| AERONAUTICAL STANDARDS GROUP DEPT OF NAVY AND AIR FORCE | 88044 |
| AERONAUTICAL STANDARDS GROUP DEPT OF NAVY AND AIR FORCE | 88044 |
| SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 |
| SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 |
| CENTER LINE STAMPING CO | 92906 |
| MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | 96906 |
| MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M | 96906 |
| PROJECT MANAGER AMPHIBIOUS LIGHTERS ST LOUIS MO | 25169 |
| CASEHARDENING INDICATOR | NOT CASEHARDENED |
| OVERALL LENGTH | 0.781 INCHES NOMINAL |
| III END ITEM IDENTIFICATION | GRUMMAN A-10 AIRCRAFT |
| FLANGE WIDTH | 0.281 INCHES NOMINAL |
| FLANGE OUTSIDE DIAMETER | 1.222 INCHES NOMINAL |
| SEAT ANGLE IN DEG | 33 |
| SLEEVE OUTSIDE DIAMETER | 1.081 INCHES NOMINAL |
| HOSE/TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED | 1.000 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| MATERIAL | STEEL |
| SURFACE TREATMENT | CADMIUM |
| STYLE DESIGNATOR | SLEEVE |
| 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. |
