204-70045-363: LONGERON.
The LONGERON is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 3.700 INCHES NOMINAL IN, overall_length: 74.500 INCHES NOMINAL IN, special_features: HEAT TREAT T62; FINISH SRF-2.30, aircraft_location: LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-110-6516, 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 2024 |
| overall_width | 3.700 INCHES NOMINAL IN |
| overall_length | 74.500 INCHES NOMINAL IN |
| special_features | HEAT TREAT T62; FINISH SRF-2.30 |
| aircraft_location | LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE |
| material_thickness | 0.050 INCHES NOMINAL IN |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | E-3A A |
| material_document_and_classification | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-110-6516 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 74.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.700 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T62; FINISH SRF-2.30 |
| AIRCRAFT LOCATION | LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | E-3A A |
No substitute or cross-reference records for this part.