160D413003-22: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_length: 11.32 INCHES NOMINAL IN, special_features: HEAT TREAT ALUMINUM ALLOY PER MIL-H-6088 AFTER FORMING, aircraft_location: 22652, material_thickness: 0.76 INCHES NOMINAL IN, end_item_identification: A10. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-613-1834, 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 |
| overall_length | 11.32 INCHES NOMINAL IN |
| special_features | HEAT TREAT ALUMINUM ALLOY PER MIL-H-6088 AFTER FORMING |
| aircraft_location | 22652 |
| material_thickness | 0.76 INCHES NOMINAL IN |
| end_item_identification | A10 |
| aircraft_mission_design_series | A10 |
| part_name_assigned_by_controlling_agency | FORMER INSTL |
| NSN | 1560-01-613-1834 |
| OVERALL LENGTH | 11.32 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.76 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT ALUMINUM ALLOY PER MIL-H-6088 AFTER FORMING |
| AIRCRAFT LOCATION | 22652 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FORMER INSTL |
| END ITEM IDENTIFICATION | A10 |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | A10 |
No substitute or cross-reference records for this part.