CYLINDER AND PISTON ASSEMBLY,LAN. Key specifications include material: STEEL COMP 12L14 OVERALL, flow_angle: 45.0 DEGREES, leg_length: 0.859 INCHES NOMINAL SECOND END IN, seat_angle: 12.0 DEGREES FIRST END, thread_class: 2A FIRST END A, connection_type: THREADED EXTERNAL PIPE SECOND END. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 4730-01-037-4916, 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 COMP 12L14 OVERALL |
| flow_angle | 45.0 DEGREES |
| leg_length | 0.859 INCHES NOMINAL SECOND END IN |
| seat_angle | 12.0 DEGREES FIRST END |
| thread_class | 2A FIRST END A |
| connection_type | THREADED EXTERNAL PIPE SECOND END |
| connection_style | FLARELESS (TUBE) FIRST END |
| special_features | GRUMMAN AIRCRAFT MODEL NO. A10 |
| nominal_thread_size | 0.250 INCHES SECOND END IN |
| media_for_which_designed | HYDRAULIC FLUID SINGLE RESPONSE |
| thread_series_designator | NPTF SECOND END |
| nondefinitive_spec/std_data | 21E FIGURE |
| NSN | 4730-01-037-4916 |
| CONNECTION STYLE | PLAIN (PIPE) SECOND END |
| CONNECTION TYPE | THREADED EXTERNAL TUBE FIRST END |
| NONDEFINITIVE SPEC/STD DATA | 21E FIGURE |
| THREAD CLASS | 2A FIRST END A |
| SPECIAL FEATURES | GRUMMAN AIRCRAFT MODEL NO. A10 |
| THREAD SERIES DESIGNATOR | UNF FIRST END |
| SEAT ANGLE | 12.0 DEGREES FIRST END |
| SPECIFICATION/STANDARD DATA | 81343-J514 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| MATERIAL | STEEL COMP 12L14 OVERALL |
| NOMINAL THREAD SIZE | 0.437 INCHES FIRST END IN |