The HOSE ASSEMBLY,NONMETALLIC is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024 OR ALUMINUM ALLOY 6061 OVERALL, flow_angle: 45.0 DEGREES, leg_length: 1.155 INCHES NOMINAL FIRST END IN, seat_angle: 12.0 DEGREES FIRST END, thread_class: 3B FIRST END, connection_type: THREADED INTERNAL TUBE FIRST END. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 4730-00-533-2850, 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 | ALUMINUM ALLOY 2024 OR ALUMINUM ALLOY 6061 OVERALL |
| flow_angle | 45.0 DEGREES |
| leg_length | 1.155 INCHES NOMINAL FIRST END IN |
| seat_angle | 12.0 DEGREES FIRST END |
| thread_class | 3B FIRST END |
| connection_type | THREADED INTERNAL TUBE FIRST END |
| connection_style | GRIPPING NIPPLE (NOSE) SECOND END |
| surface_treatment | ANODIZE OVERALL |
| operating_pressure | 6000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 1.625 INCHES FIRST END IN |
| maximum_operating_temp | 250.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| end_item_identification | AIRCRAFT APPLICATION |
| NSN | 4730-00-533-2850 |
| NOMINAL THREAD SIZE | 1.625 INCHES FIRST END IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| NOMINAL INSIDE DIAMETER HOSE ACCOMMODATED | 1.125 INCHES SECOND END IN |
| CONNECTION TYPE | THREADED EXTERNAL HOSE GRIPPING SECOND END |
| MATERIAL | ALUMINUM ALLOY 2024 OR ALUMINUM ALLOY 6061 OVERALL |
| END ITEM IDENTIFICATION | AIRCRAFT APPLICATION |
| NOMINAL OUTSIDE DIAMETER HOSE ACCOMMODATED | 1.437 INCHES SECOND END IN |
| OPERATING PRESSURE | 6000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| SEAT ANGLE | 12.0 DEGREES FIRST END |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 1.250 INCHES FIRST END IN |