| DRIVE SHAFT TYPE | THREADED |
| DRIVE CONNECTION TYPE | IMPULSE COUPLED |
| BODY MATERIAL | ALUMINUM ALLOY |
| CONTACT SET QUANTITY | 1 |
| DISTANCE BETWEEN MOUNTING FACILITY CENTERS | 4.185 INCHES NOMINAL |
| FEATURES PROVIDED | GROUNDING SWITCH |
| IGNITION TYPE FOR WHICH DESIGNED | SINGLE |
| IMPULSE QUANTITY PER REVOLUTION | 4 |
| MAXIMUM ADVANCE DEG | 20.0 |
| MOUNTING FACILITY QUANTITY | 2 |
| MOUNTING FACILITY | SLOT AND THREADED HOLE |
| MOUNTING FACILITY THREAD DIAMETER | 0.375 INCHES NOMINAL |
| MOUNTING FACILITY THREAD QUANTITY PER INCH | 16 |
| MOUNTING METHOD | FLANGE |
| MOUNTING SLOT LENGTH | 1.125 INCHES NOMINAL |
| MOUNTING SLOT WIDTH | 0.408 INCHES NOMINAL |
| MOUNTING STANDARD CONTROLLING AGENCY | SAE |
| PERFORMANCE TYPE | HIGH TENSION |
| POLE QUANTITY | 2 |
| ROTATION ELEMENT TYPE | UNMAGNETIZED, NONWOUND ROTOR |
| SHAFT ROTATION DIRECTION | COUNTERCLOCKWISE |
| SHAFT LENGTH | 0.835 INCHES NOMINAL |
| SPARK ADVANCE CONTROL METHOD | MANUAL |
| SPARK PLUG TERMINAL ACCOMMODATION THREAD SERIES | UNEF |
| SPARK PLUG TERMINAL ACCOMMODATION THREAD DIAMETER | 0.688 INCHES NOMINAL |
| SPECIAL FEATURES | GRUMMAN AEROSPACE CORP A10 AIRCRAFT |