394568: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.400 INCHES NOMINAL IN, overall_length: 4.700 INCHES NOMINAL IN, special_features: T6 EXTR BAC-1514-487 X 2.4; OPTIONAL 2024 -T4 EXTR QQ-A-267 T4 TEMPER; FINISH F-2.30, aircraft_location: FLOOR BEAM CHORD, aircraft_station_number: FS890.30. This part is cataloged in the U.S.
Government catalog under NSN 5340-00-804-0457, 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 7075 |
| overall_width | 2.400 INCHES NOMINAL IN |
| overall_length | 4.700 INCHES NOMINAL IN |
| special_features | T6 EXTR BAC-1514-487 X 2.4; OPTIONAL 2024 -T4 EXTR QQ-A-267 T4 TEMPER; FINISH F-2.30 |
| aircraft_location | FLOOR BEAM CHORD |
| aircraft_station_number | FS890.30 |
| end_item_identification | KC-135 |
| aircraft_mission_design_series | KC-135 ACFT |
| material_document_and_classification | QQ-A-277 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | CLIP |
| NSN | 5340-00-804-0457 |
| STYLE DESIGNATOR | SINGLE LOOP |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5510 ASSN STD SINGLE MATERIAL RESPONSE BAND |
| DIAMETER | 0.199 INCHES MINIMUM AND 0.209 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.484 INCHES MINIMUM AND 0.516 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.046 INCHES MINIMUM AND 0.056 INCHES MAXIMUM IN |
| DISTANCE FROM LOOP CENTER TO TONGUE END | 1.126 INCHES NOMINAL IN |
| TONGUE HOLE TYPE | ROUND, UNTHREADED |
| CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE | 0.898 INCHES MINIMUM AND 0.918 INCHES MAXIMUM IN |
| MATERIAL | STEEL COMP 321 BAND |
| LOOP INSIDE DIAMETER | 0.625 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.