The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024 AND TITANIUM, special_features: HARDNESS CRITICAL ITEM, aircraft_location: LOWER FORWARD AVIONICS DOOR, aircraft_station_number: YF 128.5 TO YF 174.5, end_item_identification: B1-B LANCER AIRCRAFT, aircraft_mission_design_series: B1. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-706-6061, 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 AND TITANIUM |
| special_features | HARDNESS CRITICAL ITEM |
| aircraft_location | LOWER FORWARD AVIONICS DOOR |
| aircraft_station_number | YF 128.5 TO YF 174.5 |
| end_item_identification | B1-B LANCER AIRCRAFT |
| aircraft_mission_design_series | B1 |
| criticality_code_justification | FEAT |
| relationship_to_similar_equipment | OPPOSITE OF -102 |
| material_document_and_classification | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | RETAINER |
| NSN | 1560-01-706-6061 |
| SPECIAL FEATURES | HARDNESS CRITICAL ITEM |
| AIRCRAFT MISSION DESIGN SERIES | B1 |
| END ITEM IDENTIFICATION | B1-B LANCER AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| AIRCRAFT LOCATION | LOWER FORWARD AVIONICS DOOR |
| AIRCRAFT STATION NUMBER | YF 128.5 TO YF 174.5 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | OPPOSITE OF -102 |
| MATERIAL | ALUMINUM ALLOY 2024 AND TITANIUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |