68A323232-1003: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.870 INCHES NOMINAL IN, overall_length: 4.690 INCHES NOMINAL IN, aircraft_location: ROLLER,INBOARD AERIAL REFUELING RECEPTACLE, surface_treatment: ANODIZE, material_thickness: 1.550 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-435-6640, 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 | 1.870 INCHES NOMINAL IN |
| overall_length | 4.690 INCHES NOMINAL IN |
| aircraft_location | ROLLER,INBOARD AERIAL REFUELING RECEPTACLE |
| surface_treatment | ANODIZE |
| material_thickness | 1.550 INCHES NOMINAL IN |
| aircraft_mission_design_series | C-141 |
| material_document_and_classification | MMS 159,COND T7351 ASSN STD 1ST MATERIAL RESPONSE |
| surface_treatment_document_and_classification | PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE |
| NSN | 1560-01-435-6640 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 159,COND T7351 ASSN STD 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 4.690 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.870 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 1.550 INCHES NOMINAL IN |
| SURFACE TREATMENT | ANODIZE |
| AIRCRAFT LOCATION | ROLLER,INBOARD AERIAL REFUELING RECEPTACLE |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | C-141 |
No substitute or cross-reference records for this part.