The REGULATOR,ENGINE GENERATOR is a the manufacturer industrial component. Key specifications include material: STEEL CORROSION RESISTING OVERALL, connection_style: PLAIN (OPTIONAL END), style_designator: PLUG, MACHINE, nominal_thread_size: 1.312 INCHES INTERNAL IN, end_item_identification: REAR ARM CYLINDER ASSEMBLY;CARRIER, BRIDGE LAUNCHING, thread_quantity_per_inch: 12 INTERNAL. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5310-00-769-6521, 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 CORROSION RESISTING OVERALL |
| connection_style | PLAIN (OPTIONAL END) |
| style_designator | PLUG, MACHINE |
| nominal_thread_size | 1.312 INCHES INTERNAL IN |
| end_item_identification | REAR ARM CYLINDER ASSEMBLY;CARRIER, BRIDGE LAUNCHING |
| thread_quantity_per_inch | 12 INTERNAL |
| NSN | 5310-00-769-6521 |
| STYLE DESIGNATOR | KEY |
| MATERIAL | STEEL COMP 1020 OVERALL |
| INTERNAL PREBENT KEY WIDTH | 0.224 INCHES MINIMUM AND 0.244 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.0498 INCHES MINIMUM AND 0.0698 INCHES MAXIMUM IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| HOLE DIAMETER | 1.641 INCHES MINIMUM AND 1.656 INCHES MAXIMUM IN |
| OUTSIDE DIAMETER | 2.531 INCHES MINIMUM AND 2.625 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, T-39; HELICOPTER, IROQUOIS UH-1; HELICOPTER, APACHE AH-64; HELICOPTER, KIOWA OH-58 A&C; HELICOPTER, OBSERVATION (AHIP), OH-58D; HELICOPTER, BLACK HAWK UH-60A; HELICOPTER, ELECTRONIC COUNTERMEASURES, EH-60A; TRUCK, FIRE/CRASH P2; HELICOPTER, CHINOOK, CH-47; HELICOPTER, COBRA/TOW, AH SERIES A |
| INTERNAL PREBENT KEY LENGTH | 0.1225 INCHES MINIMUM AND 0.1425 INCHES MAXIMUM IN |
| DISTANCE FROM CENTERLINE TO INSIDE OF PREBENT KEY | 0.672 INCHES MINIMUM AND 0.703 INCHES MAXIMUM IN |