16K2521-22: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 4.000 INCHES NOMINAL IN, overall_length: 44.000 INCHES NOMINAL IN, special_features: STIFFENER RH AFT CANOPY FRAME, aircraft_location: CANOPY, material_thickness: 0.100 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-370-3129, 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 2024 |
| overall_width | 4.000 INCHES NOMINAL IN |
| overall_length | 44.000 INCHES NOMINAL IN |
| special_features | STIFFENER RH AFT CANOPY FRAME |
| aircraft_location | CANOPY |
| material_thickness | 0.100 INCHES NOMINAL IN |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F-16D BLK 50 |
| relationship_to_similar_equipment | REPLACES 16K2521-16 |
| material_document_and_classification | QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-370-3129 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | REPLACES 16K2521-16 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4-T62 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 44.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.100 INCHES NOMINAL IN |
| SPECIAL FEATURES | STIFFENER RH AFT CANOPY FRAME |
| AIRCRAFT LOCATION | CANOPY |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-16D BLK 50 |
No substitute or cross-reference records for this part.