STRUCTURAL SECTION,SPECIAL SHAPE. Key specifications include length: 9.000 FEET NOMINAL FT, material: ALUMINUM ALLOY 6063, usage_design: AIRCRAFT, heat_treatment: T-6 SOLUTION HEAT TREATED, fabrication_method: EXTRUDED, end_item_identification: C-141 AIRCRAFT. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 9540-00-395-6411, 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.
| length | 9.000 FEET NOMINAL FT |
| material | ALUMINUM ALLOY 6063 |
| usage_design | AIRCRAFT |
| heat_treatment | T-6 SOLUTION HEAT TREATED |
| fabrication_method | EXTRUDED |
| end_item_identification | C-141 AIRCRAFT |
| weight_per_unit_measure | 0.089 POUNDS PER LINEAR FOOT LBS |
| nondefinitive_spec/std_data | T6 TEMPER |
| material_document_and_classification | AMS-QQ-A-200/9 FED SPEC SINGLE MATERIAL RESPONSE |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY MATERIAL TEMPER AND LENGTH REQUIREMENTS |
| NSN | 9540-00-395-6411 |
| LENGTH | 9.000 FEET NOMINAL FT |
| MATERIAL | ALUMINUM ALLOY 6063 |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| END ITEM IDENTIFICATION | C-141 AIRCRAFT |
| WEIGHT PER UNIT MEASURE | 0.089 POUNDS PER LINEAR FOOT LBS |
| NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/9 FED SPEC SINGLE MATERIAL RESPONSE |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY MATERIAL TEMPER AND LENGTH REQUIREMENTS |
| FABRICATION METHOD | EXTRUDED |
| USAGE DESIGN | AIRCRAFT |