NSN 6695-01-448-5789
Part Details | FLUID PURITY CONTROLLER
6695-01-448-5789 A device designed for controlling fluid purity by stopping the flow of fluid below a preset valve. It may include a recorder and/or indicator.
Alternate Parts: 17B1N90011, 17B1N9001-1, DCU280A, DCU-280/A, 367063006, 367-063-006, 367063006, 367-063-006, 6695-01-448-5789, 01-448-5789, 6695014485789, 014485789
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
66 | SEP 03, 1997 | 01-448-5789 | 12941 ( CONTROLLER, FLUID PURITY ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6695-01-448-5789
Part Number | Cage Code | Manufacturer |
---|---|---|
17B1N9001-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
DCU-280/A | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
367-063-006 | 59211 | PARKER-HANNIFIN CORPORATIONDBA CUSTOMER SUPPORT MILITARY |
367-063-006 | 26055 | PARKER-HANNIFIN CORPORATIONDBA ELECTRONICS SYSTEMS DIVISION |
Technical Data | NSN 6695-01-448-5789
Characteristic | Specifications |
---|---|
POWER SOURCE | EXTERNAL |
MAXIMUM VOLTAGE RATING IN VOLTS | 28.0 DC |
MAXIMUM WATTAGE RATING IN WATTS | 61.6 |
MAXIMUM OVERALL LENGTH | 12.620 INCHES |
MAXIMUM OVERALL WIDTH | 4.880 INCHES |
MAXIMUM OVERALL HEIGHT | 7.620 INCHES |
SPECIAL FEATURES | CONTAINS SELF-TEST CAPABILITY, WILLAUTOMATICLLY TRANSFER CONTROL TO REDUNDANT CONTROL HALF HOUSED WITHIN THE SAME LRU, MODIFIED FROM 6695-01-344-3297 PER TCTO 1C-17A-791 |
END ITEM IDENTIFICATION | C-17 AIRCRAFT |
FUNCTIONAL DESCRIPTION | CONTROLLER FOR THE ON-BOARD INERT GAS GENERATING SYSTEM (OBIGGS), RECEIVES DISCREET AND ANALOG SIGNALS FROM OBIGGS COMPONENTS, COCKPIT SWITCHES, MAINTENANCE MONITOR PANEL, AND 1553 DATAFROM THE VATIOUS WARNING AND CAUTION SYSTEM (WACS) DATABUS AND THEN POWERS VARIOUS OBIGGS VALVES OPEN OR CLOSED TO CONTROL THE GENERATION AND DISTRIBUTION OF INERT GAS TO THE FUEL TANKS |