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 product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5310-01-050-1523, 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 | 5310-01-050-1523 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-N-281,CL A FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| MATERIAL | NICKEL ALLOY OVERALL |
| CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
| HOLE DIAMETER | 0.226 INCHES MINIMUM AND 0.228 INCHES MAXIMUM IN |
| PERIPHERAL SHAPE STYLE | ROUND |
| OVERALL DIAMETER | 0.380 INCHES MINIMUM AND 0.382 INCHES MAXIMUM IN |
| THICKNESS | 0.0355 INCHES MINIMUM AND 0.0385 INCHES MAXIMUM IN |
| CENTER HOLE SHAPE STYLE | ROUND |