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 |
|---|---|---|---|---|---|---|---|---|
| AY201S3B | 55972 | A | 5 | 9 | 5 | TX | ||
| 3563150-0310 | 96774 | A | C | 1 | 5 | ZZ | 9X | |
| AY20153B | 96774 | A | 5 | 2 | 5 | ZZ | ||
| 103778-01 | 35351 | A | 5 | 2 | 5 | TX | ||
| AY201S3B | 96774 | A | 3 | 2 | 5 | ZZ | ||
| 20084 | 96214 | A | 5 | 2 | 5 | TX | ||
| 3563150-0310 | 55972 | A | 5 | 9 | E | TX | ||
| M01092-2 | 80249 | A | 5 | 9 | 5 | TX | ||
| AY101D | 55972 | A | 5 | 9 | 5 | TX | ||
| 785671-5 | 96774 | A | C | 1 | 5 | ZZ | 9X | |
| CP35-9-11-1L | 25500 | A | 5 | 2 | 5 | TX | ||
| 20084-1 | 55972 | A | 5 | 9 | 5 | TX | ||
| 20084-1 | 96774 | A | 5 | 2 | 5 | ZZ | ||
| 7406457P2 | 03508 | F | 5 | 9 | 5 | TX | ||
| 7475539P1 | 03508 | F | 5 | 9 | 5 | TX | ||
| 476596-6 | 20418 | C | 5 | 9 | 5 | TX | ||
| 2G4005-8 | 99932 | A | 5 | 2 | 5 | TX | ||
| 8485160 | 18876 | A | 5 | 2 | 1 | TX | ||
| 704-52 | 01365 | A | 5 | 2 | 5 | TX | ||
| AY20153B | 55972 | A | 5 | 9 | 5 | KE | ||
| 46285 | 96214 | A | 5 | 2 | 5 | TX | ||
| 451-1268 | 11530 | A | 5 | 9 | 5 | TX | ||
| AY101D | 96774 | A | C | 1 | 5 | ZZ | 9X | |
| 785671-5 | 55972 | A | 5 | 9 | 5 | TX |
CAGE Information
| Code | Company |
|---|---|
| 01365 | MARINE CORPS LOGISTICS COMMAND TECHN |
| 55972 | HONEYWELL INTL INC DEFENSE AVIONICS |
| 96774 | HONEYWELL INTERNATIONAL INC. DBA HON |
| 35351 | GE AVIATION SYSTEMS LLC |
| 96214 | RAYTHEON COMPANY |
| 80249 | BAE SYSTEMS INFORMATION AND ELECTRON |
| 25500 | LOCKHEED MARTIN CORPORATION DBA LOCK |
| 03508 | GENERAL ELECTRIC CO SEMI-CONDUCTOR P |
| 20418 | DRS SUSTAINMENT SYSTEMS INC. DIV DRS |
| 99932 | MOOG INC. DBA MOOG COMPONENTS GROUP |
| 18876 | U S ARMY AVIATION AND MISSILE COMMAN |
| 11530 | LOCKHEED MARTIN CORPORATION DIV 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 | 3.0 CENTIMETER-GRAMS MAXIMUM |
| AJSL | BODY SIZE | 15 |
| CQZS | SHAFT SLOT DEPTH | 0.0220 INCHES MINIMUM SINGLE SHAFT AND 0.0320 INCHES MAXIMUM SINGLE SHAFT |
| CQTM | TERMINAL LOCATION | REAR |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5600 INCHES MINIMUM AND 1.6220 INCHES MAXIMUM |
| AJVF | PHASE SHIFT ANGLE IN DEG | 5.500 INPUT TO OUTPUT NOMINAL |
| AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 33.0 ALLQJAA3.500 FINISHED-CHAMFERED |
| ABHP | OVERALL LENGTH | 2.1000 INCHES MINIMUM AND 2.1620 INCHES MAXIMUM |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| CWXK | SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| ABPC | UNDERCUT WIDTH | 0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM |
| AAQL | BODY STYLE | STANDARD ROUND C |
| CRSJ | SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8660 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 42.00 NOMINAL |
| AJWG | SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| ABPA | UNDERCUT DIAMETER | 1.3144 INCHES MINIMUM AND 1.3150 INCHES MAXIMUM |
| AJWH | SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| CRHN | SHAFT SLOT WIDTH | 0.0220 INCHES MINIMUM SINGLE SHAFT AND 0.0320 INCHES MAXIMUM SINGLE SHAFT |
| AJWQ | PILOT LENGTH | 0.0400 NOMINAL INCHES |
| ABKK | FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| AJST | ROTOR INPUT CURRENT RATING | 65.0 MILLIAMPERES NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJWR | SHOULDER LENGTH | 0.1320 NOMINAL INCHES |
| AJXB | SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| 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 |
| AHCG | MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| AAVH | SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| CWYF | SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -10.0/+10.0 |
| AJTT | STATOR DC RESISTANCE IN OHMS | 10.80 NOMINAL |
| ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| ABXF | SHAFT LENGTH | 0.5400 INCHES NOMINAL SINGLE SHAFT |
| AAFZ | BODY MATERIAL | ALUMINUM |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| AJSW | ZRO RESISTANCE IN OHMS | 80.00 NOMINAL |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 400.00 NOMINAL |
| AJVW | ALIGNMENT HOLE QUANTITY | 3 |
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704-52 ,
70452 ,
5990-00-504-6023 ,
5990005046023 ,
005046023
,
AY201S3B ,
3563150-0310 ,
AY20153B ,
103778-01 ,
AY201S3B ,
20084 ,
3563150-0310 ,
M01092-2 ,
AY101D ,
785671-5 ,
CP35-9-11-1L ,
20084-1 ,
20084-1 ,
7406457P2 ,
7475539P1 ,
476596-6 ,
2G4005-8 ,
8485160 ,
704-52 ,
AY20153B ,
46285 ,
451-1268 ,
AY101D ,
785671-5 ,