5-96280-23: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 7.200 INCHES NOMINAL IN, special_features: HEAT TREAT T6; MAKE FROM AND10135-1003, aircraft_location: FRONT SPAR ELEVATOR, end_item_identification: KC-135, aircraft_mission_design_series: KC-135. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-545-9906, 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 7075 |
| overall_length | 7.200 INCHES NOMINAL IN |
| special_features | HEAT TREAT T6; MAKE FROM AND10135-1003 |
| aircraft_location | FRONT SPAR ELEVATOR |
| end_item_identification | KC-135 |
| aircraft_mission_design_series | KC-135 |
| material_document_and_classification | QQ-A-283 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | STIFFENER |
| NSN | 1560-01-545-9906 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-283 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.200 INCHES NOMINAL IN |
| SPECIAL FEATURES | HEAT TREAT T6; MAKE FROM AND10135-1003 |
| AIRCRAFT LOCATION | FRONT SPAR ELEVATOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER |
| END ITEM IDENTIFICATION | KC-135 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | KC-135 |
No substitute or cross-reference records for this part.