| DESIGN TYPE | MAIN LANDING GEAR |
| AIRCRAFT FOR WHICH DESIGNED | SIKORSKY HELICOPTER S-92A |
| GEAR EXTENSION AND RETRACTION METHOD | HYDRAULIC CYLINDER |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MAIN LANDING GEAR ASSEMBLY |
| PROPRIETARY CHARACTERISTICS | PACS |
| REFERENCE DATA AND LITERATURE | SIKORSKY MAINTENANCE MANUAL SA S92A-AMM-000 |
| SPECIAL FEATURES | MAINTENANCE MANUAL PUB NO. SA S92A-AMM-000 ISSUE DATE JUN 15/04 REVISED NOV 30/07;32-10-02 PAGE 213/214 APR 30/08 FIG.ITEM 201-1;UNITS PER ASSY RF;SIKORSKY SOURCE CONTROL DWG/V20517 P/N 2392-2303-001/USED ON 92250-12000-013/-014/REPLACED BY 92250-12805-043;MLG CRASH AND WEIGHT-ON WHEELS SWITCHES-REMOVAL/INSTALLATION FIGURE 201 PAGE 211 APR 30/08 |
| WHEEL QUANTITY ACCOMMODATED | 2 |