68A240094-2021: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 4.400 INCHES NOMINAL IN, overall_length: 4.750 INCHES NOMINAL IN, special_features: NEXT HIGHER ASSEMBLY,68A240001,U/O F-15A,B,C,D,E;HEAT TREAT TO 2024-T62 PER PS15534;DIM ARE STOCK MATERIAL A, aircraft_location: RUDDER CLOSURE, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-504-7375, 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 | ALUMINUM ALLOY 2024 |
| overall_width | 4.400 INCHES NOMINAL IN |
| overall_length | 4.750 INCHES NOMINAL IN |
| special_features | NEXT HIGHER ASSEMBLY,68A240001,U/O F-15A,B,C,D,E;HEAT TREAT TO 2024-T62 PER PS15534;DIM ARE STOCK MATERIAL A |
| aircraft_location | RUDDER CLOSURE |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_mission_design_series | F-15A,B,C,D,E A |
| material_document_and_classification | QQ-A-250/5 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FORMERS-RUDDER CLOSURE |
| NSN | 1560-01-504-7375 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 COND 0 FED SPEC 1ST MATERIAL RESPONSE |
| OVERALL LENGTH | 4.750 INCHES NOMINAL IN |
| OVERALL WIDTH | 4.400 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | NEXT HIGHER ASSEMBLY,68A240001,U/O F-15A,B,C,D,E;HEAT TREAT TO 2024-T62 PER PS15534;DIM ARE STOCK MATERIAL A |
| AIRCRAFT LOCATION | RUDDER CLOSURE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FORMERS-RUDDER CLOSURE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15A,B,C,D,E A |
No substitute or cross-reference records for this part.