SLEEVE,COMPRESSION,TUBE-HOSE FIT. Key specifications include material: STEEL OVERALL, flow_angle: 90.0 DEGREES, leg_length: 0.790 INCHES NOMINAL FIRST END IN, seat_angle: 20.0 DEGREES FIRST END, reducer_type: CONCENTRIC, thread_class: 2A FIRST END A. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 4730-00-069-1187, 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 | STEEL OVERALL |
| flow_angle | 90.0 DEGREES |
| leg_length | 0.790 INCHES NOMINAL FIRST END IN |
| seat_angle | 20.0 DEGREES FIRST END |
| reducer_type | CONCENTRIC |
| thread_class | 2A FIRST END A |
| connection_type | BUTT WELD PIPE SECOND END |
| connection_style | BEVELED (PIPE) SECOND END |
| nominal_thread_size | 0.531 INCHES FIRST END IN |
| maximum_operating_temp | 200.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| nominal_overall_length | 4.000 INCHES IN |
| thread_quantity_per_inch | 24 FIRST END |
| NSN | 4730-00-069-1187 |
| MATERIAL | COPPER ALLOY OVERALL |
| THREAD SERIES DESIGNATOR | NPTF SECOND END |
| NOMINAL THREAD SIZE | 0.531 INCHES FIRST END IN |
| NONDEFINITIVE SPEC/STD DATA | 7A FIGURE A |
| THREAD SERIES DESIGNATOR | UNS FIRST END |
| THREAD QUANTITY PER INCH | 24 FIRST END |
| FLOW ANGLE | 90.0 DEGREES |
| END ITEM IDENTIFICATION | 3810-00-151-4431 CRANE-SHOVEL; 2330-01-275-7474 HEMAT TRAILER;2320-01-097-0248,2320-01-097-0249,2320-01-100-7672,2320-01-097-0260,2320-01-195-7641 HEMTT (HEAVY EXPANDED MOBILITY TACTICAL TRUCKS); MRAP - COUGAR CAT1 A1; MRAP - COUGAR ISS 1.5; MRAP - COUGAR ISS 1.0; HIGH-MOBILITY ARTILLERY ROCKET SYSTEM (HIMARS) |
| SPECIFICATION/STANDARD DATA | 81343-J246 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| LEG LENGTH | 0.790 INCHES NOMINAL FIRST END IN |