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| MRC | Criteria | Characteristic |
|---|---|---|
| AAXX | MOUNTING TYPE | BASE, SHOCK MOUNT |
| AWZJ | POWER SOURCE | EXTERNAL |
| ZZZV | III FSC APPLICATION DATA | AIRCRAFT FLIGHT DIRECTOR SYSTEM. F-105 AND T-38 AIRCRAFT |
| AXQK | OUTPUT INTELLIGENCE TYPE | HORIZONTAL VERTICAL ACCELERATION SIGNAL DISPLACEMENT ANALOG DATA |
| FAAZ | PHASE | SINGLE |
| AXQH | INPUT INTELLIGENCE TYPE | PITCH-ROLL SIGNAL DATA HEADING ERROR COURSE |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| AEEF | CONNECTOR MANUFACTURER PART NUMBER | KPTIH20-41P |
| SR-1 | MANUFACTURERS CODE | 81349 |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| SR-1 | NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MILC27170 |
| SR-1 | DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | CPU4A |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26.5 |
| AARB | TERMINAL TYPE | CONNECTOR, RECEPTACLE |
| SR-1 | SPEC/STD CONTROLLING DATA | |
| APXH | TERMINAL LOCATION | END |
| AEEE | CONNECTOR MANUFACTURER CODE | 71468 |
| CPU-1506-1 | CPU-123E B | CPU-133 A | CPU-133 A |
| CPU-133 A | CPU-1.4-EB | CPU-136 A | CPU-133 A |
| CPU-123G B | CPU 1017 | CPU-133 A | CPU-136 A |
| CPU-1504-1 | CPU-133 A | CPU 1017 | CPU-123E B |
 |
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