Part Number: AS21922-12C

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CONDITION:
NS
SOCIETY OF AUTOMOTIVE ENGINEERS INC81343
THE BOEING COMPANY81205
MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M96906
MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M96906
CASEHARDENING INDICATORNOT CASEHARDENED
OVERALL LENGTH0.750 INCHES NOMINAL
FLANGE WIDTH0.090 INCHES NOMINAL
FLANGE OUTSIDE DIAMETER0.938 INCHES NOMINAL
SEAT ANGLE IN DEG35
SLEEVE OUTSIDE DIAMETER0.836 INCHES NOMINAL
HOSE/TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED0.750 INCHES NOMINAL
MATERIALSTEEL,CORROSION RESISTING,PER STD BELOW
SURFACE TREATMENTPASSIVATE
STYLE DESIGNATORFLARELESS
SPECIAL FEATURESSHELTER MARKED S-183/MSC-31, AIR TRANSPORTABLE,3SKIDS ON BOTTOM,LIFTINGAND TOWING EYES,SLINGS FOR LIFTING ANDHOLDDOWN,COMPLEMENT LISTING PER SCL- 1987 LESS EQUIPMENT LISTED IN PAR 3.6.1
A FLANGED CYLINDRICAL ITEM HAVING A SHARP CUTTING SURFACE ON THE INSIDE DIAMETER AT THE END OPPOSITE THE FLANGE. THE CUTTING EDGE, IN USE, IS DESIGNED TO IMBED IN THE TUBING DUE TO PRESSURE EXERTED WHEN THE OUTSIDE DIAMETER OF THE SLEEVE IS FORCED INTO AND AGAINST AN ANGULAR SEAT. THIS FIRMLY ATTACHES THE SLEEVE TO THE TUBING AND THE FLANGED END THEN SERVES AS A BEARING SURFACE FOR THE COUPLING NUT TO BRING THE TUBING INTO THE MATING FITTING.