68R320094-2003: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, overall_width: 5.000 INCHES NOMINAL IN, overall_length: 86.000 INCHES NOMINAL IN, special_features: NHA 68S80979; 6AL04V, aircraft_location: SPEEDBRAKE STIFFENING STRAPS, material_thickness: 0.032 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-271-3459, 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 | TITANIUM ALLOY |
| overall_width | 5.000 INCHES NOMINAL IN |
| overall_length | 86.000 INCHES NOMINAL IN |
| special_features | NHA 68S80979; 6AL04V |
| aircraft_location | SPEEDBRAKE STIFFENING STRAPS |
| material_thickness | 0.032 INCHES NOMINAL IN |
| end_item_identification | F-15 |
| material_document_and_classification | MIL-T-9046 TYP 3 COMP C COND A MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-271-3459 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 TYP 3 COMP C COND A MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 86.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 5.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.032 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA 68S80979; 6AL04V |
| AIRCRAFT LOCATION | SPEEDBRAKE STIFFENING STRAPS |
| END ITEM IDENTIFICATION | F-15 |
| MATERIAL | TITANIUM ALLOY |
No substitute or cross-reference records for this part.