160D115028-133: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 28.000 INCHES NOMINAL IN, special_features: ALCLAD SH; HEAT TREAT TO -T6 PER MIL-H-6088; 7075-0, aircraft_location: DOOR INSTALLATION-GUN ACCESS, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-577-0311, 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 | 6.000 INCHES NOMINAL IN |
| overall_length | 28.000 INCHES NOMINAL IN |
| special_features | ALCLAD SH; HEAT TREAT TO -T6 PER MIL-H-6088; 7075-0 |
| aircraft_location | DOOR INSTALLATION-GUN ACCESS |
| material_thickness | 0.050 INCHES NOMINAL IN |
| aircraft_station_number | FS204-227 |
| end_item_identification | A-10 ACFT |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ZEE |
| NSN | 1560-01-577-0311 |
| AIRCRAFT STATION NUMBER | FS204-227 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 28.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | ALCLAD SH; HEAT TREAT TO -T6 PER MIL-H-6088; 7075-0 |
| AIRCRAFT LOCATION | DOOR INSTALLATION-GUN ACCESS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ZEE |
| END ITEM IDENTIFICATION | A-10 ACFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
No substitute or cross-reference records for this part.