68A321066-2282: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 5.900 INCHES NOMINAL IN, overall_length: 15.100 INCHES NOMINAL IN, special_features: DIM ARE STOCK MATL;HEAT TREAT TO 7075-T6 PER PS15520;ANODIZE PER PS13201 TYPE 2 CLASS 1, aircraft_location: LINER,FUEL TANK NUMBER 1 SIDE, material_thickness: 0.080 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-499-5293, 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 | 5.900 INCHES NOMINAL IN |
| overall_length | 15.100 INCHES NOMINAL IN |
| special_features | DIM ARE STOCK MATL;HEAT TREAT TO 7075-T6 PER PS15520;ANODIZE PER PS13201 TYPE 2 CLASS 1 |
| aircraft_location | LINER,FUEL TANK NUMBER 1 SIDE |
| material_thickness | 0.080 INCHES NOMINAL IN |
| aircraft_station_number | FS415.000 TO FS458.800 |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | QQ-A-250/12 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | DOUBLER |
| NSN | 1560-01-499-5293 |
| AIRCRAFT STATION NUMBER | FS415.000 TO FS458.800 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 15.100 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.900 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.080 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIM ARE STOCK MATL;HEAT TREAT TO 7075-T6 PER PS15520;ANODIZE PER PS13201 TYPE 2 CLASS 1 |
| AIRCRAFT LOCATION | LINER,FUEL TANK NUMBER 1 SIDE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |
No substitute or cross-reference records for this part.