DPL4021T1210W: REDUCER,TUBE.
The REDUCER,TUBE is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY UNS R54520 OVERALL, seat_angle: 12.0 DEGREES FIRST END, reducer_type: CONCENTRIC, thread_class: 3B FIRST END, connection_type: UNTHREADED INTERNAL TUBE SECOND END, connection_style: SWAGED W/ GROOVES (TUBE) SECOND END. This part is cataloged in the U.S.
Government catalog under NSN 4730-01-460-3932, 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 | TITANIUM ALLOY UNS R54520 OVERALL |
| seat_angle | 12.0 DEGREES FIRST END |
| reducer_type | CONCENTRIC |
| thread_class | 3B FIRST END |
| connection_type | UNTHREADED INTERNAL TUBE SECOND END |
| connection_style | SWAGED W/ GROOVES (TUBE) SECOND END |
| special_features | SAFETY WIRE HOLE IS W |
| operating_pressure | 4000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 1.062 INCHES FIRST END IN |
| nominal_overall_length | 3.160 INCHES IN |
| end_item_identification | AIRCRAFT,AIRLIFTER C-17A A |
| thread_quantity_per_inch | 12 FIRST END |
| NSN | 4730-01-460-3932 |
| CONNECTION STYLE | SWAGED W/ GROOVES (TUBE) SECOND END |
| TUBING WALL NOMINAL THICKNESS FOR WHICH DESIGNED | 0.052 INCHES SECOND END IN |
| NOMINAL OVERALL LENGTH | 3.160 INCHES IN |
| CONNECTION TYPE | UNTHREADED INTERNAL TUBE SECOND END |
| CONNECTION TYPE | THREADED INTERNAL TUBE FIRST END |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.625 INCHES SECOND END IN |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.750 INCHES FIRST END IN |
| OPERATING PRESSURE | 4000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| NOMINAL THREAD SIZE | 1.062 INCHES FIRST END IN |
| SEAT ANGLE | 12.0 DEGREES FIRST END |