COMPRESSOR,AIRCRAFT GAS TURBINE. Key specifications include material: STEEL OVERALL, flow_angle: 90.0 DEGREES, leg_length: 2.330 INCHES NOMINAL FIRST END IN, seat_angle: 37.0 DEGREES FIRST END, thread_class: 2A ALL ENDS A, connection_type: THREADED EXTERNAL BOSS SECOND END. This part is cataloged in the Federal Logistics Information System under NSN 4730-01-050-1599, 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 | 2.330 INCHES NOMINAL FIRST END IN |
| seat_angle | 37.0 DEGREES FIRST END |
| thread_class | 2A ALL ENDS A |
| connection_type | THREADED EXTERNAL BOSS SECOND END |
| connection_style | EXTERNAL SEAT FOR GASKET SEAL (BOSS) SECOND END |
| surface_treatment | CADMIUM OVERALL |
| operating_pressure | 3000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 1.875 INCHES ALL ENDS IN |
| maximum_operating_temp | 250.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| end_item_identification | GRUMMAN A-10 ACFT; MULTIPLE LAUNCH ROCKET SYSTEM (MLRS) |
| NSN | 4730-01-050-1599 |
| CONNECTION STYLE | EXTERNAL SEAT FOR GASKET SEAL (BOSS) SECOND END |
| LEG LENGTH | 2.390 INCHES NOMINAL SECOND END IN |
| FLOW ANGLE | 90.0 DEGREES |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 1.500 INCHES FIRST END IN |
| MEDIA FOR WHICH DESIGNED | HYDRAULIC FLUID SINGLE RESPONSE |
| FURNISHED ITEMS AND QUANTITY | 1 TUBE COUPLING NUT AND 1 COMPRESSION SLEEVE |
| NOMINAL THREAD SIZE | 1.875 INCHES ALL ENDS IN |
| OPERATING PRESSURE | 3000.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| SURFACE TREATMENT | CADMIUM OVERALL |
| MATERIAL | STEEL OVERALL |