FITTING ASSEMBLY,HEAD END CYLIND. Key specifications include length: 120.000 INCHES MINIMUM AND 144.000 INCHES MAXIMUM IN, material: STEEL COMP 4130, heat_treatment: HARD TEMPER, basic_shape_style: FLAT, surface_condition: ROUGH TURNED OVERALL, fabrication_method: ROLLED. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9510-00-079-6184, 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.
| length | 120.000 INCHES MINIMUM AND 144.000 INCHES MAXIMUM IN |
| material | STEEL COMP 4130 |
| heat_treatment | HARD TEMPER |
| basic_shape_style | FLAT |
| surface_condition | ROUGH TURNED OVERALL |
| fabrication_method | ROLLED |
| cross-sectional_width | 3.000 INCHES NOMINAL IN |
| end_item_identification | F/A-18E/F HORNET AIRCRAFT |
| cross-sectional_thickness | 1.0000 INCHES NOMINAL IN |
| nondefinitive_spec/std_data | F3 CONDITION |
| specification/standard_data | 81343-AMS-S-6758 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| cross_section_outside_diameter | 1.000 INCHES NOMINAL IN |
| NSN | 9510-00-079-6184 |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| CROSS-SECTIONAL WIDTH | 3.000 INCHES NOMINAL IN |
| BASIC SHAPE STYLE | FLAT |
| MATERIAL | STEEL COMP 4130 |
| NONDEFINITIVE SPEC/STD DATA | F4 CONDITION AND FLAT FORM |
| CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL IN |
| WEIGHT PER UNIT MEASURE | 10.200 POUNDS PER LINEAR FOOT LBS |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6758 MIL SPEC 1ST MATERIAL RESPONSE |
No verified substitutes available.