| MATERIAL | ALUMINUM ALLOY 6061 BODY |
| ALUMINUM ALLOY 6061 NIPPLE |
| ALUMINUM ALLOY 2024 NUT |
| ALUMINUM ALLOY 6061 SHOULDER |
| ALUMINUM ALLOY 2024 UNION |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/8,ALLOY 6061,T6 FED SPEC SINGLE MATERIAL RESPONSE BODY |
| QQ-A-225/8,ALLOY 6061,T6 FED SPEC SINGLE MATERIAL RESPONSE NIPPLE |
| QQ-A-225/6,ALLOY 2024 FED SPEC SINGLE MATERIAL RESPONSE NUT |
| QQ-A-225/8,ALLOY 6061,T651 FED SPEC SINGLE MATERIAL RESPONSE SHOULDER |
| QQ-A-225/6,ALLOY 2024,@0 FED SPEC SINGLE MATERIAL RESPONSE UNION |
| MEDIA FOR WHICH DESIGNED | WATER-OIL-GAS SINGLE RESPONSE |
| MAXIMUM OPERATING PRESSURE | 1250.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
| MAXIMUM OPERATING TEMP | -54.0 DEG FAHRENHEIT 1ST RESPONSE |
| 135.0 DEG FAHRENHEIT 2ND RESPONSE |
| CONNECTION TYPE | THREADED INTERNAL TUBE 1ST END |
| THREADED EXTERNAL HOSE GRIPPING 2ND END |
| CONNECTION STYLE | SWIVEL NUT, FLARE (TUBE) STYLE 3 OPTIONAL END 1ST END |
| SWIVEL NUT (HOSE GRIPPING) 2ND END |
| SEAT ANGLE | 37.0 DEGREES 1ST END |
| NOMINAL INSIDE DIAMETER HOSE ACCOMMODATED | 0.875 INCHES 2ND END |
| NOMINAL OUTSIDE DIAMETER HOSE ACCOMMODATED | 1.109 INCHES 2ND END |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 1.000 INCHES 1ST END |
| THREAD SERIES DESIGNATOR | UNJ 1ST END |
| NOMINAL THREAD SIZE | 1.312 INCHES 1ST END |
| THREAD QUANTITY PER INCH | 12 1ST END |
| THREAD CLASS | 3B 1ST END |
| LEG LENGTH | 1.500 INCHES NOMINAL 1ST END |
| 2.062 INCHES NOMINAL 2ND END |
| FLOW ANGLE | 45.0 DEGREES |
| FURNISHED ITEMS AND QUANTITY | 1 HOSE COUPLING NUT |
| SPECIAL FEATURES | GRUMMAN A10 AIRCRAFT |
| SPEC/STD CONTROLLING DATA | |
| MANUFACTURERS CODE | 81349 |
| NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MIL-DTL-27272 |
| MANUFACTURERS CODE | 96906 |
| DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MS27382-16 |