114S3902-432: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL CORROSION RESISTING, overall_width: 17.500 INCHES NOMINAL IN, overall_length: 24.000 INCHES NOMINAL IN, aircraft_location: PYLON INSTALLATION, ENGINE FAIRING, material_thickness: 0.020 INCHES NOMINAL IN, aircraft_mission_design_series: CH-47D. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-471-4986, 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 CORROSION RESISTING |
| overall_width | 17.500 INCHES NOMINAL IN |
| overall_length | 24.000 INCHES NOMINAL IN |
| special_features | MATERIAL: CRES COMP 302 OR 304, ANNEALED SURFACE COND 2D, MIL-S-5059 UTS 75000 OR CRES COMP 3212 ANNEALED SURFACE COND 2DM MIL-S-6721 |
| aircraft_location | PYLON INSTALLATION, ENGINE FAIRING |
| material_thickness | 0.020 INCHES NOMINAL IN |
| aircraft_mission_design_series | CH-47D |
| NSN | 1560-01-471-4986 |
| OVERALL LENGTH | 24.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 17.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.020 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATERIAL: CRES COMP 302 OR 304, ANNEALED SURFACE COND 2D, MIL-S-5059 UTS 75000 OR CRES COMP 3212 ANNEALED SURFACE COND 2DM MIL-S-6721 |
| AIRCRAFT LOCATION | PYLON INSTALLATION, ENGINE FAIRING |
| MATERIAL | STEEL CORROSION RESISTING |
| AIRCRAFT MISSION DESIGN SERIES | CH-47D |
No substitute or cross-reference records for this part.