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The minimum control speed (V MC) of a multi-engine aircraft (specifically an airplane) is a V-speed that specifies the calibrated airspeed below which directional or lateral control of the aircraft can no longer be maintained, after the failure of one or more engines.
V 1 is the critical engine failure recognition speed or takeoff decision speed. It is the speed above which the takeoff will continue even if an engine fails or another problem occurs, such as a blown tire. [ 9 ]
The ASI in multi-engine aircraft includes two additional radial markings, one red and one blue, associated with potential engine failure. The radial red line near the bottom of green arc indicates V mc , the minimum indicated airspeed at which the aircraft can be controlled with the critical engine inoperative.
VMC visual meteorological conditions: VMC minimum control speed with critical engine out VNAV vertical navigation Or: V/NAV VNC VFR navigation chart VNE Never exceed speed: VNO Maximum structural cruising speed VNR VHF navigation receiver VOR VHF omni-directional range: VOR/DME VOR with Distance measuring equipment: VOR/MB VOR marker beacon VORTAC
V MC, the minimum control speed(s) of a multi-engine aircraft; Visual meteorological conditions, an aviation flight category in which visual flight rules flight is permitted; Vaughan Metropolitan Centre station, a Toronto Transit Commission subway station, Canada; Vevey–Montreux–Chillon–Villeneuve tramway, a former tramway in the Swiss ...
Unlike the pushrod systems used by DaimlerChrysler's Multi-Displacement System and General Motors' Active Fuel Management, Honda's VCM uses overhead cams. A solenoid unlocks the cam followers on one bank from their respective rockers, so the cam follower floats freely while the valve springs keep the valves closed. The system operates through ...