NSN 6685-01-483-9725 · NIIN 014839725 · FSC 6685
NO DASHES 6685014839725
In Stock
SENSOR,VIBRATION
Pressure, Temperature, and Humidity Measuring and Controlling Instruments
Application: F119 ENGINE FOR F22 AIRCRAFT
Technical characteristics
7 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 2.075 |
| AGAV | END ITEM IDENTIFICATION | F119 ENGINE FOR F22 AIRCRAFT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | VIBRATION SENSOR |
| FEAT | SPECIAL FEATURES | OPERATING FREQUENCY RANGE 70 TO 800 HZ;INTEGRAL 15 INCH DOUBLE SHIELDED PIGTAIL CABLE WITH A PURPLE POLYTETRAFLUOROETHYLENE IMPREGNATED NOMEX OVERBRAID;I/O CONNECTIONS ARE MADE THROUGH A D38999/26MC98PN CONNECTOR |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | FROM A CONDITION OF STEADY-STATE AMBIENT AIR TEMPERATURE OF 159 DEG C AND A STEADY-STATE MOUNTING TEMP OF 218 DEG C THE AMBIENT AND MOUNTING TEMP MAY RAMP SIMULTANEOUSLY TO 207 DEG C AND 332 DEG C RESPECTIVELY AT RESPECTIVE RATES NOT TO EXCEED 22 DEG C/SEC AND 111 DEG C/SEC; AND MAY DWELL AT THOSE TEMPERATURES FOR A TIME NOT TO EXCEED 5 MINUTES; TEMPERATURES SHALL THEN RETURN TO THE ORIGINAL STEADY-STATE TEMP;THREE 1/4-28 INTEGRAL WASHER BOLTS IN A TRIANGULAR 30-BOLT MOUNTING PATTERN ON A 1.625 DIAMETER BOLT CIRCLE;HOUSING WIDTH 0.925 INCHES;EXTENT OF MOUNTING FLANGE 2.385 IN. DIA;MOUNTING FLANGE THICKNESS 0.280 INCHES |