Follow this procedure to start the engine using the external power source.
1. Magnetos, Master switch, Generator switch: OFF
2. Open the receptacle door and insert the external power source’s plug into the
socket
3. Engine start-up procedure (see Sect. 4 in this manual)
4. Disconnect the external power source’s plug and close firmly the receptacle
door.
PITOT AND STATIC PRESSURE SYSTEMS
The airspeed indicator system for the aircraft is shown below and consists of
two static ports located on the sides of the aircraft forward of the cabin and by
a pitot tube located on the left wing strut.
FIG. 7-5. AIRSPEED INDICATOR SYSTEM