L3005007-013: DOOR,AIRCRAFT.
The DOOR,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, thickness: 0.750 INCHES NOMINAL IN, overall_width: 7.500 INCHES NOMINAL IN, overall_length: 9.250 INCHES NOMINAL IN, aircraft_location: FUSELAGE STUB SKIN, end_item_identification: B1-B AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-719-4923, 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 |
| thickness | 0.750 INCHES NOMINAL IN |
| overall_width | 7.500 INCHES NOMINAL IN |
| overall_length | 9.250 INCHES NOMINAL IN |
| aircraft_location | FUSELAGE STUB SKIN |
| end_item_identification | B1-B AIRCRAFT |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | B1-B |
| material_document_and_classification | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | DOOR |
| NSN | 1560-01-719-4923 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 9.250 INCHES NOMINAL IN |
| OVERALL WIDTH | 7.500 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | FUSELAGE STUB SKIN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOOR |
| END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | B1-B |
| THICKNESS | 0.750 INCHES NOMINAL IN |