AERONAUTICAL STANDARDS GROUP DEPT OF NAVY AND AIR FORCE | 88044 |
SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 |
FABER ENTERPRISES, INC. | 14397 |
CROWN FITTING CO INC | 22995 |
COLLINS ENGINEERING CORP | 71563 |
MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | 96906 |
CASEHARDENING INDICATOR | NOT CASEHARDENED |
OVERALL LENGTH | 0.438 INCHES NOMINAL |
III END ITEM IDENTIFICATION | F-16 AIRCRAFT |
FLANGE WIDTH | 0.156 INCHES NOMINAL |
FLANGE OUTSIDE DIAMETER | 0.445 INCHES NOMINAL |
SEAT ANGLE IN DEG | 33 |
SLEEVE OUTSIDE DIAMETER | 0.366 INCHES NOMINAL |
HOSE/TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED | 0.313 INCHES NOMINAL |
MATERIAL | STEEL COMP 304 OR STEEL COMP 316 |
SURFACE TREATMENT | PASSIVATE |
STYLE DESIGNATOR | SLEEVE |
SPECIFICATION/STANDARD DATA | 96906-MS20819 GOVERNMENT STANDARD |
A flanged cylindrical metallic item designed to be used on tubing to back up the flared end and to provide a bearing surface for the coupling nut, thereby reducing wear on the tubing flare. The inside diameter of the flanged end is countersunk to form a seat for the flare when assembled to a mating fitting. |