AN150544: STUD,STEPPED.
The STUD,STEPPED is a the manufacturer industrial component. Key specifications include material: STEEL, thread_class: 3A NUT THREAD A, overall_length: 1.125 INCHES NOMINAL IN, style_designator: STEPPED, thread_direction: RIGHT-HAND NUT THREAD, surface_treatment: CADMIUM OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 5307-01-735-0185, 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 |
| thread_class | 3A NUT THREAD A |
| overall_length | 1.125 INCHES NOMINAL IN |
| special_features | CRITICAL APPLICATION ITEM (CAI); DESCRIPTION: STUD, STEPPED, 1.5 DIA ENGAGEMENT, .250-20 X .190-32; SYSTEM: F/A-18E-G FLIGHT CONTROLS, FC MECH (LEADING EDGE FLAP) |
| style_designator | STEPPED |
| thread_direction | RIGHT-HAND NUT THREAD |
| surface_treatment | CADMIUM OVERALL |
| nominal_thread_size | 0.1900 INCHES FIRST MOUNTING FACILITY ALL CENTER GROUPINGS IN |
| supplementary_features | TO PROVIDE MOUNTING ATTACH POINT FOR THE ASYMMETRY CONTROL UNIT (ACU) TO THE OUTBOARD LEADING EDGE FLAP (OLEF) TRANSMISSION |
| end_item_identification | FIGHTER AIRCRAFT (F18 E/F) |
| thread_quantity_per_inch | 20 NUT THREAD |
| thread_series_designator | UNF FIRST MOUNTING FACILITY ALL CENTER GROUPINGS |
| NSN | 5307-01-735-0185 |
| SUPPLEMENTARY FEATURES | TO PROVIDE MOUNTING ATTACH POINT FOR THE ASYMMETRY CONTROL UNIT (ACU) TO THE OUTBOARD LEADING EDGE FLAP (OLEF) TRANSMISSION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| STYLE DESIGNATOR | STEPPED |
| OVERALL LENGTH | 1.125 INCHES NOMINAL IN |
| THREAD DIRECTION | RIGHT-HAND NUT THREAD |
| THREAD DIRECTION | RIGHT-HAND FIRST MOUNTING FACILITY ALL CENTER GROUPINGS |
| NOMINAL THREAD SIZE | 0.2500 INCHES NUT THREAD IN |
| NOMINAL THREAD SIZE | 0.1900 INCHES FIRST MOUNTING FACILITY ALL CENTER GROUPINGS IN |
| SPECIAL FEATURES | CRITICAL APPLICATION ITEM (CAI); DESCRIPTION: STUD, STEPPED, 1.5 DIA ENGAGEMENT, .250-20 X .190-32; SYSTEM: F/A-18E-G FLIGHT CONTROLS, FC MECH (LEADING EDGE FLAP) |
| SURFACE TREATMENT | CADMIUM OVERALL |
No substitute or cross-reference records for this part.