7020-52-400-4047: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, aircraft_location: FAIRING INSTL-MAIN ROTOR PYLON, material_thickness: 0.040 INCHES NOMINAL IN, aircraft_station_number: 485 TO 525, end_item_identification: SH-60B;FAIRING INSTL-STA 485-525 MAIN ROTOR PYLON, aircraft_mission_design_series: SH-60B. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-274-4595, 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 7075 |
| aircraft_location | FAIRING INSTL-MAIN ROTOR PYLON |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | 485 TO 525 |
| end_item_identification | SH-60B;FAIRING INSTL-STA 485-525 MAIN ROTOR PYLON |
| aircraft_mission_design_series | SH-60B |
| material_document_and_classification | QQ-A-250/18 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | INAVY-STRAP ASSEMBLY |
| NSN | 1560-01-274-4595 |
| AIRCRAFT STATION NUMBER | 485 TO 525 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/18 ASSN STD SINGLE MATERIAL RESPONSE |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | FAIRING INSTL-MAIN ROTOR PYLON |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY-STRAP ASSEMBLY |
| END ITEM IDENTIFICATION | SH-60B;FAIRING INSTL-STA 485-525 MAIN ROTOR PYLON |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | SH-60B |
No substitute or cross-reference records for this part.