2006699-5: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: STEEL CORROSION RESISTING, overall_width: 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN, overall_length: 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN, aircraft_location: DOOR ASSEMBLY, material_thickness: 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN, end_item_identification: AIRCRAFT, HORNET F/A-18. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-490-4552, 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 | STEEL CORROSION RESISTING |
| hole_quantity | 2 |
| overall_width | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN |
| overall_length | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| aircraft_location | DOOR ASSEMBLY |
| material_thickness | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN |
| end_item_identification | AIRCRAFT, HORNET F/A-18 |
| aircraft_mission_design_series | C-135 |
| part_name_assigned_by_controlling_agency | CLAMP |
| NSN | 1560-01-490-4552 |
| OVERALL LENGTH | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM IN |
| AIRCRAFT LOCATION | DOOR ASSEMBLY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CLAMP |
| END ITEM IDENTIFICATION | AIRCRAFT, HORNET F/A-18 |
| MATERIAL | STEEL CORROSION RESISTING |
| HOLE QUANTITY | 2 |
| AIRCRAFT MISSION DESIGN SERIES | C-135 |
No substitute or cross-reference records for this part.