68A116120-2005: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.500 INCHES NOMINAL IN, overall_length: 6.750 INCHES NOMINAL IN, special_features: NHA 68A110001, aircraft_location: OUTBOARD TRAILING EDGE MACHINING SKIN FILLER, material_thickness: 1.500 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-253-1202, 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 | 2.500 INCHES NOMINAL IN |
| overall_length | 6.750 INCHES NOMINAL IN |
| special_features | NHA 68A110001 |
| aircraft_location | OUTBOARD TRAILING EDGE MACHINING SKIN FILLER |
| material_thickness | 1.500 INCHES NOMINAL IN |
| end_item_identification | F-15 |
| material_document_and_classification | MMS-149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-253-1202 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS-149 T851 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 6.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 1.500 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA 68A110001 |
| AIRCRAFT LOCATION | OUTBOARD TRAILING EDGE MACHINING SKIN FILLER |
| END ITEM IDENTIFICATION | F-15 |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.