| CONNECTION TYPE | THREADED INTERNAL TUBE ALL ENDS |
| MEDIA FOR WHICH DESIGNED | FUEL SINGLE RESPONSE |
| MEASURING METHOD AND LENGTH | 14.500 INCHES NOMINAL OVERALL |
| CROSS-SECTIONAL SHAPE STYLE | ROUND |
| TEMP RATING | -65.0 DEG FAHRENHEIT AND |
| 250.0 DEG FAHRENHEIT SINGLE RESPONSE |
| MAXIMUM OPERATING PRESSURE | 1000.0 POUNDS PER SQUARE INCH |
| LAYER COMPOSITION AND LOCATION | 1ST LAYER BRAIDED CORROSION RESISTANT STEEL WIRE, PARTIAL COVERAGE AND |
| OUTER LAYER BRAIDED CORROSION RESISTANT STEEL WIRE |
| INSIDE DIAMETER | 0.219 INCHES NOMINAL |
| OUTSIDE DIAMETER | 0.250 INCHES NOMINAL |
| INSIDE SURFACE CONDITION | SMOOTH |
| CONNECTION STYLE | SWIVEL NUT FLARE ALL ENDS |
| SEAT ANGLE | 37.0 DEGREES ALL ENDS |
| END CONNECTION DESIGN | STRAIGHT 1ST END |
| THREAD SERIES DESIGNATOR | UNJF ALL ENDS |
| NOMINAL THREAD SIZE | 0.438 INCHES ALL ENDS |
| THREAD CLASS | 3B ALL ENDS |
| THREAD DIRECTION | RIGHT-HAND ALL ENDS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HOSE ASSY, LUBE, LUBE/FUEL INSTALLATION, T400 TURBOSHAFT ENGINE TEST SYSTEM |
| SPEC/STD CONTROLLING DATA | |
| MANUFACTURERS CODE | 81349 |
| NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MIL-DTL-83796/1 |
| DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | M83796/1E1440A |