19.4.14) Battery
19.4.15) Relay
19.5) Internal consumer of electric power
▲ WARNING: The power consumption of extra loads has to be limited to the extent
item
fuel pump (main) ........................... max.
fuel pump (stand by) ..................... max.
TCU
(1
servo motor ................................... max.
warning lamp
caution lamp
sum
(3
(1
internal power consumption, without servo motor and lamps
(2
standard value, actual value up to aircraft manufacturer
(3
without electric starter and start relay
A complete electrical load analysis covering all installed loads must be calculated by the
aircraft manufacturer.
Effectivity: 914 Series
Edition 2 / Rev. 0
INSTALLATION MANUAL
See Fig. 69.
■ CAUTION:
To warrant reliable engine start use a battery of at least 16 Ah
capacity (depending on the type and specification we recom-
mend 18 Ah).
See Fig. 69.
that the internal need of power (fuel pumps, TCU, servo etc.) is always
covered.
Refer to graph (current output over speed) of the integrated generator
and the external alternator.
........................................... max.
(2
............................. approx.0,25 A
(2
.............................. approx.0,25 A
...........................................
BRP-Rotax
current consumption
3 A
3 A
0,3 A
1 A
~ 8 A
page 126
July 01/2008