Pilot Controls - Lycoming TEO-540-A1A Installation And Operation Manual

TEO-540-A1A Engine Installation and Operation Manual

Pilot Controls

Table 1 identifies pilot controls for the TEO-540-A1A engine. Figure 1 shows typical cockpit
controls.
EECS aircraft breaker set to ON
Ignition switch ON
Ignition switch OFF
Ignition switch START
Pre-Flight Test (PFT) switch
Fuel Pump Switch - ON
Fuel Pump Switch - AUTO
Fuel Pump Switch - OFF
Power Control Lever
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October 2018
PILOT CONTROLS AND ANNUNCIATORS
Table 1
Pilot Controls
Figure 1
EECS Cockpit Controls and Indicators
Airframe power is supplied to EECS
EECS enables fuel and spark to the engine
EECS disables fuel and spark to the engine
Enables power to the starter
Starts the pre-flight test sequence or sends an
acknowledgement and stops the pre-flight test
Turns the aircraft fuel boost pump ON
continuously
Enables control of the aircraft fuel boost
pump by the EECS
Turns the aircraft fuel boost-pump OFF
Controls engine power
Pilot Controls and Annunciators
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