68A331072-2004A: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include height: 4.120 INCHES NOMINAL IN, material: TITANIUM ALLOY, overall_width: 4.940 INCHES NOMINAL IN, overall_length: 5.090 INCHES NOMINAL IN, special_features: REQUESTED NAME-UPSTOP,FLAP, aircraft_location: UPSTOP,FLAP. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-441-4932, 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.
| height | 4.120 INCHES NOMINAL IN |
| material | TITANIUM ALLOY |
| overall_width | 4.940 INCHES NOMINAL IN |
| overall_length | 5.090 INCHES NOMINAL IN |
| special_features | REQUESTED NAME-UPSTOP,FLAP |
| aircraft_location | UPSTOP,FLAP |
| aircraft_mission_design_series | F-15 |
| material_document_and_classification | MIL-T-9047,COMP 6 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-441-4932 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9047,COMP 6 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 5.090 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.940 INCHES NOMINAL IN |
| HEIGHT | 4.120 INCHES NOMINAL IN |
| SPECIAL FEATURES | REQUESTED NAME-UPSTOP,FLAP |
| AIRCRAFT LOCATION | UPSTOP,FLAP |
| MATERIAL | TITANIUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | F-15 |