CENTER TO CENTER DISTANCE | 2.620 INCHES |
CONNECTION STYLE | DOUBLE COMPRESSION(TUBE) ERR-100 |
CONNECTION TYPE | THREADED INTERNAL TUBE 2ND END |
CONNECTION TYPE | THREADED INTERNAL TUBE 1ST END |
CONNECTION TYPE | UNTHREADED EXTERNAL TUBE 3RD END |
CONNECTION STYLE | GROOVED (TUBE) 3RD END |
FLOW CONTROL DEVICE | PISTON |
MATERIAL | ALUMINUM ALLOY BODY |
PROPRIETARY CHARACTERISTICS | PACS |
MAXIMUM OPERATING TEMP | 275.0 DEG FAHRENHEIT SINGLE RESPONSE |
MAXIMUM OPERATING PRESSURE | 3000.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
MEDIA FOR WHICH DESIGNED | FUEL/OIL, HYDROCARBON SINGLE RESPONSE |
NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.250 INCHES 1ST END |
NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.250 INCHES 2ND END |
SPECIAL FEATURES | A-10 AIRCRAFT |
SEAT ANGLE | 45.0 DEGREES 1ST END |
SEAT ANGLE | 45.0 DEGREES 2ND END |
VALVE OPERATION METHOD | AUTOMATIC |
VALVE DISCHARGE FLOW RATE | 2.5 GALLONS PER MINUTE |
STYLE DESIGNATOR | TEE W/OFFSET |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625,TYPE 2 MIL SPEC SINGLE TREATMENT RESPONSE |
SURFACE TREATMENT | ANODIZE |
THREAD CLASS | 3B 1ST END |
THREAD CLASS | 3B 2ND END |
THREAD DIRECTION | RIGHT-HAND 1ST END |
THREAD DIRECTION | RIGHT-HAND 2ND END |