L2300225-003: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, special_features: HT TR PER ST0111LA0009,TEMPER T62, aircraft_location: VERTICAL STAB TIP, material_thickness: 0.175 INCHES NOMINAL IN, aircraft_station_number: ZVS184.762 TO ZVS199.762 AND YVS238.283 TO YVS292.723, end_item_identification: B-1B. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-155-4732, 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 |
| special_features | HT TR PER ST0111LA0009,TEMPER T62 |
| aircraft_location | VERTICAL STAB TIP |
| material_thickness | 0.175 INCHES NOMINAL IN |
| aircraft_station_number | ZVS184.762 TO ZVS199.762 AND YVS238.283 TO YVS292.723 |
| end_item_identification | B-1B |
| NSN | 1560-01-155-4732 |
| AIRCRAFT STATION NUMBER | ZVS184.762 TO ZVS199.762 AND YVS238.283 TO YVS292.723 |
| MATERIAL THICKNESS | 0.175 INCHES NOMINAL IN |
| SPECIAL FEATURES | HT TR PER ST0111LA0009,TEMPER T62 |
| AIRCRAFT LOCATION | VERTICAL STAB TIP |
| END ITEM IDENTIFICATION | B-1B |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.