160D115009-269: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, special_features: U/O -31; NHA 160D111000, aircraft_location: DOOR INSTL-LADDER, aircraft_station_number: STA238-STA254, side_for_which_designed: LEFT SIDE, aircraft_mission_design_series: A-10. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-516-8045, 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 |
| special_features | U/O -31; NHA 160D111000 |
| aircraft_location | DOOR INSTL-LADDER |
| aircraft_station_number | STA238-STA254 |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | A-10 |
| material_document_and_classification | MIL-C-7438,GRADE B,CLASS 2 (NONPERFORATED),DENSITY 4.4,CELL SIZE 3/16,FOIL SIZE .0015, ALOY 5052 MIL SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | HONEYCOMB CORE |
| NSN | 1560-01-516-8045 |
| AIRCRAFT STATION NUMBER | STA238-STA254 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-C-7438,GRADE B,CLASS 2 (NONPERFORATED),DENSITY 4.4,CELL SIZE 3/16,FOIL SIZE .0015, ALOY 5052 MIL SPEC SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | U/O -31; NHA 160D111000 |
| AIRCRAFT LOCATION | DOOR INSTL-LADDER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HONEYCOMB CORE |
| MATERIAL | ALUMINUM ALLOY 5052 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | A-10 |
No substitute or cross-reference records for this part.