Tecnam P-Mentor - 2. Electrical System

1
st
Edition - Rev. 0
Section 3 – EMERGENCY PROCEDURES
ELECTRICAL SYSTEM
P-Mentor – Aircraft Flight Manual Page 3 - 7
2. ELECTRICAL SYSTEM
2.1. Low Volt
Annunciator Light
Alert
Low Voltage
Annunciation window
Alert
ESS VOLT
Essential Voltage
1. Circuit breaker(s)………………………….
CHECK
2. Avionic Master ……..…………………….
OFF
3. Pitot heat switch …………………………
OFF
4. Load Shedding …...……………………….
PERFORM
(Strobe lights set OFF)
5. Land as soon as practical
The ECU System requires an electrical power source for its
operation. If one alternator fails, continued engine operation is
assured by the other alternator. Therefore, the airframe loads
are supplied by battery.