123CS10141-13: SKIN,AIRCRAFT.
The SKIN,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, thickness: 0.100 INCHES NOMINAL IN, overall_width: 17.000 INCHES NOMINAL IN, overall_length: 23.000 INCHES NOMINAL IN, aircraft_location: DOOR ASSY-CONT. SURF STAB UPPER SKIN, STA 54 & 148, aircraft_station_number: 54 AND 148.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-531-7516, 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 |
| thickness | 0.100 INCHES NOMINAL IN |
| overall_width | 17.000 INCHES NOMINAL IN |
| overall_length | 23.000 INCHES NOMINAL IN |
| aircraft_location | DOOR ASSY-CONT. SURF STAB UPPER SKIN, STA 54 & 148 |
| aircraft_station_number | 54 AND 148 |
| end_item_identification | E-2C; DOOR ASSY-INSTL. CONT. SUR. STAB. UPPER SKIN, STA 54 AND 148 |
| aircraft_mission_design_series | E-2C |
| material_document_and_classification | QQ-A-250/13 ASSN STD ALL MATERIAL RESPONSES |
| part_name_assigned_by_controlling_agency | INAVY:SKIN ASSEMBLY |
| NSN | 1560-01-531-7516 |
| AIRCRAFT STATION NUMBER | 54 AND 148 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 ASSN STD ALL MATERIAL RESPONSES |
| OVERALL LENGTH | 23.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 17.000 INCHES NOMINAL IN |
| AIRCRAFT LOCATION | DOOR ASSY-CONT. SURF STAB UPPER SKIN, STA 54 & 148 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY:SKIN ASSEMBLY |
| END ITEM IDENTIFICATION | E-2C; DOOR ASSY-INSTL. CONT. SUR. STAB. UPPER SKIN, STA 54 AND 148 |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | E-2C |
| THICKNESS | 0.100 INCHES NOMINAL IN |