The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_length: 45.230 INCHES NOMINAL IN, aircraft_location: LWR FWD AVIONICS DOOR, end_item_identification: B1-B AIRCRAFT, aircraft_mission_design_series: B1-B AIRCRAFT, criticality_code_justification: FEAT. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-714-4666, 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_length | 45.230 INCHES NOMINAL IN |
| aircraft_location | LWR FWD AVIONICS DOOR |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | RETAINER |
| NSN | 1560-01-714-4666 |
| AIRCRAFT MISSION DESIGN SERIES | B1-B AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT LOCATION | LWR FWD AVIONICS DOOR |
| SPECIAL FEATURES | THIS DRAWING CONTAINS HARDNESS CRITICAL ITEMS(HCI)OR HARDNESS CRITICAL PROCESSES(HCP)ALL CHANGES TO ITEMS OR PROCESSES SO ANNOTATED ON THE DRAWING OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACTS; |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| OVERALL LENGTH | 45.230 INCHES NOMINAL IN |