVERS
Inclusions:
Exclusions:
EXCLUDES SYNCHRO SYSTEMS; SERVO MECHANISMS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 10.0 CENTIMETER-GRAMS MAXIMUM |
| AJSL | BODY SIZE | 15 |
| CQTM | TERMINAL LOCATION | REAR |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 40.00 NOMINAL |
| AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 400.0 MILLIWATTS NOMINAL |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| ABPA | UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| CQZS | SHAFT SLOT DEPTH | 0.0210 INCHES MINIMUM SINGLE SHAFT AND 0.0310 INCHES MAXIMUM SINGLE SHAFT |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
| AAQL | BODY STYLE | STANDARD ROUND C |
| ABHP | OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| CRSJ | SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
| AJWQ | PILOT LENGTH | 0.0400 INCHES NOMINAL |
| ABKK | FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| CRHN | SHAFT SLOT WIDTH | 0.0210 INCHES MINIMUM SINGLE SHAFT AND 0.0310 INCHES MAXIMUM SINGLE SHAFT |
| AJST | ROTOR INPUT CURRENT RATING | 65.0 MILLIAMPERES NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJWR | SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| AAVL | PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| CRSY | ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| AAVH | SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| AAFZ | BODY MATERIAL | STEEL, STAINLESS |
| ABPC | UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -10.0/+10.0 |
| AJSW | ZRO RESISTANCE IN OHMS | 70.00 NOMINAL |
| ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| ABXF | SHAFT LENGTH | 0.5400 INCHES NOMINAL SINGLE SHAFT |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 30.0 CENTIMETER-GRAMS MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 400.00 NOMINAL |
| AJVW | ALIGNMENT HOLE QUANTITY | 4 |
| AJVF | PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT NOMINAL |
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