| NORTHROP GRUMMAN SYSTEMS CORPORATION | |
| ROBERT M. HADLEY COMPANY, INC.,RAYTHEON COMPANY,RAYTHEON COMPANY,NORTHROP GRUMMAN SYSTEMS CORPORATION | |
| AIRCRAFT, TOMCAT F-14 | |
| NOT ESTABLISHED | |
| 2.840 INCHES MAXIMUM | |
| 0.188 INCHES NOMINAL SINGLE GROUP | |
| 400.0 HERTZ NOMINAL SINGLE COMPONENT | |
| SINGLE PHASE TO SINGLE PHASE SINGLE COMPONENT | |
| INTERNAL SHIELD BROUGHT OUT TO TERMINAL SINGLE COMPONENT | |
| 2.000 INCHES MAXIMUM | |
| 2.000 INCHES MAXIMUM | |
| 1.690 INCHES MAXIMUM | |
| 2.375 INCHES NOMINAL SINGLE MOUNTING FACILITY SINGLE CENTER GROUP | |
| FULLY INCLOSED | |
| 2 | |
| FLANGE SINGLE GROUP AND UNTHREADED HOLE | |
| 1 PRIMARY SINGLE COMPONENT AND 1 SECONDARY | |
| 2.5 AMPERES AC MAXIMUM | |
| 115.00 AC VOLTS NOMINAL SINGLE COMPONENT SINGLE PRIMARY | |
| 9.00 AC VOLTS NOMINAL SINGLE COMPONENT SINGLE SECONDARY AND 10.00 AC VOLTS NOMINAL AND 12.00 AC VOLTS NOMINAL AND 28.00 AC VOLTS NOMINAL | |
| 9 TAB, SOLDER LUG |
