The TIRE,PNEUMATIC,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: COPPER ALLOY 360 OR COPPER ALLOY 345 OVERALL, leg_length: 0.547 INCHES NOMINAL SECOND END IN, seat_angle: 42.0 DEGREES FIRST END, thread_class: 2B FIRST END, connection_type: THREADED INTERNAL TUBE FIRST END, connection_style: INVERTED FLARE (TUBE) FIRST END. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2620-00-060-7013, 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 | COPPER ALLOY 360 OR COPPER ALLOY 345 OVERALL |
| leg_length | 0.547 INCHES NOMINAL SECOND END IN |
| seat_angle | 42.0 DEGREES FIRST END |
| thread_class | 2B FIRST END |
| connection_type | THREADED INTERNAL TUBE FIRST END |
| connection_style | INVERTED FLARE (TUBE) FIRST END |
| nominal_thread_size | 0.625 INCHES FIRST END IN |
| thread_series_designator | UNF SECOND END |
| nondefinitive_spec/std_data | 7B FIGURE |
| specification/standard_data | 81343-J512 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| nominal_outside_diameter_tube_accommodated | 0.375 INCHES SECOND END IN |
| NSN | 2620-00-060-7013 |
| SERVICE TYPE | AIRCRAFT HELICOPTER |
| END ITEM IDENTIFICATION | U-1/O-2/CH-43/HH-60H/MH-60R/SH-60,MLG/NLG/TLG |
| TIRE AND SIZE DESIGNATION | 6.00-6 NUMERIC |
| TREAD PATTERN | GROOVED |
| TIRE PLY ARRANGEMENT | BIAS |
| TIRE LOAD MAXIMUM CAPACITY | 3920.0 POUNDS STATIC LOAD LBS |
| TIRE AIR RETENTION METHOD | TUBELESS TYPE |
| SPECIFICATION/STANDARD DATA | 81349-MIL-T-5041 GOVERNMENT SPECIFICATION |
| MATERIAL | PLASTIC POLYAMIDE NYLON |
| SPECIAL FEATURES | RATED SPEED 139 KNOTS PER HR |