68A332003-2215: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: TITANIUM ALLOY, overall_width: 3.450 INCHES NOMINAL IN, overall_length: 19.350 INCHES NOMINAL IN, special_features: ANGLE;MATERIAL 6AL-6V-2SN V, aircraft_location: FORMER-EMPENNAGE SUPPORT BEAM FS 721.830, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-421-0924, 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 ALLOY |
| overall_width | 3.450 INCHES NOMINAL IN |
| overall_length | 19.350 INCHES NOMINAL IN |
| special_features | ANGLE;MATERIAL 6AL-6V-2SN V |
| aircraft_location | FORMER-EMPENNAGE SUPPORT BEAM FS 721.830 |
| material_thickness | 0.063 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15S |
| material_document_and_classification | MMS-1203 MFR REF SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-421-0924 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS-1203 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 19.350 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.450 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | ANGLE;MATERIAL 6AL-6V-2SN V |
| AIRCRAFT LOCATION | FORMER-EMPENNAGE SUPPORT BEAM FS 721.830 |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15S |
No substitute or cross-reference records for this part.