L2400014-005: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 6.750 INCHES NOMINAL IN, overall_length: 37.210 INCHES NOMINAL IN, special_features: NHA L2400001;OPPOSITE -006;CRITICAL FEATURES SUCH AS TOLERANCE, FIT, RESTRICTION OR APPLICATION.ACTION ID 45473258, aircraft_location: VERTICAL STABILIZER LWR RUDDER SEAL LAND, material_thickness: 0.100 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-437-7261, 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 | 6.750 INCHES NOMINAL IN |
| overall_length | 37.210 INCHES NOMINAL IN |
| special_features | NHA L2400001;OPPOSITE -006;CRITICAL FEATURES SUCH AS TOLERANCE, FIT, RESTRICTION OR APPLICATION.ACTION ID 45473258 |
| aircraft_location | VERTICAL STABILIZER LWR RUDDER SEAL LAND |
| material_thickness | 0.100 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-1B ACFT |
| criticality_code_justification | FEAT |
| material_document_and_classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-437-7261 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 37.210 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.750 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.100 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA L2400001;OPPOSITE -006;CRITICAL FEATURES SUCH AS TOLERANCE, FIT, RESTRICTION OR APPLICATION.ACTION ID 45473258 |
| AIRCRAFT LOCATION | VERTICAL STABILIZER LWR RUDDER SEAL LAND |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT |
No substitute or cross-reference records for this part.