vi WWW.GOFLY.ONLINE Y ONLI NE FLI GHT SCHOOL CONTENTS Stall warning device................................................................................................................................................... 27 Stick or control column position ................................................................................................................................ 27 Stall buffet.................................................................................................................................................................. 27 Stall recovery procedure............................................................................................................................................ 27 The factors which will result in stall speed changes.................................................................................................. 27 Flaps.......................................................................................................................................................................... 28 Power......................................................................................................................................................................... 28 Weight........................................................................................................................................................................ 28 Wing shear, gusts and thermals. ............................................................................................................................... 28 Ice and frost............................................................................................................................................................... 29 Rolling G loading. ...................................................................................................................................................... 29 Windrop Stall and Spin recovery. .............................................................................................................................. 29 Spin recovery technique............................................................................................................................................ 31 Taxi, Take-Off, And Landing........................................................................................................................31 Nose wheel aircraft.................................................................................................................................................... 31 Tail wheel aircraft....................................................................................................................................................... 31 Propeller torque......................................................................................................................................................... 31 Slipstream effect........................................................................................................................................................ 33 Gyroscopic effect....................................................................................................................................................... 33 Ground effect............................................................................................................................................................. 33 Wheelbarrowing......................................................................................................................................................... 33 Prevent or recover from wheelbarrowing................................................................................................................... 33 Pilot induced oscillations............................................................................................................................................ 33 Overcontrol................................................................................................................................................................ 33 Control Sensitivity...................................................................................................................................................... 35 Inexperience or Lack of Training................................................................................................................................ 35 Prevent or recover from pilot induced oscillation....................................................................................................... 35 Takeoff and landing into wind. ................................................................................................................................... 35 Using flap during the landing phase. ......................................................................................................................... 35 Attitude during descent path...................................................................................................................................... 35 The approach path angle........................................................................................................................................... 35 The landing roll.......................................................................................................................................................... 35 Airspeed fluctuations. ................................................................................................................................................ 37 Rate of descent or climb changes. ............................................................................................................................ 37 Unstable approach or flight path................................................................................................................................ 37 Wake Turbulence..........................................................................................................................................37 Vortex flow................................................................................................................................................................. 37 Aircraft Weight. .......................................................................................................................................................... 37 Speed. ....................................................................................................................................................................... 37
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