4031916: FERRULE,COMPRESSION,TUBE FITTING.
FERRULE,COMPRESSION,TUBE FITTING. Key specifications include material: NICKEL ALLOY, overall_length: 0.675 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN, style_designator: INVERTED FLARE, casehardening_indicator: NOT CASEHARDENED, end_item_identification: ENGINE AIRCRAFT F100-PW-229 F15E, F16C/D., flange_outside_diameter: 0.489 INCHES MINIMUM AND 0.491 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 4730-01-451-5975, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | NICKEL ALLOY |
| overall_length | 0.675 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN |
| style_designator | INVERTED FLARE |
| casehardening_indicator | NOT CASEHARDENED |
| end_item_identification | ENGINE AIRCRAFT F100-PW-229 F15E, F16C/D. |
| flange_outside_diameter | 0.489 INCHES MINIMUM AND 0.491 INCHES MAXIMUM IN |
| sleeve_outside_diameter | 0.690 INCHES MINIMUM AND 0.694 INCHES MAXIMUM IN |
| hose/tube_outside_diameter_for_which_designed | 0.375 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN |
| NSN | 4730-01-451-5975 |
| STYLE DESIGNATOR | INVERTED FLARE |
| OVERALL LENGTH | 0.675 INCHES MINIMUM AND 0.695 INCHES MAXIMUM IN |
| SLEEVE OUTSIDE DIAMETER | 0.690 INCHES MINIMUM AND 0.694 INCHES MAXIMUM IN |
| CASEHARDENING INDICATOR | NOT CASEHARDENED |
| END ITEM IDENTIFICATION | ENGINE AIRCRAFT F100-PW-229 F15E, F16C/D. |
| MATERIAL | NICKEL ALLOY |
| FLANGE OUTSIDE DIAMETER | 0.489 INCHES MINIMUM AND 0.491 INCHES MAXIMUM IN |
| HOSE/TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED | 0.375 INCHES MINIMUM AND 0.380 INCHES MAXIMUM IN |
No substitute or cross-reference records for this part.