901-031-422-107: SPAR,AIRCRAFT.
The SPAR,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7050, overall_width: 12.50 INCHES NOMINAL IN, overall_length: 75.20 INCHES NOMINAL IN, special_features: COLOR 16081 ENGINE GREY, material_thickness: 2.0 INCHES NOMINAL IN, aircraft_station_number: 1.1.1.4 AFT FUSELAGE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-615-2772, 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 7050 |
| overall_width | 12.50 INCHES NOMINAL IN |
| overall_length | 75.20 INCHES NOMINAL IN |
| special_features | COLOR 16081 ENGINE GREY |
| material_thickness | 2.0 INCHES NOMINAL IN |
| aircraft_station_number | 1.1.1.4 AFT FUSELAGE |
| end_item_identification | V-22 |
| aircraft_mission_design_series | V22 |
| part_name_assigned_by_controlling_agency | BEAM, SIDE RAMP |
| NSN | 1560-01-615-2772 |
| AIRCRAFT STATION NUMBER | 1.1.1.4 AFT FUSELAGE |
| OVERALL LENGTH | 75.20 INCHES NOMINAL IN |
| OVERALL WIDTH | 12.50 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 2.0 INCHES NOMINAL IN |
| SPECIAL FEATURES | COLOR 16081 ENGINE GREY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BEAM, SIDE RAMP |
| END ITEM IDENTIFICATION | V-22 |
| MATERIAL | ALUMINUM ALLOY 7050 |
| AIRCRAFT MISSION DESIGN SERIES | V22 |
No substitute or cross-reference records for this part.