211309-2: 211309-2.
The 211309-2 is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, special_features: 51108429 EXTR; UPPER LEFT;NEXT ASSY 2-11300, aircraft_location: FUSELAGE STRUCTURE, aircraft_station_number: FS325, end_item_identification: T-38 ACFT, side_for_which_designed: LEFT SIDE. This part is cataloged in the U.S.
Government catalog under NSN 5999-01-388-6532, 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 |
| special_features | 51108429 EXTR; UPPER LEFT;NEXT ASSY 2-11300 |
| aircraft_location | FUSELAGE STRUCTURE |
| aircraft_station_number | FS325 |
| end_item_identification | T-38 ACFT |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | T-38 ACFT |
| material_document_and_classification | QQ-A-277-T6 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | CAP-BULKHEAD UPR LEFT |
| NSN | 5999-01-388-6532 |
| PIN DIAMETER | 0.029 INCHES MINIMUM AND 0.031 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-G-45204, TYPE I, CLASS 1 MIL SPEC 1ST TREATMENT RESPONSE AND QQ-N-290 FED SPEC 2ND TREATMENT RESPONSE BODY AND CONTACT |
| OVERALL DIAMETER | 0.072 INCHES MINIMUM AND 0.075 INCHES MAXIMUM IN |
| PRECIOUS MATERIAL | GOLD |
| MOUNTING METHOD | FORCE FIT |
| STYLE DESIGNATOR | PIN CONTACT |
| PRECIOUS MATERIAL AND WEIGHT | 0.005 GOLD GRAINS, TROY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-B-750 FED SPEC SINGLE MATERIAL RESPONSE BODY AND CONTACT |
| OVERALL LENGTH | 0.828 INCHES NOMINAL IN |
| SURFACE TREATMENT | GOLD AND NICKEL BODY AND CONTACT |
No substitute or cross-reference records for this part.