The FRAME,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.80 INCHES NOMINAL IN, overall_length: 5.0 INCHES NOMINAL IN, special_features: HEAT TREATED TP T6, material_thickness: 0.071 INCHES NOMINAL IN, aircraft_station_number: 291.50. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1560-01-659-5650, 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_width | 2.80 INCHES NOMINAL IN |
| overall_length | 5.0 INCHES NOMINAL IN |
| special_features | HEAT TREATED TP T6 |
| material_thickness | 0.071 INCHES NOMINAL IN |
| aircraft_station_number | 291.50 |
| end_item_identification | T-38 |
| aircraft_mission_design_series | T-38 |
| material_document_and_classification | QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ANGLE |
| NSN | 1560-01-659-5650 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | HEAT TREATED TP T6 |
| MATERIAL THICKNESS | 0.071 INCHES NOMINAL IN |
| OVERALL LENGTH | 5.0 INCHES NOMINAL IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE |
| END ITEM IDENTIFICATION | T-38 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| OVERALL WIDTH | 2.80 INCHES NOMINAL IN |
| AIRCRAFT STATION NUMBER | 291.50 |
| AIRCRAFT MISSION DESIGN SERIES | T-38 |
No verified substitutes available.