相关题目
In the description of the airplane's Engine, the accessories shall be described simply including: 1.Oil pump 2.Fuel pump 3.Hydraulic pump 4.Air pump 5.Tachometer 6.Torque meter 7.Electrical power source 8.Propeller synchronizer 9.Exhaust gas temperature probe
In the description of the airplane's Engine, the cooling system including cowl flaps shall be described.
In the description of the airplane's Engine, the air induction system shall be described including: 1.Path of flow of the air 2.Icing protection 3.Filtering 4.Supercharging/Turbocharging 5.Restrictions, warnings, tips
In the description of the airplane's Engine, proper operation and care of the engine when new and after the break in period should be described.
In the description of the airplane's Engine, the following information about engine instrumentation shall be described: 1.the method of operation 2.limits of readings and typical values where applicable.
In the description of the airplane's Engine, the engine controls shall be described including: 1.Throttle or power control 2.Propeller control 3.Mixture control 4.Cooling controls 5.Turbocharger controls 6.Friction lock
In the description of the airplane's Engine, give the following information as deemed necessary: 1.Manufacturer and model number 2.Type of engine, number of cylinders, type of compressor, etc. 3.Rated power 4.Rated engine speed 5.Gear reduction if applicable 6.Accessories normally installed 7.Turbocharging or other augmentation 8.Restrictions, warnings, tips
In the description of the airplane's Control Locks, how to engage control locks or secure control surfaces shall be explained.
In the description of the airplane's Doors, Windows and Exits, precise instructions for using emergency exits shall be given.
In the description of the airplane's Doors, Windows and Exits, how to close a door or window if it opens accidentally in flight and any restrictions there may be on purposely opening in flight shall be discussed.
