AT-092676-102: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: RUBBER AND GLASS FIBER, overall_width: 24.500 INCHES NOMINAL IN, overall_length: 29.380 INCHES NOMINAL IN, special_features: COMPOSITE LAMINATE, aircraft_location: CAUL PLATE TF-39 TRANSCOWL INBOARD SKIN REPAIR, material_thickness: 0.430 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-498-4615, 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 | RUBBER AND GLASS FIBER |
| overall_width | 24.500 INCHES NOMINAL IN |
| overall_length | 29.380 INCHES NOMINAL IN |
| special_features | COMPOSITE LAMINATE |
| aircraft_location | CAUL PLATE TF-39 TRANSCOWL INBOARD SKIN REPAIR |
| material_thickness | 0.430 INCHES NOMINAL IN |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | C-5 |
| NSN | 1560-01-498-4615 |
| OVERALL LENGTH | 29.380 INCHES NOMINAL IN |
| OVERALL WIDTH | 24.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.430 INCHES NOMINAL IN |
| SPECIAL FEATURES | COMPOSITE LAMINATE |
| AIRCRAFT LOCATION | CAUL PLATE TF-39 TRANSCOWL INBOARD SKIN REPAIR |
| MATERIAL | RUBBER AND GLASS FIBER |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | C-5 |
No substitute or cross-reference records for this part.