3392AS1817-2: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 6061, overall_width: 3.75 INCHES NOMINAL IN, overall_length: 5.75 INCHES NOMINAL IN, part_name_assigned_by_controlling_agency: PANEL,STRUCTURAL COMPONENT,AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-642-2020, 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 6061 |
| overall_width | 3.75 INCHES NOMINAL IN |
| overall_length | 5.75 INCHES NOMINAL IN |
| part_name_assigned_by_controlling_agency | PANEL,STRUCTURAL COMPONENT,AIRCRAFT |
| NSN | 1560-01-642-2020 |
| OVERALL LENGTH | 5.75 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.75 INCHES NOMINAL IN |
| SPECIAL FEATURES | SYSTEM USED ON MH-60S FFFW;NEXT HIGHER ASSEMBLY 3392AS1818;EDGE LIGHT PANEL ASSEMBLY;PANEL SHALL BE ACCORDANCE WITH MIL-DTL-7788, CLASS-NVIS GREEN A, IN ACCORDANCE WITH MIL-L-85762, TYPE V, 5V AC. THE FRONT PANEL CURRENT SHALL NOT EXCEED 0.75 AMPS. PANEL SHALL BE BLACK COLOR NO. 37038;PANEL TEMPERATURE REQUIREMENTS SHALL BE IN ACCORDANCE WITH MIL-E-5400, PARAGRAPH 3.2.24.1 FOR CLASS 1A EQUIPMENT;TOUCH TEMPERATURE SHALL CONFORM TO MIL-HDBK-454, GUIDANCE 1, PARAGRAPH 4.4;PANEL SHALL WITH STAND EXPOSURE TO FUNGUS GROWTH IN ACCORDANCE WITH MIL-STD-810F, METHOD 508.5 IN OPERATING CONDITIONS V |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL,STRUCTURAL COMPONENT,AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 6061 |