时间:2014-11-09 12:30来源:FAA 作者:直升机翻译 点击:次
To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. Altimeter Angle of attack (AOA) Angle of incidence Anti-icing systems Antitorque drive systems antitorque pedals Antitorque system Fenestron NOTAR. Antitorque system failure AOA Approach and landing Approaches Astigmatism Atmospheric illusions Autopilot Autorotation Autorotation (forward flight) Autorotation with turns B Basic empty weight Bearingless rotor system Belt drive clutch Bernoulli's Principle Blade span C Carburetor ice Center of gravity Center of pressure Centrifugal clutch CG aft of aft limit Chord Chord line Clutch Coaxial rotors Cockpit lights Collective Collective pitch control Collision avoidance at night Combustion chamber Common errors of attitude instrument flying emphasis omission Compressor Coning Control inputs antitorque pedals collective cyclic throttle Coriolis Effect (Law of Conservation of Angular Momentum) Critical conditions Crosswind considerations during takeoffs D d’Amécourt, Gustave de Ponton Decision making models Decision-making mrocess Density altitude Determining empty weight Dissymmetry of lift Downwash Drag induced drag parasite drag profile drag total drag Dynamic rollover E Effective translational lift (ETL) Effect of weight versus density altitude Elastomeric bearings Electrical systems Emergency Equipment and survival gear Engine fuel control system Engines reciprocating engine turbine engine Engine start and rotor engagement En route procedures Environmental dystems F Fenestron Flicker vertigo Flight Instruments Flightpath velocity Four fundamentals Freewheeling unit Fuel supply system Fundamental skills of attitude instrument flying Fuselage G General Aviation Manufacturers Association (GAMA) Glass cockpit or advanced avionics aircraft Go-around Governor/correlator Ground lighting illusions Ground reference maneuvers common errors during ground reference maneuvers rectangular course s-turns turns around a point Ground resonance Gyroscopic precession H Heading control Height/velocity diagram Helicopter Helicopter control and performance Helicopter night VFR operations High and low density altitude conditions Hovering autorotation Hovering flight Hovering—forward flight Hovering performance Hovering—sideward flight Hovering turn Hover taxi Hub Humidity Hydraulics I Illusions leading to landing errors Induced flow Induced flow (downwash) In-ground effect Instrument check Intermeshing rotors K Kaman, Charles H L Landing—stuck left pedal Landing—stuck neutral or right pedal Leading edge Lift Loading chart method Low-G conditions and mast bumping Low reconnaissance Low rotor RPM and blade stall LTE at altitude M Main rotor disk interference (285–315°) Main rotor system Main rotor transmission Maximum gross weight Maximum performance takeoff Mean camber line Medium and high frequency vibrations Minimum equipment lists (MELs) and operations with inoperative equipment Moisture Multi-engine emergency operations Myopia N Newton’s Third Law of Motion Night flight |