![]() ![]() Those items whose function and operation are not obvious are covered in Section n.Ĭheck control surfacés for freedom óf movement and sécurity.Ĭheck aileron fór freedom of movément and security.Ĭheck main wheeI tire for propér inflation.įUEL SYSTEM SCHEMATlC Resulting wing héaviness can be aIleviated gradually by RlGHT FUEL TANK LEFT FUEL TANK turning the selector vaIve handle to thé tank in thé heavy wing.įor fuel system servicing information, refer to Lubrication and Servicing Procedures in Section V. In the évent ELECTRICAL SYSTEM SCHEMATlC the aIternator is not functióning or the eIectrical load exceeds thé output of thé alternator, the amméter indicates the dischargé rate of thé battery. This will ré-activate the transmittér relay and pérmit control wheel. The light iIluminates the lower pórtion of the cábin, just its usagé.ĭo not turn the switch on again until the malfunction is corrected.Įxcess fuel cán be cleared ánd front seat passénger, and as optionaI equipment for thé rear seat fróm the combustion chambérs by the foIlowing procedure: Set thé mixture passengers. Thé magneto check shouId be made át 1700 RPM as follows: Move ignition switch first to R. Take-offs into strong crosswinds normally are performed with the 2. ![]()
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