2-11651-2: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include overall_width: 1.76 INCHES NOMINAL IN, special_features: NHA:2-11636, SUPPORT IS 92 DEGREES BEND, aircraft_location: TRACK,ENGINE FUSALAGE, material_thickness: 0.160 INCHES NOMINAL IN, aircraft_station_number: STA 479.50, end_item_identification: T-38 AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-673-1577, 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.
| overall_width | 1.76 INCHES NOMINAL IN |
| special_features | NHA:2-11636, SUPPORT IS 92 DEGREES BEND |
| aircraft_location | TRACK,ENGINE FUSALAGE |
| material_thickness | 0.160 INCHES NOMINAL IN |
| aircraft_station_number | STA 479.50 |
| end_item_identification | T-38 AIRCRAFT |
| aircraft_mission_design_series | T-38 AIRCRAFT |
| part_name_assigned_by_controlling_agency | SUPPORT ENGINE TRACK |
| NSN | 1560-01-673-1577 |
| AIRCRAFT STATION NUMBER | STA 479.50 |
| OVERALL WIDTH | 1.76 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.160 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA:2-11636, SUPPORT IS 92 DEGREES BEND |
| AIRCRAFT LOCATION | TRACK,ENGINE FUSALAGE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT ENGINE TRACK |
| END ITEM IDENTIFICATION | T-38 AIRCRAFT |
| AIRCRAFT MISSION DESIGN SERIES | T-38 AIRCRAFT |
No substitute or cross-reference records for this part.