Aeronautical Electrical System


The aeronautical electrical system works mainly with a Battery - 20230129064209 and an Alternator - 20230126105047. They're both switched on in normal operation.

A Regulator allows the alternator to provide exactly the power required by the servos.

Why is the Ammeter - 20230126110013 positive when starting?

After starting, the ammeter is positive because the battery has been discharged and must be recharged by the alternator.

Composition

Faults

Easement failure

In the event of a malfunction, the C.A.P.S procedure is used:

In case of blown circuit breaker or fuse :

Under load

Negative current => Check fuse or circuit breaker ALT fuse.

Overloaded

Positive current => Regulator problem: switch off the alternator.

Alternator out of order

Relieve the electrical load by reducing the number of services used.

Static Electricity

Beware of static electricity which may cause abnormal operation of the utilities.

The aircraft is equipped with a number of electrostatic dissipators to get rid of this electricity.

Faulty treated

Once a fault has been dealt with, the B.A.D. sequence is carried out:

META

Status:: #wiki/notes/mature
Plantations:: Aerotechnics - 20230216083955
References:: Le Manuel de Pilotage d'Avion