901-031-814-171: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 0.42000 INCHES NOMINAL IN, overall_length: 13.5000 INCHES NOMINAL IN, special_features: 1123 FWD FUSELAGE AVIONICS RACK;BREAK SHARP EDGES PER BAC5300;AL ALLOY WROUGHT 7075;TEMPER TY3, end_item_identification: V-22, material_document_and_classification: AMS-QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-598-8935, 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 | 0.42000 INCHES NOMINAL IN |
| overall_length | 13.5000 INCHES NOMINAL IN |
| special_features | 1123 FWD FUSELAGE AVIONICS RACK;BREAK SHARP EDGES PER BAC5300;AL ALLOY WROUGHT 7075;TEMPER TY3 |
| end_item_identification | V-22 |
| material_document_and_classification | AMS-QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | RETAINER |
| surface_treatment_document_and_classification | VF-3.49 MFR REF SINGLE TREATMENT RESPONSE |
| NSN | 1560-01-598-8935 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | VF-3.49 MFR REF SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 13.5000 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.42000 INCHES NOMINAL IN |
| SPECIAL FEATURES | 1123 FWD FUSELAGE AVIONICS RACK;BREAK SHARP EDGES PER BAC5300;AL ALLOY WROUGHT 7075;TEMPER TY3 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER |
| END ITEM IDENTIFICATION | V-22 |
| MATERIAL | ALUMINUM ALLOY 7075 |
No substitute or cross-reference records for this part.