160D611611-35: FITTING,STRUCTURAL COMPONENT,AIR.
FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.275 INCHES NOMINAL IN, overall_length: 20.000 INCHES NOMINAL IN, special_features: AL, PLATE; DIMS. ARE STOCKSIZE MATL; NHA 160D611330; T7351, aircraft_location: CENTER SPAR, material_thickness: 2.275 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-565-4976, 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 | 2.275 INCHES NOMINAL IN |
| overall_length | 20.000 INCHES NOMINAL IN |
| special_features | AL, PLATE; DIMS. ARE STOCKSIZE MATL; NHA 160D611330; T7351 |
| aircraft_location | CENTER SPAR |
| material_thickness | 2.275 INCHES NOMINAL IN |
| aircraft_station_number | 0.00, 23.00 AND 66.00 |
| end_item_identification | A-10 ACFT |
| aircraft_mission_design_series | A-10 AIRCRAFT |
| material_document_and_classification | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FITTING, FWD |
| NSN | 1560-01-565-4976 |
| AIRCRAFT STATION NUMBER | 0.00, 23.00 AND 66.00 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 20.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.275 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 2.275 INCHES NOMINAL IN |
| SPECIAL FEATURES | AL, PLATE; DIMS. ARE STOCKSIZE MATL; NHA 160D611330; T7351 |
| AIRCRAFT LOCATION | CENTER SPAR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FITTING, FWD |
| END ITEM IDENTIFICATION | A-10 ACFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
No substitute or cross-reference records for this part.