907004: 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 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 |
| OVERALL DIAMETER | 0.380 INCHES MINIMUM AND 0.382 INCHES MAXIMUM IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-N-281,CL A FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
| PERIPHERAL SHAPE STYLE | ROUND |
| MATERIAL | NICKEL ALLOY OVERALL |
| CENTER HOLE SHAPE STYLE | ROUND |
| HOLE DIAMETER | 0.226 INCHES MINIMUM AND 0.228 INCHES MAXIMUM IN |
| THICKNESS | 0.0355 INCHES MINIMUM AND 0.0385 INCHES MAXIMUM IN |
No substitute or cross-reference records for this part.