3-64202-1: FITTING,STRUCTURAL COMPONENT,AIR.
FITTING,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM, aircraft_location: AFT FUSELAGE, side_for_which_designed: BOTH SIDES, aircraft_mission_design_series: C-130B. This part is cataloged in the U.S.
Government catalog under NSN 5306-00-108-9652, 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 |
| aircraft_location | AFT FUSELAGE |
| side_for_which_designed | BOTH SIDES |
| aircraft_mission_design_series | C-130B |
| NSN | 5306-00-108-9652 |
| HEAD HEIGHT | 0.125 INCHES MINIMUM AND 0.140 INCHES MAXIMUM IN |
| FASTENER LENGTH | 1.348 INCHES MINIMUM AND 1.378 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | TY 2 CL 2,FSCM 76823 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| THREAD LENGTH | 0.374 INCHES MINIMUM AND 0.404 INCHES MAXIMUM IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5626 COND C4 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
| FIRST DIAMETER FROM HEAD | 0.186 INCHES MINIMUM AND 0.191 INCHES MAXIMUM IN |
| NOMINAL THREAD DIAMETER | 0.250 INCHES IN |
| HEAD STYLE | DISHED HEXAGON |
| THREAD DIRECTION | RIGHT-HAND |
| WIDTH BETWEEN FLATS | 0.430 INCHES MINIMUM AND 0.439 INCHES MAXIMUM IN |