310C268-1: REPAIR FITTING ASSY.
The REPAIR FITTING ASSY is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_length: 1.060 INCHES NOMINAL IN, overall_diameter: 1.500 INCHES NOMINAL IN, special_features: MATERIAL IS IAW AMS-QQ-A-200/8; INSERT, SCREW THREAD IS 0.900 INCHES IN LENGTH AND 0.510 INCHES NOMINAL IN DIAMETER IN, end_item_identification: TAIL FIN ATTACHMENT FOR CH-53E MODEL AIRCRAFT, accessory_components_and_quantity: INSERT SCREW THREAD 1; REPAIR FITTING 1. This part is cataloged in the U.S.
Government catalog under NSN 1680-01-550-6854, 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 | ALUMINUM ALLOY |
| overall_length | 1.060 INCHES NOMINAL IN |
| overall_diameter | 1.500 INCHES NOMINAL IN |
| special_features | MATERIAL IS IAW AMS-QQ-A-200/8; INSERT, SCREW THREAD IS 0.900 INCHES IN LENGTH AND 0.510 INCHES NOMINAL IN DIAMETER IN |
| end_item_identification | TAIL FIN ATTACHMENT FOR CH-53E MODEL AIRCRAFT |
| accessory_components_and_quantity | INSERT SCREW THREAD 1; REPAIR FITTING 1 |
| thread_size_and_series/type_designator | 0.-13/2B UNIFIED NATIONAL COARSE (UNC) |
| part_name_assigned_by_controlling_agency | (INAVY) REPAIR FITTING ASSEMBLY |
| NSN | 1680-01-550-6854 |
| OVERALL DIAMETER | 1.500 INCHES NOMINAL IN |
| OVERALL LENGTH | 1.060 INCHES NOMINAL IN |
| ACCESSORY COMPONENTS AND QUANTITY | INSERT SCREW THREAD 1; REPAIR FITTING 1 |
| SPECIAL FEATURES | MATERIAL IS IAW AMS-QQ-A-200/8; INSERT, SCREW THREAD IS 0.900 INCHES IN LENGTH AND 0.510 INCHES NOMINAL IN DIAMETER IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | (INAVY) REPAIR FITTING ASSEMBLY |
| END ITEM IDENTIFICATION | TAIL FIN ATTACHMENT FOR CH-53E MODEL AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY |
| THREAD SIZE AND SERIES/TYPE DESIGNATOR | 0.-13/2B UNIFIED NATIONAL COARSE (UNC) |
No substitute or cross-reference records for this part.