123BH10004-5: FLOOR,AIRCRAFT.
The FLOOR,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, thickness: 0.492 INCHES NOMINAL IN, overall_width: 29.000 INCHES NOMINAL IN, overall_length: 21.000 INCHES NOMINAL IN, surface_treatment: ALODIZE AND PAINT EPOXY, fabrication_method: HONEYCOMB. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-461-8994, 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 |
| thickness | 0.492 INCHES NOMINAL IN |
| overall_width | 29.000 INCHES NOMINAL IN |
| overall_length | 21.000 INCHES NOMINAL IN |
| surface_treatment | ALODIZE AND PAINT EPOXY |
| fabrication_method | HONEYCOMB |
| aircraft_station_number | 555 |
| end_item_identification | E-2 |
| aircraft_mission_design_series | FUSELAGE,MID SECTION |
| material_document_and_classification | ALUMINUM ALLOY 7075 FED SPEC SINGLE MATERIAL RESPONSE |
| surface_treatment_document_and_classification | QQ-A-250/13 FED SPEC SINGLE TREATMENT RESPONSE |
| NSN | 1560-01-461-8994 |
| AIRCRAFT STATION NUMBER | 555 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | ALUMINUM ALLOY 7075 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 21.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 29.000 INCHES NOMINAL IN |
| SURFACE TREATMENT | ALODIZE AND PAINT EPOXY |
| END ITEM IDENTIFICATION | E-2 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| FABRICATION METHOD | HONEYCOMB |
| AIRCRAFT MISSION DESIGN SERIES | FUSELAGE,MID SECTION |
No substitute or cross-reference records for this part.