3392AS1802: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, thickness: 0.063 INCHES NOMINAL IN, overall_width: 4.94 INCHES NOMINAL IN, overall_length: 7.25 INCHES NOMINAL IN, part_name_assigned_by_controlling_agency: PLATE,STRUCTURAL,AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-642-2256, 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 5052 |
| thickness | 0.063 INCHES NOMINAL IN |
| overall_width | 4.94 INCHES NOMINAL IN |
| overall_length | 7.25 INCHES NOMINAL IN |
| part_name_assigned_by_controlling_agency | PLATE,STRUCTURAL,AIRCRAFT |
| NSN | 1560-01-642-2256 |
| OVERALL LENGTH | 7.25 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.94 INCHES NOMINAL IN |
| SPECIAL FEATURES | PANEL ASSEMBLY, RIGHT SIDE;SYSTEM USED ON MH-60S FFFW;NEXT HIGHER ASSEMBLY 3392AS1888;ALL SURFACES UNLESS OTHERWISE SPECIFIED SHALL BE PREPARED, COATED, AND CLEANED AS SPECIFIED IN MIL-PRF-23377, TYPE II. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PLATE,STRUCTURAL,AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 5052 |
| THICKNESS | 0.063 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.