| BOLT HOLE QUANTITY | 4 |
| CONNECTION TYPE | FLANGE, RECTANGULAR W/HOLES |
| CRITICALITY CODE JUSTIFICATION | FEAT AND AGAV |
| FACE TO FACE DISTANCE | 1.378 INCHES |
| FLANGE FACE DESIGN | PLAIN |
| MAXIMUM OPERATING PRESSURE AND MEDIA FOR WHICH DESIGNED | 60.0 POUNDS PER SQUARE INCH FUEL/OIL, HYDROCARBON |
| III MATERIAL | ALUMINUM ALLOY BODY |
| INLET RELATIONSHIP WITH OUTLET | IDENTICAL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VALVE SHUT-OFF FUEL SYSTEM FUSLAGE |
| PROPRIETARY CHARACTERISTICS | PACS |
| MAXIMUM OPERATING TEMP AND MEDIA FOR WHICH DESIGNED | 160.0 DEG FAHRENHEIT FUEL/OIL, HYDROCARBON |
| SPECIAL FEATURES | 1WEIGHT 2.150 LBS; VALVE MEETS MIL-V-8608A; CONTAINS MANUAL OVERRIDE; AMBIENT TEMP -65 DEG FEH TO +160 DEG FEH; FLUID TEMP -65 DEG FEH TO +135 DEG FEH; PROOF PRESSURE 188 PSIG; BURST PRESSURE 375 PSIG; VALVE MEETS MIL-V-8608A; WEIGHT 2.15 LBS |
| VALVE OPERATION METHOD | ELECTRIC MOTOR |
| VOLTAGE IN VOLTS AND CURRENT TYPE | 28.0 DC |
| STEM TYPE | NONRISING |
| SUPPLEMENTARY FEATURES | APPL TO HELICOPTER,UH-60 AIR REFUELING |