| AIRPLANE TYPE TIRE SIZE ACCOMMODATED | 12 TO 34IN RIM DIA |
| DEVELOPED HYDRAULIC PRESSURE | 25000.0 POUNDS PER SQUARE INCH |
| ENTRY DATE | 03-11-06 |
| FUNCTIONAL CLASSIFICATION | GG-5.1 |
| FUNCTIONAL DESCRIPTION | AIR DRIVEN HYDRAULIC PUMP AIRCRAFT TIRE BEAD BREAKER FOR 15-60IN OD X 12-26IN WIDE ON 12-34IN DIA RIM |
| HYDRAULIC UNIT DRIVE TYPE | COMPRESSED AIR |
| OPERATION METHOD | POWERED |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BEAD BREAKER, PNEUMATIC TIRE |
| MAXIMUM AUTOMOTIVE TYPE TIRE SIZE ACCOMMODATED | 26IN TIRE WIDTH X 34IN RIM DIA |
| MINIMUM AUTOMOTIVE TYPE TIRE SIZE ACCOMMODATED | 12IN TIRE WIDTH X 12IN RIM DIA |
| REFERENCE DATA AND LITERATURE | WARNER-ROBINS ALC PD03WR/LEEE |
| RELATIONSHIP TO SIMILAR EQUIPMENT | TYPE 2 IS EXPLOSION PROOF MOTOR DRIVEN |
| SPECIAL FEATURES | NOT TO EXCEED 2000 LB WEIGHT; SPIDER PLATE ASSEMBLY OR UNIVERSAL SPIDER ASSEMBLY TYPE; MIL-PRF-5606 HYDRAULIC FLUID; ONE PERSON OPERATION; BOTH BEADS OF TIRE BROKEN IN ONE-STROKE WITH NO DESTRUCTION OF TIRE |
| WORKING MECHANISM PRESSURE SUPPLY METHOD | HYDRAULIC RAM |