2006003-107: TRUNNION STRUT,LANDING SYSTEMS.
The TRUNNION STRUT,LANDING SYSTEMS is a the manufacturer industrial component. Key specifications include material: STEEL, overall_length: 47.481 INCHES MINIMUM AND 47.541 INCHES MAXIMUM IN, overall_diameter: 3.180 INCHES NOMINAL IN, surface_treatment: CADMIUM, end_item_identification: F-16 AIRCRAFT, reference_data_and_literature: T.O.4S1-109-4,FIG.1,INDEX 35. This part is cataloged in the U.S.
Government catalog under NSN 1620-01-441-6911, 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 |
| overall_length | 47.481 INCHES MINIMUM AND 47.541 INCHES MAXIMUM IN |
| overall_diameter | 3.180 INCHES NOMINAL IN |
| surface_treatment | CADMIUM |
| end_item_identification | F-16 AIRCRAFT |
| reference_data_and_literature | T.O.4S1-109-4,FIG.1,INDEX 35 |
| part_name_assigned_by_controlling_agency | TENSION STRUT ASSEMBLY |
| NSN | 1620-01-441-6911 |
| OVERALL DIAMETER | 3.180 INCHES NOMINAL IN |
| REFERENCE DATA AND LITERATURE | T.O.4S1-109-4,FIG.1,INDEX 35 |
| OVERALL LENGTH | 47.481 INCHES MINIMUM AND 47.541 INCHES MAXIMUM IN |
| SURFACE TREATMENT | CADMIUM |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TENSION STRUT ASSEMBLY |
| END ITEM IDENTIFICATION | F-16 AIRCRAFT |
| MATERIAL | STEEL |
No substitute or cross-reference records for this part.