The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_length: 25.420 INCHES NOMINAL IN, aircraft_location: LWR FWD AVIONICS DOOR, end_item_identification: B1-B AIRCRAFT, aircraft_mission_design_series: B1-B, 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 1560-01-714-3523, 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 | TITANIUM ALLOY |
| overall_length | 25.420 INCHES NOMINAL IN |
| aircraft_location | LWR FWD AVIONICS DOOR |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B |
| criticality_code_justification | FEAT |
| material_document_and_classification | MIL-T-9046 MIL STD SINGLE MATERIAL RESPONSE OR AMS 4901 NATIONAL STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | RETAINER |
| NSN | 1560-01-714-3523 |
| 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; |
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL STD SINGLE MATERIAL RESPONSE OR AMS 4901 NATIONAL STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 25.420 INCHES NOMINAL IN |
| AIRCRAFT MISSION DESIGN SERIES | B1-B |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| AIRCRAFT LOCATION | LWR FWD AVIONICS DOOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER |