68A316077-2001: FITTING,STRUCTURAL COMPONENT,AIR.
FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.000 INCHES NOMINAL IN, overall_length: 3.500 INCHES NOMINAL IN, special_features: COND T7351;OPPOSTIE -2002;NHA 68A316085, aircraft_location: FWD FUSELAGE, material_thickness: 0.750 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-588-7219, 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 |
| overall_width | 2.000 INCHES NOMINAL IN |
| overall_length | 3.500 INCHES NOMINAL IN |
| special_features | COND T7351;OPPOSTIE -2002;NHA 68A316085 |
| aircraft_location | FWD FUSELAGE |
| material_thickness | 0.750 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-16 ACFT |
| material_document_and_classification | MMS 159 MIL SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | CANOPY STOP FITTING |
| NSN | 1560-01-588-7219 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS 159 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.750 INCHES NOMINAL IN |
| SPECIAL FEATURES | COND T7351;OPPOSTIE -2002;NHA 68A316085 |
| AIRCRAFT LOCATION | FWD FUSELAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CANOPY STOP FITTING |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F-16 ACFT |
No substitute or cross-reference records for this part.