| RAYTHEON COMPANY | |
| 9032.10.0000 | |
| AIRCRAFT, TOMCAT F-14 | |
| 0.500 INCHES MAXIMUM | |
| 0.315 INCHES NOMINAL | |
| 0.572 INCHES MAXIMUM | |
| DISC | |
| CLAMP | |
| HERMETICALLY SEALED CASE | |
| INCREASE | |
| 1 POLE, SINGLE THROW, NORMALLY CLOSED, MOMENTARY ACTION | |
| TAB, SOLDER LUG | |
| 1.0 AMPERES RESISTIVE LOAD FIRST VOLTAGE | |
| 1.0 AMPERES RESISTIVE LOAD SECOND VOLTAGE | |
| DEACTUATION POINT NOT ADJUSTABLE AND ACTUATION POINT NOT ADJUSTABLE | |
| 100.00 ACTUATION POINT MINIMUM DEGREES FAHRENHEIT AND 110.00 ACTUATION POINT MAXIMUM DEGREES FAHRENHEIT AND 91.00 DEACTUATION POINT MINIMUM DEGREES FAHRENHEIT AND 101.00 DEACTUATION POINT MAXIMUM DEGREES FAHRENHEIT | |
| 115.0 AC AT SEA LEVEL FIRST VOLTAGE | |
| 30.0 DC AT SEA LEVEL SECOND VOLTAGE | |
| 60.0 SINGLE VOLTAGE | |
| GAS | |
| 59 DISC | |
| 96906-MIL-STD-202 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
