5306PL1495364: BOLT,SHOULDER.
The BOLT,SHOULDER is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY OVERALL, head_style: ROUND W/WRENCH FLATS CHAMFERED, head_height: 0.060 INCHES MINIMUM AND 0.070 INCHES MAXIMUM IN, thread_class: 3A A, head_diameter: 0.730 INCHES MINIMUM AND 0.737 INCHES MAXIMUM IN, thread_length: 1.167 INCHES MINIMUM AND 1.270 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 5306-00-425-8474, 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 | TITANIUM ALLOY OVERALL |
| head_style | ROUND W/WRENCH FLATS CHAMFERED |
| head_height | 0.060 INCHES MINIMUM AND 0.070 INCHES MAXIMUM IN |
| thread_class | 3A A |
| head_diameter | 0.730 INCHES MINIMUM AND 0.737 INCHES MAXIMUM IN |
| thread_length | 1.167 INCHES MINIMUM AND 1.270 INCHES MAXIMUM IN |
| shoulder_shape | ROUND FIRST SHOULDER |
| fastener_length | 1.300 INCHES MINIMUM AND 1.320 INCHES MAXIMUM IN |
| shoulder_length | 0.050 INCHES MINIMUM AND 0.070 INCHES MAXIMUM FIRST SHOULDER IN |
| special_features | TWO HOLES DRILLED THROUGH HEAD 0.098 IN. MIN 0.103 IN. MAX DIA,0.520 IN. C TO C BETWEEN BOLT HOLES IN |
| thread_direction | RIGHT-HAND |
| shoulder_diameter | 0.248 INCHES MINIMUM AND 0.250 INCHES MAXIMUM FIRST SHOULDER IN |
| NSN | 5306-00-425-8474 |
| HEAD HEIGHT | 0.060 INCHES MINIMUM AND 0.070 INCHES MAXIMUM IN |
| FASTENER LENGTH | 1.300 INCHES MINIMUM AND 1.320 INCHES MAXIMUM IN |
| SHOULDER LENGTH | 0.050 INCHES MINIMUM AND 0.070 INCHES MAXIMUM FIRST SHOULDER IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | PWA 37 FSCM 77445 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| SHOULDER DIAMETER | 0.248 INCHES MINIMUM AND 0.250 INCHES MAXIMUM FIRST SHOULDER IN |
| THREAD LENGTH | 1.167 INCHES MINIMUM AND 1.270 INCHES MAXIMUM IN |
| SHOULDER SHAPE | ROUND FIRST SHOULDER |
| SUPPLEMENTARY FEATURES | BOLT FAILURE COULD CAUSE ENGINE OR AIRCRAFT FAILURE |
| CRITICALITY CODE JUSTIFICATION | SUPP |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
No substitute or cross-reference records for this part.