39-4407-4: STIFFENER,AIRCRAFT.
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: 13.00 INCHES NOMINAL IN, special_features: 2 HOLES DIAMETER 0.096 INCHES IN, aircraft_location: TIP GEAR-STRUT DOOR WING TRAILING EDGE, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-692-5528, 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 | 13.00 INCHES NOMINAL IN |
| special_features | 2 HOLES DIAMETER 0.096 INCHES IN |
| aircraft_location | TIP GEAR-STRUT DOOR WING TRAILING EDGE |
| material_thickness | 0.063 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 | 1560-01-692-5528 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 0 TEMP ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 13.00 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | 2 HOLES DIAMETER 0.096 INCHES IN |
| AIRCRAFT LOCATION | TIP GEAR-STRUT DOOR WING TRAILING EDGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER |
| END ITEM IDENTIFICATION | B-52 AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |