The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.800 INCHES NOMINAL IN, overall_length: 14.700 INCHES NOMINAL IN, aircraft_location: TIP GEAR-STRUT DOOR WING TRAILING EDGE, material_thickness: 0.040 INCHES NOMINAL IN, end_item_identification: B-52 AIRCRAFT. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-692-5762, 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 7075 |
| overall_width | 1.800 INCHES NOMINAL IN |
| overall_length | 14.700 INCHES NOMINAL IN |
| aircraft_location | TIP GEAR-STRUT DOOR WING TRAILING EDGE |
| material_thickness | 0.040 INCHES NOMINAL IN |
| end_item_identification | B-52 AIRCRAFT |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-287 0 TEMP ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | STIFFENER |
| NSN | 1560-01-692-5762 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER |
| END ITEM IDENTIFICATION | B-52 AIRCRAFT |
| OVERALL WIDTH | 1.800 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | TIP GEAR-STRUT DOOR WING TRAILING EDGE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 0 TEMP ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| OVERALL LENGTH | 14.700 INCHES NOMINAL IN |