68A240001-2047: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 4.000 INCHES NOMINAL IN, overall_length: 7.000 INCHES NOMINAL IN, special_features: ANODIZE PER PS13201 TYPE2 CLASS 1;HEAT TREAT TO COND T62 PER PG15534, aircraft_location: RUDDER ASSEMBLY, aircraft_mission_design_series: F-15. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-504-5256, 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 2024 |
| overall_width | 4.000 INCHES NOMINAL IN |
| overall_length | 7.000 INCHES NOMINAL IN |
| special_features | ANODIZE PER PS13201 TYPE2 CLASS 1;HEAT TREAT TO COND T62 PER PG15534 |
| aircraft_location | RUDDER ASSEMBLY |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/5 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | RUDDER ASSY-VERTICAL STABLIZER |
| NSN | 1560-01-504-5256 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 7.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | ANODIZE PER PS13201 TYPE2 CLASS 1;HEAT TREAT TO COND T62 PER PG15534 |
| AIRCRAFT LOCATION | RUDDER ASSEMBLY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RUDDER ASSY-VERTICAL STABLIZER |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.