The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM, overall_width: 4.000 INCHES NOMINAL IN, overall_length: 5.000 INCHES NOMINAL IN, special_features: MYLAR MASTERS ARE KEPT IN BLDG 472;PHOTO LAB CODE 97205., aircraft_location: NACELLE FIREWALL STA 126, material_thickness: 0.020 INCHES NOMINAL IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5360-01-221-3221, 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 | TITANIUM |
| overall_width | 4.000 INCHES NOMINAL IN |
| overall_length | 5.000 INCHES NOMINAL IN |
| special_features | MYLAR MASTERS ARE KEPT IN BLDG 472;PHOTO LAB CODE 97205. |
| aircraft_location | NACELLE FIREWALL STA 126 |
| material_thickness | 0.020 INCHES NOMINAL IN |
| aircraft_station_number | 126 |
| end_item_identification | C-2A REPROCURED; DOUBLERS REPAIR, NACELLE FIREWALL STA 126 A |
| aircraft_mission_design_series | C-2A REPROCURED A |
| relationship_to_similar_equipment | DOUBLERS P/N 72023-13 AND 72023-15, CAGE CODE 91145. |
| material_document_and_classification | MIL-T-9046.MIL-T-9046CLASS 6 MIL SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | INAVY:DOUBLER |
| NSN | 5360-01-221-3221 |
| END LENGTH | 0.380 INCHES NOMINAL BOTH ENDS IN |
| INSIDE DIAMETER | 0.124 INCHES NOMINAL IN |
| COIL HELIX DIRECTION | RIGHT-HAND OR LEFT-HAND |
| END STYLE | ONE HOOK END BOTH ENDS |
| STYLE DESIGNATOR | SINGLE TORSION LEFT HAND |
| END ANGULAR RELATIONSHIP | ENDS ANGLED ONE TO OTHER |
| SPRING FREE LENGTH | 0.400 INCHES MAXIMUM IN |
| SPRING FREE OUTSIDE DIAMETER | 0.160 INCHES NOMINAL IN |
| MATERIAL | STEEL OVERALL |