LEVER,UPLOCK SWITCH,LANDING GEAR. Key specifications include end_item_identification: AIRCRAFT MODEL C130; AIRCRAFT, HERCULES C-130F; AIRCRAFT, HERCULES KC-130; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130), general_characteristics_item_description: STEEL,AMS5362,0.235 IN. DIA HOLE THRU 1 PLACE IN.
This product is currently in active production with full OEM support. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 3110-00-295-3347, 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.
| end_item_identification | AIRCRAFT MODEL C130; AIRCRAFT, HERCULES C-130F; AIRCRAFT, HERCULES KC-130; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130) |
| general_characteristics_item_description | STEEL,AMS5362,0.235 IN. DIA HOLE THRU 1 PLACE IN |
| NSN | 3110-00-295-3347 |
| STANDARD TOLERANCE DESIGNATION | ABEC NO.1 |
| BORE SHAPE | STRAIGHT |
| BORE DIAMETER | 0.2497 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM IN |
| MATERIAL | STEEL COMP 410 RETAINER |
| MATERIAL | STEEL COMP 440A BALL A |
| MATERIAL | STEEL COMP 440A OUTER RING A |
| STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
| MATERIAL | STEEL COMP 440A INNER RING A |
| OVERALL WIDTH | 0.1910 INCHES MINIMUM AND 0.1960 INCHES MAXIMUM IN |
| LOAD DIRECTION | RADIAL |